MAINTENANCE / OPERATIONAL /
PLACARDING PROCEDURES MANUAL
Including Aircraft GV-SP (G550/G500)
and Aircraft GIV-X (G450/G350)
Revision 8
November 7, 2014
GAC DOC. No. V-1
G
C
2014 Gulfstream Aerospace
Corporation
DISCLAIMER FOR MAINTENANCE / OPERATIONAL / PLACARDING
PROCEDURES MANUAL (GAC DOC. NO. GV-1)
The technical information presented herein has been determined to be correct at time of publication. However, should a
direct conflict exist between this and other official publications, e.g., Master Minimum Equipment List (MMEL), Airplane
Flight Manuals (AFM), Maintenance Manuals, those publications take precedence.
COPYRIGHT 2014 GULFSTREAM AEROSPACE CORPORATION
All rights reserved, including the right to reproduce this publication. No part may be reproduced, stored in any retrieval
system, or transmitted in any part or form or by any means, electronic, photocopying, microfilm, microfiche, mechanical,
or otherwise, without prior written permission of Gulfstream Aerospace Corporation.
TABLE OF CONTENTS
PAGE
FRONT MATTER ....................................................................................................................................................................................................................................................... F-1
Table of Contents ................................................................................................................................................................................................................................ F-1
General Information .......................................................................................................................................................................................................................... F-14
Revision Log ..................................................................................................................................................................................................................................... F-16
Minimum Navigational Equipment Table ......................................................................................................................................................................................... F-18
En Route Navigation Requirements .................................................................................................................................................................................................. F-20
Future Air Navigation System (FANS) Requirement ....................................................................................................................................................................... F-21
SECTION ONE – LINE REPLACEABLE UNIT (LRU) COMPONENT RELIEF ............................................................................................................................................. 1-1
ATA 21
AIR CONDITIONING........................................................................................................................................................................................................................... 21-1
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Cabin Altitude Indicator (Overhead Panel) ....................................................................................................................................................................................... 21-1
Cabin Differential Pressure Indicator ................................................................................................................................................................................................ 21-2
HON TUS Calculator ........................................................................................................................................................................................................................ 21-3
Cabin Rate of Climb Indicator .......................................................................................................................................................................................................... 21-4
Automatic Pressurization Control Systems ....................................................................................................................................................................................... 21-4
Manual Pressurization Control System ............................................................................................................................................................................................. 21-5
Semi-Auto Pressurization Control System ........................................................................................................................................................................................ 21-5
Cabin Altitude Pressure Warning System ......................................................................................................................................................................................... 21-6
Pressurization Outflow Valve Position Indicator .............................................................................................................................................................................. 21-6
Cockpit Zone Temperature Control System & Cabin Zone Temperature Control Systems.............................................................................................................. 21-7
Cockpit/Cabin Zone Temperature Indicators (Overhead Panel) ....................................................................................................................................................... 21-8
Duct Temperature Indicators (Overhead Panel) ................................................................................................................................................................................ 21-8
Environmental Control System (ECS) Packs .................................................................................................................................................................................... 21-9
Three-In-One Cabin Pneumatic Pressurization Monitoring Instrument ............................................................................................................................................ 21-9
Air Conditioning System Pack Inlet Valves .................................................................................................................................................................................... 21-10
Outflow Valve System .................................................................................................................................................................................................................... 21-10
Pressure Relief Valve ...................................................................................................................................................................................................................... 21-11
Cabin Pressure Indicator and Control Panel .................................................................................................................................................................................... 21-12
Selector Panel (Semi-Auto) ............................................................................................................................................................................................................. 21-13
Remote Filter (Pressure Relief Valve PRV) .................................................................................................................................................................................... 21-13
CPAM (Cabin Pressure Acquisition Module) ................................................................................................................................................................................. 21-13
Ram Air System .............................................................................................................................................................................................................................. 21-14
PSU Fan .......................................................................................................................................................................................................................................... 21-15
Front Matter
F-1
TABLE OF CONTENTS
(CONTINUED)
ATA 22
AUTO FLIGHT ...................................................................................................................................................................................................................................... 22-1
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ATA 23
Autothrottle Systems ......................................................................................................................................................................................................................... 22-1
Performance Management Systems (SmartPerf/TOLD) ................................................................................................................................................................... 22-1
Control Wheel Autopilot Disconnect Buttons ................................................................................................................................................................................... 22-1
Autothrottle Disconnect Buttons (on Thrust Lever Handles) ............................................................................................................................................................ 22-2
Autothrottle Engage/Disengage Switches (on Thrust Lever Stem) ................................................................................................................................................... 22-2
Touch Control Steering Switches (TCS) ........................................................................................................................................................................................... 22-2
Autopilots (Flight Guidance Computer (FGC) / Flight Directors) .................................................................................................................................................... 22-3
Yaw Damper Systems ....................................................................................................................................................................................................................... 22-3
Takeoff/Go-Around (TO/GA) Buttons (on Power Lever Handles) ................................................................................................................................................... 22-4
Mach Trim Systems (GV/SP/G-IV-X only) ...................................................................................................................................................................................... 22-5
COMMUNICATIONS ........................................................................................................................................................................................................................... 23-1
1. Communications Systems (VHF, UHF) ............................................................................................................................................................................................ 23-1
2. Cockpit Voice Recorder (CVR) ........................................................................................................................................................................................................ 23-2
3. Selective Call System (SELCAL) ..................................................................................................................................................................................................... 23-3
4. Emergency Locator Transmitters (ELT) ........................................................................................................................................................................................... 23-4
5. Crewmember Interphone System ...................................................................................................................................................................................................... 23-5
6. Interphone Systems ........................................................................................................................................................................................................................... 23-8
7. Cockpit Speakers ............................................................................................................................................................................................................................... 23-8
8. Passenger Address Systems (PA) ...................................................................................................................................................................................................... 23-9
9. Satellite Communication Systems ................................................................................................................................................................................................... 23-11
10. Prerecorded Passenger Announcement Systems ............................................................................................................................................................................. 23-11
11. Flight Deck Hand Microphones ...................................................................................................................................................................................................... 23-11
12. Flight Deck Headsets Earphones / Headphones and Boom Microphones ....................................................................................................................................... 23-12
13. Right Side Radio Frequency Management Unit (RFMU) (GV)...................................................................................................................................................... 23-14
14. Alerting System (Audio/Visual) ...................................................................................................................................................................................................... 23-14
15 Handset Systems ............................................................................................................................................................................................................................. 23-15
16. Radio Tuning Functions (GV-SP, GIV-X) ...................................................................................................................................................................................... 23-16
17. High Frequency (HF) Communication Systems ............................................................................................................................................................................. 23-17
18. NAVCOM Radio (GV-SP, GIV-X) ................................................................................................................................................................................................ 23-17
19. Audio Interface Units (AIUs) (GV only) ........................................................................................................................................................................................ 23-18
20. Datalink System (GV) ..................................................................................................................................................................................................................... 21-18
21. Modular Radio Cabinet (MRC) Power Supplies (GV-SP, GIV-X)................................................................................................................................................. 23-19
22. Headsets .......................................................................................................................................................................................................................................... 23-19
23. Flight Deck Hand Microphones ...................................................................................................................................................................................................... 23-19
24. Communications Management Function / CMF (GV-SP/GIV-X) .................................................................................................................................................. 23-20
25. Controller Pilot Data Link Communications (CPDLC) .................................................................................................................................................................. 23-20
Front Matter
F-2
TABLE OF CONTENTS
(CONTINUED)
ATA 24
ELECTRICAL POWER........................................................................................................................................................................................................................ 24-1
1. Engine Generators ............................................................................................................................................................................................................................. 24-1
2. APU Generator .................................................................................................................................................................................................................................. 24-4
3. Transformer-Rectifier Units (TRUs) ................................................................................................................................................................................................. 24-4
4. Battery Chargers................................................................................................................................................................................................................................ 24-5
5. Main Airplane Batteries .................................................................................................................................................................................................................... 24-5
6. Battery Ammeters (Overhead Panel)................................................................................................................................................................................................. 24-6
7. Battery Voltmeters ............................................................................................................................................................................................................................ 24-6
8. Electrical Power System EICAS Displays ........................................................................................................................................................................................ 24-7
9. Master Power Switch Lights (Left, Right, APU, EXT) ................................................................................................................................................................... 24-11
10. Battery Temperature Indicating System .......................................................................................................................................................................................... 24-11
11. Standby Electrical System ............................................................................................................................................................................................................... 24-11
12. External Power System ................................................................................................................................................................................................................... 24-12
13. Low Battery Power Audible Warning System (Sonalert) ............................................................................................................................................................... 24-12
14. Ground Service Bus System ............................................................................................................................................................................................................ 24-12
15. 50Hz/60Hz AC Electrical Power Systems ...................................................................................................................................................................................... 24-12
16. IRU Back Up Batteries (GV) .......................................................................................................................................................................................................... 24-12
ATA 25
EQUIPMENT/FURNISHINGS............................................................................................................................................................................................................. 25-1
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Overwater Equipment ....................................................................................................................................................................................................................... 25-1
Passenger Seats ................................................................................................................................................................................................................................. 25-1
Crewmember Shoulder Harnesses..................................................................................................................................................................................................... 25-4
Observer Seat(s) ................................................................................................................................................................................................................................ 25-5
Megaphones ...................................................................................................................................................................................................................................... 25-6
Floatation Devices ............................................................................................................................................................................................................................. 25-6
"Fasten Seat Belt While Seated" Signs or Placards ........................................................................................................................................................................... 25-7
Storage Bins/Cabin, Galley and Lavatory Storage Compartment/Closets ........................................................................................................................................ 25-7
Cargo Restraint System ..................................................................................................................................................................................................................... 25-9
Flight Attendant Seat Assembly ...................................................................................................................................................................................................... 25-10
Galley/Cabin Waste Receptacles Access Doors/Covers ................................................................................................................................................................. 25-12
Exterior Lavatory Door Ashtrays .................................................................................................................................................................................................... 25-13
External Camera System ................................................................................................................................................................................................................. 25-13
Emergency Vision Assurance System (EVAS) ............................................................................................................................................................................... 25-13
Pilot Seat(s) ..................................................................................................................................................................................................................................... 25-14
Rudder Pedal Adjustment ................................................................................................................................................................................................................ 25-15
Cockpit Convenience Items............................................................................................................................................................................................................. 25-15
Keyed Locks.................................................................................................................................................................................................................................... 25-15
Front Matter
F-3
TABLE OF CONTENTS
(CONTINUED)
ATA 25
EQUIPMENT/FURNISHIGNS (continued) ....................................................................................................................................................................................... 25-15
19.
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25.
ATA 26
FIRE PROTECTION............................................................................................................................................................................................................................. 26-1
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ATA 27
Airplane Ladders ............................................................................................................................................................................................................................. 25-15
Baggage Compartment Shelves....................................................................................................................................................................................................... 25-16
Crewmember Flashlight Holder Assemblies (Including Flashlight) ............................................................................................................................................... 25-16
Non-Essential Equipment & Furnishings NEF ............................................................................................................................................................................... 25-17
Automatic External Defibrillator (AED) and/or Associated Equipment ......................................................................................................................................... 25-18
Emergency Medical Kit (EMK) and/or Associated Equipment ...................................................................................................................................................... 25-18
First Aid Kit and/or Associated Equipment .................................................................................................................................................................................... 25-19
Portable Fire Extinguishers ............................................................................................................................................................................................................... 26-1
Wing Overheat Warning Systems ..................................................................................................................................................................................................... 26-1
APU Fire Detection System .............................................................................................................................................................................................................. 26-1
Rear Baggage Compartment Smoke Detector Systems..................................................................................................................................................................... 26-2
Lavatory Smoke Detection Systems .................................................................................................................................................................................................. 26-3
Lavatory Fire Extinguisher Systems ................................................................................................................................................................................................. 26-4
Galley Smoke Detection Systems ..................................................................................................................................................................................................... 26-4
Galley Fire Extinguishing Systems ................................................................................................................................................................................................... 26-5
Engine Fire Detection Systems ......................................................................................................................................................................................................... 26-5
Flame Detectors................................................................................................................................................................................................................................. 26-5
Electronic Equipment Rack Overheat Warning System .................................................................................................................................................................... 26-5
Passenger Compartment Closet Smoke Detectors............................................................................................................................................................................. 26-5
Entranceway Baggage Compartment Smoke Detectors .................................................................................................................................................................... 26-6
Cargo Compartment Fire Detection/Suppression Systems................................................................................................................................................................ 26-6
APU Fire Bottle................................................................................................................................................................................................................................. 26-7
FLIGHT CONTROLS ........................................................................................................................................................................................................................... 27-1
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9.
Rudder Limit Indication System ....................................................................................................................................................................................................... 27-1
Single Rudder Indication System ...................................................................................................................................................................................................... 27-1
Automatic Ground Spoiler System.................................................................................................................................................................................................... 27-1
Electric Elevator Trim System .......................................................................................................................................................................................................... 27-1
Control Wheel Elevator Trim Switches ............................................................................................................................................................................................ 27-2
Flap/Stabilizer Control Channels ...................................................................................................................................................................................................... 27-2
Single Speed Brake Indication System.............................................................................................................................................................................................. 27-2
Elevator Trim Actuator Heater Systems ............................................................................................................................................................................................ 27-2
Aileron Trim Actuator Heater ........................................................................................................................................................................................................... 27-3
Front Matter
F-4
TABLE OF CONTENTS
(CONTINUED)
ATA 27
FLIGHT CONTROLS (continued)........................................................................................................................................................................................................ 27-3
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ATA 28
FUEL ....................................................................................................................................................................................................................................................... 28-1
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ATA 29
Autopilot Elevator Servos (GV-SP, GIV-X) ..................................................................................................................................................................................... 27-3
Autopilot Pitch Trim Servos (GV-SP, GIV-X) ................................................................................................................................................................................. 27-3
Autopilot Aileron Servos (GV-SP, GIV-X) ...................................................................................................................................................................................... 27-3
Autopilot Yaw Damper Servos (GV-SP, GIV-X) ............................................................................................................................................................................. 27-4
Stall Barrier Systems ......................................................................................................................................................................................................................... 27-4
Flight Control Synoptic Display........................................................................................................................................................................................................ 27-5
Gust Lock .......................................................................................................................................................................................................................................... 27-5
Fuel Tank Temperature Systems ....................................................................................................................................................................................................... 28-1
EICAS or Standby RFMU (GV) / MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems ..................................................................................................... 28-1
Fuel Low Quantity Warning Systems ............................................................................................................................................................................................... 28-3
Fuel Boost Pumps.............................................................................................................................................................................................................................. 28-3
Fuel Intertank Valve .......................................................................................................................................................................................................................... 28-4
Heated Fuel Return System (HFRS) (GV, GV-SP) .......................................................................................................................................................................... 28-4
Fuel Boost Pump Warning Systems .................................................................................................................................................................................................. 28-4
Fuel Crossflow Valve ........................................................................................................................................................................................................................ 28-5
Pressure Fueling System (Single Point Refueling)............................................................................................................................................................................ 28-6
Ground Service Control Panel ........................................................................................................................................................................................................... 28-6
Automatic Fueling System ................................................................................................................................................................................................................ 28-6
Fuel Cap Chains ................................................................................................................................................................................................................................ 28-6
Single Point Refueling Cap ............................................................................................................................................................................................................... 28-7
Mid Wing Ejector (MWE) System (GV, GV-SP) ............................................................................................................................................................................. 28-7
HYDRAULIC POWER ......................................................................................................................................................................................................................... 29-1
1.
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6.
7.
8.
9.
Brake Accumulator Pressure Gauge (Nose Wheel Well) .................................................................................................................................................................. 29-1
Auxiliary Hydraulic Pump Pressure Indicator................................................................................................................................................................................... 29-1
Power Transfer Unit (PTU) Hydraulic Pressure Indication............................................................................................................................................................... 29-1
PTU Hydraulic Pump (Auto Mode) .................................................................................................................................................................................................. 29-1
Auxiliary Hydraulic Pump (Auto Mode) .......................................................................................................................................................................................... 29-1
Left Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) ..................................................................................................... 29-2
Right Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) ................................................................................................... 29-2
Left Hydraulic System Quantity Indication (EICAS) ....................................................................................................................................................................... 29-2
Right Hydraulic System Quantity Indication (EICAS) ..................................................................................................................................................................... 29-2
Front Matter
F-5
TABLE OF CONTENTS
(CONTINUED)
ATA 29
HYDRAULIC POWER (continued) ...................................................................................................................................................................................................... 29-2
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ATA 30
ICE AND RAIN PROTECTION .......................................................................................................................................................................................................... 30-1
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ATA 31
Hydraulic Reservoir Temperature Sensors ........................................................................................................................................................................................ 29-3
Hydraulic Reservoir Replenishing System ........................................................................................................................................................................................ 29-3
Brake Accumulator Pressure Gauge (cockpit dial) ........................................................................................................................................................................... 29-3
Brake Synoptic Page Accumulator Pressure Indication .................................................................................................................................................................... 29-4
Cowl Anti-Ice Pressure Indication Systems ...................................................................................................................................................................................... 30-1
Wing Anti-Ice Systems ..................................................................................................................................................................................................................... 30-1
Windshield Heat Systems .................................................................................................................................................................................................................. 30-2
Side Window Heat Systems .............................................................................................................................................................................................................. 30-2
Anti-Ice Heater Switch Lights ........................................................................................................................................................................................................... 30-3
Pitot Heaters ...................................................................................................................................................................................................................................... 30-3
Ice Detection Systems ....................................................................................................................................................................................................................... 30-3
Cowl Anti-Ice Systems...................................................................................................................................................................................................................... 30-4
Cowl Pressure Differential Indication System .................................................................................................................................................................................. 30-6
Windshield Blower System ............................................................................................................................................................................................................... 30-6
Cabin Window Heat System ............................................................................................................................................................................................................. 30-7
INDICATING/RECORDING SYSTEM .............................................................................................................................................................................................. 31-1
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13.
14.
15.
Clocks (Cockpit) ............................................................................................................................................................................................................................... 31-1
Flight Data Recorder (FDR) Systems................................................................................................................................................................................................ 31-1
Brake Temperature Monitoring System (BTMS) .............................................................................................................................................................................. 31-3
G Monitor System ............................................................................................................................................................................................................................. 31-3
Electronic Checklist ......................................................................................................................................................................................................................... 31-4
Data Acquisition Unit (DAU) Channels (GV) .................................................................................................................................................................................. 31-4
Security System ................................................................................................................................................................................................................................. 31-4
Engine Cowl Open Indicating System .............................................................................................................................................................................................. 31-4
Airplane Personality Modules (APM) (GV-SP, GIV-X) .................................................................................................................................................................. 31-5
Plastic Guard Switch Covers ............................................................................................................................................................................................................. 31-5
Configuration Management Systems (GV-SP, GIV-X) .................................................................................................................................................................... 31-5
InfraRed Counter Measuring System (IRCM) or Directional InfraRed Counter Measuring System (DIRCM) ............................................................................... 31-5
Quick Access Recorder (QAR) ......................................................................................................................................................................................................... 31-6
XM Weather ...................................................................................................................................................................................................................................... 31-6
Modular Avionics Unit (MAU) Channels (GV-SP/GIV-X).............................................................................................................................................................. 31-6
Front Matter
F-6
TABLE OF CONTENTS
(CONTINUED)
ATA 32
LANDING GEAR................................................................................................................................................................................................................................... 32-1
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ATA 33
Anti-Skid System .............................................................................................................................................................................................................................. 32-1
Rudder Pedal Steering System .......................................................................................................................................................................................................... 32-1
Landing Gear Position Indicators ...................................................................................................................................................................................................... 32-2
Variable Gain Nose Wheel Steering.................................................................................................................................................................................................. 32-2
Nosewheel Steering Accessory Hardware (Torque Link Lanyards) ................................................................................................................................................. 32-2
Emergency Landing Gear Extension Bottle Pressure Gauge (Nose Wheelwell) .............................................................................................................................. 32-2
Emergency Landing Gear Extension Bottle Pressure Cockpit CAS Indication (Summary Page)..................................................................................................... 32-2
Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GIV-X) ....................................................................... 32-3
Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GV/GV-SP) ................................................................ 32-4
LIGHTS................................................................................................................................................................................................................................................... 33-1
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19.
Cockpit/Flight Deck/Flight Compartment Instrument Lighting Systems (Excluding EFIS and EICAS) ......................................................................................... 33-1
Passenger Cabin Interior Illumination Systems ................................................................................................................................................................................. 33-1
Passenger Lighted Information Signs ................................................................................................................................................................................................ 33-2
Position Light Bulbs .......................................................................................................................................................................................................................... 33-3
Beacon Light ..................................................................................................................................................................................................................................... 33-4
Strobes (Anti-Collision Lights) ......................................................................................................................................................................................................... 33-4
Wing Inspection Lights ..................................................................................................................................................................................................................... 33-4
Landing Lights .................................................................................................................................................................................................................................. 33-5
Taxi Light System ............................................................................................................................................................................................................................. 33-5
Wing Tip Taxi Light Systems ........................................................................................................................................................................................................... 33-5
Floor Proximity Emergency Escape Path Marking System Lights ................................................................................................................................................... 33-6
Pulselight System (Identification Lights) .......................................................................................................................................................................................... 33-6
Recognition Light System ................................................................................................................................................................................................................. 33-6
Logo Light System ............................................................................................................................................................................................................................ 33-6
Ramp Lights Systems ........................................................................................................................................................................................................................ 33-7
Flashlight Charging Systems ............................................................................................................................................................................................................. 33-7
Aft Compartment Lights (Boiler Room) ........................................................................................................................................................................................... 33-7
Cargo Compartment Light................................................................................................................................................................................................................. 33-7
Pylon Mounted Exterior Baggage Loading Light Systems ............................................................................................................................................................... 33-7
Front Matter
F-7
TABLE OF CONTENTS
(CONTINUED)
ATA 33
LIGHTS (continued) ............................................................................................................................................................................................................................... 33-8
20.
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22.
23.
24.
25.
26.
27.
28.
29.
ATA 34
Wheel Well Lights ............................................................................................................................................................................................................................ 33-8
Exterior Emergency Evacuation Lighting System ............................................................................................................................................................................ 33-8
Service Door Lights .......................................................................................................................................................................................................................... 33-8
Dim and Test Enunciator Channels ................................................................................................................................................................................................... 33-8
Airstair Lights ................................................................................................................................................................................................................................... 33-9
Dome Light ....................................................................................................................................................................................................................................... 33-9
Baggage Compartment Light ............................................................................................................................................................................................................ 33-9
Cockpit Flashlight ............................................................................................................................................................................................................................. 33-9
Wing Tip Position Light LED Element Banks ................................................................................................................................................................................ 33-10
Tail Position Light LED Element Banks ......................................................................................................................................................................................... 33-10
NAVIGATION........................................................................................................................................................................................................................................ 34-1
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22.
Directional Compass Reference Sensors ........................................................................................................................................................................................... 34-1
Attitude Reference Sensors ............................................................................................................................................................................................................... 34-1
Standby Flight Displays .................................................................................................................................................................................................................... 34-1
Weather Radar Systems..................................................................................................................................................................................................................... 34-5
VOR/ILS Navigation Systems .......................................................................................................................................................................................................... 34-6
Marker Beacon Systems .................................................................................................................................................................................................................... 34-6
Automatic Direction Finding Systems .............................................................................................................................................................................................. 34-6
ATC Transponder and Automatic Altitude Reporting Systems ........................................................................................................................................................ 34-7
Distance Measuring Equipment (DME) Systems .............................................................................................................................................................................. 34-8
Standby RMI (Electro-Mechanical) (GV) ......................................................................................................................................................................................... 34-8
Radio Altimeter Systems ................................................................................................................................................................................................................... 34-9
Long Range Navigation Systems (IRS, GPS and GNSSU) .............................................................................................................................................................. 34-9
Terrain Awareness and Warning System (TAWS) ......................................................................................................................................................................... 34-10
Lasertrak NDU (GV) ....................................................................................................................................................................................................................... 34-16
Flight Management Systems (CDU & Nav Computer Only) (GV only) ........................................................................................................................................ 34-17
Navigation Management System..................................................................................................................................................................................................... 34-18
Lightning Sensor Systems (LSS) .................................................................................................................................................................................................... 34-19
Stormscope ...................................................................................................................................................................................................................................... 34-19
Traffic Alert Collision and Avoidance System ............................................................................................................................................................................... 34-19
Microwave Landing Systems (MLS) .............................................................................................................................................................................................. 34-22
Symbol Generators (GV)................................................................................................................................................................................................................. 34-22
Guidance Panel Digital Indications and Mode Select Indications ................................................................................................................................................... 34-22
Front Matter
F-8
TABLE OF CONTENTS
(CONTINUED)
ATA 34
NAVIGATION (continued) .................................................................................................................................................................................................................. 34-26
23. Altitude Alerting System ................................................................................................................................................................................................................. 34-26
24. Display Units ................................................................................................................................................................................................................................... 34-27
25. Standby Magnetic Compass System (Flux Valve) (GV) ................................................................................................................................................................. 34-29
Magnetometer (GV-SP, GIV-X) ..................................................................................................................................................................................................... 34-29
26. Non-Stabilized Magnetic Compass ................................................................................................................................................................................................. 34-30
27. Head Up Display System ................................................................................................................................................................................................................ 34-30
28. Airborne Flight Information System (AFIS) ................................................................................................................................................................................... 34-31
29. Slip-Skid Indicator .......................................................................................................................................................................................................................... 34-31
30. Data Loader (GV)............................................................................................................................................................................................................................ 34-32
Data Management Unit (DMU) (GV-SP, GIV-X) .......................................................................................................................................................................... 34-32
31. Air Data Computers/Systems .......................................................................................................................................................................................................... 34-32
32. Integrated Avionics Computers (IACs) (GV) ................................................................................................................................................................................. 34-33
33. Bus Controllers (GV) ...................................................................................................................................................................................................................... 34-34
34. Airshow Controller System ............................................................................................................................................................................................................. 34-34
35. Windshear Warning and Flight Guidance System (Reactive) ......................................................................................................................................................... 34-35
36. Windshear Detection and Avoidance System (Predictive) .............................................................................................................................................................. 34-35
37. Cockpit Video Monitors .................................................................................................................................................................................................................. 34-35
38. Heads Up Checklist ......................................................................................................................................................................................................................... 34-35
39. Enhanced Vision System (EVS)...................................................................................................................................................................................................... 34-36
40. Terrain Server Function/EGPWM Modules (GV-SP, GIV-X) ....................................................................................................................................................... 34-36
41. Electronic Flight Bag ...................................................................................................................................................................................................................... 34-36
42. Advanced Graphics Modules (AGM) (GV-SP, GIV-X) ................................................................................................................................................................. 34-37
43. Cockpit Printer ................................................................................................................................................................................................................................ 34-38
44. Cursor Control Devices (GV-SP, GIV-X)....................................................................................................................................................................................... 34-38
45. Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) ................................................................................................................................................... 34-39
46. Advanced Graphics Module (AGM) Databases (GV-SP, GIV-X).................................................................................................................................................. 34-41
47. Charts Function (GV-SP, GIV-X) ................................................................................................................................................................................................... 34-41
48. Video Function (GV-SP, GIV-X).................................................................................................................................................................................................... 34-41
49. Automatic Dependent Sueviellance-Broadcast (ADS-B) System ................................................................................................................................................... 34-42
50. Right Side Display Controller (GV) ................................................................................................................................................................................................ 34-43
Right Side Display Controller (GV-SP/GIV-X) .............................................................................................................................................................................. 34-44
51. Synthetic Vision Primary Flight Display (SV PFD) Functions ....................................................................................................................................................... 34-45
52. DDA (Digital to Distance Adapter) (GV only) ............................................................................................................................................................................... 34-45
53. GNSSU WASS (Wide Area Augmentation System or SBAS – Space Based Augmentation System) Function ........................................................................... 34-45
54. CAS Scroll Switches ....................................................................................................................................................................................................................... 34-45
Front Matter
F-9
TABLE OF CONTENTS
(CONTINUED)
ATA 35
OXYGEN ................................................................................................................................................................................................................................................ 35-1
1. Passenger Oxygen System and Supply.............................................................................................................................................................................................. 35-1
2. Cabin Oxygen ON Warning System ................................................................................................................................................................................................. 35-1
3. Oxygen Service Panel Pressure Gauges ............................................................................................................................................................................................ 35-3
4. Portable Oxygen Dispensing Units (Bottle and Mask)...................................................................................................................................................................... 35-3
5. Oxygen Supply Warning Systems ..................................................................................................................................................................................................... 35-3
6. Protective Breathing Equipment (PBE)............................................................................................................................................................................................. 35-4
7. Electronic Equipment Rack Oxygen Pressure Gauges ...................................................................................................................................................................... 35-4
8. Cockpit Oxygen Pressure Indications ............................................................................................................................................................................................... 35-4
9. Therapeutic Oxygen .......................................................................................................................................................................................................................... 35-4
10. High Landing Field Elevation Passenger Oxygen Controller high Altitude Switch ......................................................................................................................... 35-5
ATA 36
PNEUMATIC ......................................................................................................................................................................................................................................... 36-1
1.
2.
3.
4.
ATA 38
WATER/WASTE ................................................................................................................................................................................................................................... 38-1
1.
2.
3.
4.
ATA 45
Bleed Air Systems ............................................................................................................................................................................................................................. 36-1
Bleed Air Hot Warning Systems ....................................................................................................................................................................................................... 36-4
Isolation Valve .................................................................................................................................................................................................................................. 36-6
Bleed Air System Switch Capsule Lights.......................................................................................................................................................................................... 36-6
Potable Water Systems ...................................................................................................................................................................................................................... 38-1
Lavatory Waste Systems (Including Wheelchair Accessible Lavatories) ......................................................................................................................................... 38-1
Lavatory Dump/Drain System........................................................................................................................................................................................................... 38-2
Vacuum Toilet Holding Tank Indicator ............................................................................................................................................................................................ 38-2
CENTRAL MAINTENANCE COMPUTER ....................................................................................................................................................................................... 45-1
1.
2.
Maintenance Data Acquisition Unit (MDAU) (GV) ......................................................................................................................................................................... 45-1
Central Maintenance Computer (CMC) (GV-SP, GIV-X) ................................................................................................................................................................ 45-1
Front Matter
F - 10
TABLE OF CONTENTS
(CONTINUED)
ATA 46
NEW TECHNOLOGY .......................................................................................................................................................................................................................... 46-1
1.
ATA 49
Electronic Flight Bag Systems (EFBs) .............................................................................................................................................................................................. 46-1
AIRBORNE AUXILIARY POWER .................................................................................................................................................................................................... 49-1
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
17.
18.
19.
20.
21.
22.
23.
24.
Auxiliary Power Unit (APU) ............................................................................................................................................................................................................. 49-1
APU EGT Indicators (EICAS and Overhead) ................................................................................................................................................................................... 49-1
APU Tachometers (EICAS and Overhead) ....................................................................................................................................................................................... 49-1
APU "READY" Light System........................................................................................................................................................................................................... 49-2
APU Remote Oil Quantity/Servicing System ................................................................................................................................................................................... 49-2
APU Oil Pressure Gauges ................................................................................................................................................................................................................. 49-2
APU Oil Temperature Gauges .......................................................................................................................................................................................................... 49-2
APU Fuel Pressure Gauges ............................................................................................................................................................................................................... 49-2
APU Start Indicator Light ................................................................................................................................................................................................................. 49-2
APU Air Load Control Valve ............................................................................................................................................................................................................ 49-3
APU External Fire Warning Alarm (Fire Warning Bell) .................................................................................................................................................................. 49-3
APU Air Inlet Door System .............................................................................................................................................................................................................. 49-3
Bleed Air Augmentation Valve (GV, GV-SP) .................................................................................................................................................................................. 49-4
Surge Control Valve (GV, GV-SP) ................................................................................................................................................................................................... 49-4
Ignition System Channels (GV, GV-SP) ........................................................................................................................................................................................... 49-4
EGT Thermocouple System (GV, GV-SP) ....................................................................................................................................................................................... 49-4
Temperature Resistance Bulb (T2) .................................................................................................................................................................................................... 49-5
Inlet Pressure Transmitter (P2) (GV, GV-SP) ................................................................................................................................................................................... 49-5
RPM Speed Sensor Channels (GV, GV-SP) ..................................................................................................................................................................................... 49-5
APU Hour Meter ............................................................................................................................................................................................................................... 49-5
Oil Temperature (GV, GV-SP) ......................................................................................................................................................................................................... 49-5
Deprime Solenoid (GV, GV-SP) ....................................................................................................................................................................................................... 49-6
Oil Heater (GV, GV-SP) ................................................................................................................................................................................................................... 49-6
APU Start/Engine Cowl Interrupt System ......................................................................................................................................................................................... 49-6
Front Matter
F - 11
TABLE OF CONTENTS
(CONTINUED)
ATA 52
DOORS .................................................................................................................................................................................................................................................... 52-1
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
ATA 71
POWERPLANT ..................................................................................................................................................................................................................................... 71-1
1.
ATA 73
EPA Tank Ejector Pump ................................................................................................................................................................................................................... 71-1
ENGINE FUEL & CONTROL ............................................................................................................................................................................................................. 73-1
1.
2.
3.
ATA 74
Door Warning Light System ............................................................................................................................................................................................................. 52-1
Cargo Door Operating System .......................................................................................................................................................................................................... 52-1
Cargo Door Warning Light System ................................................................................................................................................................................................... 52-1
Door Seal Pressure Indicator ............................................................................................................................................................................................................. 52-2
Main Entry Door Normal Operating System ..................................................................................................................................................................................... 52-2
Main Entry Door Acoustic Curtain/Door System ............................................................................................................................................................................. 52-2
Lavatory Door ................................................................................................................................................................................................................................... 52-3
Baggage Door Warning System ........................................................................................................................................................................................................ 52-3
Main Entry Door Warning System .................................................................................................................................................................................................... 52-3
Internal Baggage Door Warning System (GV, GV-SP) .................................................................................................................................................................... 52-3
Internal Pocket Doors ........................................................................................................................................................................................................................ 52-4
Cabin Over Wing Exit Window Warning System............................................................................................................................................................................. 52-4
Fuel Flow Indication Systems ........................................................................................................................................................................................................... 73-1
Fuel Low Pressure Warning Systems (EICAS) ................................................................................................................................................................................. 73-1
Engine FADEC Systems (GV, GV-SP) ............................................................................................................................................................................................ 73-2
Engine FADEC System (GIV-X) ...................................................................................................................................................................................................... 73-3
IGNITION............................................................................................................................................................................................................................................... 74-1
1.
2.
Ignition Systems ................................................................................................................................................................................................................................ 74-1
Ignition ON Indicator Systems .......................................................................................................................................................................................................... 74-2
Front Matter
F - 12
TABLE OF CONTENTS
(CONTINUED)
ATA 77
ENGINE INDICATING ........................................................................................................................................................................................................................ 77-1
1.
2.
3.
4.
5.
ATA 78
ENGINE EXHAUST .............................................................................................................................................................................................................................. 78-1
1.
ATA 79
Thrust Reversers ................................................................................................................................................................................................................................ 78-1
ENGINE OIL .......................................................................................................................................................................................................................................... 79-1
1.
2.
3.
4.
5.
ATA 80
HP Tachometer Indications EICAS................................................................................................................................................................................................... 77-1
Engine Vibration Monitor Systems Sensors...................................................................................................................................................................................... 77-1
Standby Engine Instruments Indicating System (RFMU) (GV) ........................................................................................................................................................ 77-2
Standby Engine Instruments on Multifunction Control Display (MCDU) (GV-SP, GIV-X) ........................................................................................................... 77-2
Engine Vibration Monitoring System ............................................................................................................................................................................................... 77-2
Low Oil Pressure Warning System ................................................................................................................................................................................................... 79-1
Engine Oil Replenishment System .................................................................................................................................................................................................... 79-1
Impending Oil Filter Bypass Indications ........................................................................................................................................................................................... 79-1
Oil Quantity Indication Systems (EICAS/Ground Service Control Panel) ....................................................................................................................................... 79-2
Oil Filter Pressure Switch Fault Indications ...................................................................................................................................................................................... 79-2
STARTING ............................................................................................................................................................................................................................................. 80-1
1.
2.
3.
4.
Engine Starting Systems .................................................................................................................................................................................................................... 80-1
Auto Start System.............................................................................................................................................................................................................................. 80-1
Start Valve Position Indications ........................................................................................................................................................................................................ 80-2
Start Valve Position Indicator Lights ................................................................................................................................................................................................ 80-3
SECTION TWO – CREW ALERTING SYSTEM (CAS) MESSAGE RELIEF ................................................................................................................................................... 2-1
Statement Page ........................................................................................................................................................................................................................................... 2-2
CAS Messages...........................................................................................................................................................................................................................2-3 thru 2-131
Front Matter
F - 13
General Information
Gulfstream has developed this manual to assist operators in development of their Maintenance, Operational, and
Placarding Procedures (MOP) for the Gulfstream V aircraft as required by the Federal Aviation Administration (FAA)
Advisory Circular 91-67 dated July 28, 1991. This manual is intended for use in conjunction with the Gulfstream V
Master Minimum Equipment List (MMEL), Revision 8, dated November 7, 2014. Operators must apply to local FAA
office for approval of a specific MEL and MOP for their aircraft. Part 91 operators should be aware that the published
MMEL is intended for 14 CFR 121, 125, 129 and 135 operations as specified in the preamble. 14 CFR 91 operators
must obtain a 14 CFR 91 Preamble from the local FAA office.
This manual’s revision number will reflect the last issued FAA approved MMEL revision number. Updates to this
manual prior to the next FAA approved MMEL revision will be identified by a point and a letter following the assigned
FAA revision number, e.g., first update will be reflected as Revision 8a.
The Aircraft Discrepancy Log Sheet where all inoperative items will be noted is referred to as ADLS throughout this
document. Those items marked with three asterisks (***) are optional items. Those items which are not production
installed items will require the operator to develop specific maintenance, operational and placarding procedures for
their installation.
The following was accomplished by the Original GV Maintenance, Operational, and Placarding Manual. Users should
review and become familiar with the manual.
1.
2.
3.
4.
Formatted manual in a table format similar to MMEL.
Electronically formatted in Microsoft Word for Windows 2.0
Corrected technical errors throughout the manual.
Corrected typographical errors throughout the manual.
Note:
If errors are noted in this manual, submit a fax providing details and suggested corrections for the error to
Gulfstream Technical Publications at (912) 965-3520.
Note:
If assistance is needed regarding the MMEL, MEL or MOP implementation or usage, contact the local FAA
office.
Front Matter
F - 14
NOTICE
NOTICE
NOTICE
Any time an item in the MMEL calls for an (M) procedure to be accomplished prior to dispatch with the
listed item inoperative, the definitions at the beginning of the MMEL states that these procedures are
normally accomplished by maintenance personnel. However, other personnel may be qualified and authorized
to perform certain functions.
The ultimate responsibility for the accomplishment of all maintenance
procedures, regardless of who performs them, is the responsibility of the operator. In short, a properly
trained flight crew member may perform an (M) procedure such as but not limited to pulling and collaring
circuit breakers, changing light bulbs, changing or moving Display Units, making adjustments to seats,
verifying proper operation of systems or components, swapping connectors from an inoperative unit to an
operative unit, and/or closing/locking of doors if that crew member has been trained to do so.
It is
recommended that training records be kept at the home base of operations for personnel that have been
trained to perform (M) procedures. The applicable paragraph from the MMEL is below.
15."(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished
prior to operation with the listed item inoperative. Normally these procedures are accomplished by
maintenance personnel; however, other personnel may be qualified and authorized to perform certain
functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test
equipment should be accomplished by maintenance personnel. The satisfactory accomplishment of all
maintenance procedures, regardless of who performs them, is the responsibility of the operator. Appropriate
procedures are required to be published as part of the operator's manual or MEL.
The FAA recently revised 14 CFR to address Extended Operations (ETOPS) of Multi-Engine Airplanes.
The new rule applies to GAC airplanes operated under 14 CFR Part 135 on stage lengths where the single
engine cruise segment exceeds 180 minutes. On those flights, the MMEL becomes more restrictive for
certain items. Those items have been identified in this MMEL revision by the words, "Except for ER
operations, . . .”.
Front Matter
F - 15
Revision Dates for Gulfstream Aerospace Model G-V, GV-SP (G550, G500), GIV-X (G450, G350) FAA
MOPP: (For an explanation of changes, refer to the Gulfstream Aerospace Model G-V, GV-SP (G550, G500), GIV-X
(G450, G350) FAA MMEL Highlights of Change page.)
Material Dated:
August 19, 1996
August 19, 1998
June 4, 2001
November 9, 2001
August 11, 2003
December 2, 2003
December 14, 2004
June 2, 2006
July 5, 2006
June, 2007
July 24, 2007
February 4, 2010
November 8, 2010
May 17, 2013
November 7, 2014
Reflects Update
Type:
Original
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Number:
0
1
2
2a
3
3a
4
4a
4b
5
6
7
7a
7b
8
Front Matter
F - 16
THIS PAGE INTENTIONALLY LEFT BLANK
Front Matter
F - 17
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MOP REV. NO.: 8
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
MOP DATE: 11/07/2014
MINIMUM NAVIGATIONAL EQUIPMENT
POSITION SENSORS
MINIMUM NAVIGATIONAL EQUIPMENT
FMS
Enroute
Terminal
Approach
FMS Modes
MNPS
AC 91-70x
AC 120-33
RNP (General)
AC 90-105
RNP 10
FAA Order 8400.12x
RNAV and RNP
Operations
Approaches With
Required Position
Sensors
B-RNAV
EASA AMC 20-4
AC 90-96A
RNP 4
FAA Order 8400.33x
RNP 2
AC 90-105
RNAV 2
AC 90-100A
RNP 1
AC 90-105
RNAV 1
AC 90-100A
P-RNAV
AC 90-96A/JAA TGL-10
RNAV-WAAS
LPV AC 90-107
RNAV-BARO
AC 90-105
RNP AR
AC 90-101
NOTE
GPS
DME/DME
VOR/DME
IRS
1
1
1
1
1
A, B
1
1
1
1
1
A, B
1
1
1
1
2
2
1
1
1
1
1
2
1
1
1
1
1
1
1
1
2
2
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
2
2
A, B, F
A, B, C
2
A, B
A, B, C, D
A
A, C
A, B, D
1
A, B, E
A, B
1
A, B, E
A, B, F
A
A
A
Front Matter
F - 18
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
MOP REV. NO.: 8
MOP DATE: 11/07/2014
MINIMUM NAVIGATIONAL EQUIPMENT
NOTES:
A. When more than one position sensor is available, the FMS will select the one with the lowest EPU.
B. The FMS may use any one of the indicated position sensors.
1) Aircraft may be flown on routes requiring two Long Range Navigation (LRN) systems provided that two FMS’s, two GPS position sensors or
two Inertial Reference System (IRS) position sensors are operational or one GPS and one IRS sensor are operational.
2) Aircraft may be flown on routes requiring one LRN system provided that one FMS, one GPS sensor, or one IRS position sensor is
operational.
C. Limited to 5.0 hours of IRS-only navigation after the last GPS, DME/DME, or VOR/DME update.
D. When DME/DME position sensor is used, one IRS position sensor must be available to bridge gaps in DME infrastructure. This is referred to on
charts as DME/DME/IRU.
E. P-RNAV does not require IRS support for the DME/DME position sensor.
F. VOR, VOR/DME, TACAN or VOR/DME RNAV approaches.
Front Matter
F - 19
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
MOP REV. NO.: 8
MOP DATE: 11/07/2014
EN ROUTE NAVIGATION REQUIREMENTS
RVSM Operations are authorized:
The following equipment must be operative:
 2 Air Data Systems (must be two of the following: 1, 2, 3)
 1 ATC Transponder with both altitude reporting systems operative on remaining transponder
 1 Flight Guidance Computer with operable autopilot “altitude hold” function
 1 Altitude Alerting System
 Traffic Alert and Collision Avoidance System (TCAS II)
NAT MNPS Operations are authorized:
To meet navigation accuracy requirements, two independent long range navigational systems must be operative.
B-RNAV (RNAV 5 or RNP5) Operations are authorized:
While at least one FMS is operating, and while at least one of the following pieces of equipment is operating: GPS / VOR and DME / IRS
Aircraft may be dispatched in B-RNAV area provided the following is complied with:
For IRS only, B-RNAV capability is provided for up to 2 hours without FMS sensor updating.
One VOR/DME must be available as a NAV source (possibility to revert to conventional navigation means in case loss of last B-RNAV system).
RNP10 Operations are authorized:
Aircraft may be dispatched in RNP10 area provided:
At least two Flight Management Systems are operative and at least two GPS are operative,
or
At least two IRS are operative.
For IRS only, RNP10 capability is provided for up to 5.0 hours in duration without FMS sensor updating.
P-RNAV (RNAV 1 or RNAV 2) Operations are authorized:
At least two Flight Management Systems are operative and either of the following navigation modes such that EPU does not exceed RNP requirements:




HYBRID
GPS
DME / DME
VOR / DME
Front Matter
F - 20
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
MOP REV. NO.: 8
MOP DATE: 11/07/2014
FUTURE AIR NAVIGATION SYSTEM (FANS) REQUIREMENTS
FANS 1/A Operations are authorized
The following equipment must be operative:
 2 MCDU's
 SATCOM for overwater or remote area flights
 1 VHF Datalink radio for overland flights
 1 CMF (Communications Management Function or Datalink Function)
 1 HF radio for overwater or remote area flights
Front Matter
F - 21
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
PAGE NUMBER: 1-1
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
SECTION ONE
LINE REPLACEABLE UNIT
(LRU) COMPONENT RELIEF
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
1. Cabin Altitude Indicator
(Overhead Panel)
PAGE NUMBER: 21-1
MMEL REV. NO.: 8
C
1
0
May be inoperative provided cabin
altitude is available on EICAS Synoptic
display.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Altitude Indicator and will be
noted on ADLS.
C
1
0
May be inoperative provided:
a) Cabin Pressure Selector Panel is
operative, and
b) Pressurization is operated in AUTO
mode.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Altitude Indicator and will be
noted on ADLS.
C
1
0
May be inoperative provided:
a) Cabin Differential Pressure
Indicator is operative, and
b) A chart is provided to crew to
convert Cabin Differential Pressure
to Cabin Altitude.
NOTE: See chart on page 21-3.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Altitude Indicator and will be
noted on ADLS.
D
1
0
May be inoperative provided airplane is
equipped with additional pneumatic threein-one cabin pressurization monitoring
instrument, and Cabin Altitude Indicator
portion is fully operative.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Altitude Indicator and will be
noted on ADLS.
C
1
0
(O) May be inoperative provided airplane
is operated in unpressurized
configuration.
None required.
To
operate
the
airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air
ON.
Monitor
cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard will
be placed adjacent to Cabin
Altitude Indicator and will be
noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
Cabin Differential
Pressure Indicator
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
2.
PAGE NUMBER: 21-2
MMEL REV. NO.: 8
D
1
0
May be inoperative provided cabin
differential pressure is available on
EICAS Synoptic display.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Differential Pressure
Indicator and will be noted on
ADLS.
C
1
0
May be inoperative provided:
a) Cabin Pressure Selector Panel is
operative, and
b) Pressurization is operated in AUTO
mode.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Differential Pressure
Indicator and will be noted
on ADLS.
D
1
0
May be inoperative provided:
a) Cabin Altitude Indicator is
operative, and
b) A chart is provided to crew to
convert Cabin Altitude to Cabin
Differential Pressure.
NOTE: See sample chart on page 21-3.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Differential Pressure
Indicator and will be noted
on ADLS.
D
1
0
May be inoperative provided airplane is
equipped with additional pneumatic threein-one cabin pressurization monitoring
instrument, and Cabin Altitude Indicator
portion is fully operative.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Differential Pressure
Indicator and will be noted
on ADLS.
C
1
0
(O) May be inoperative provided airplane None required.
is operated in unpressurized configuration.
To
operate
the
airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air
ON.
Monitor
cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard will
be placed adjacent to Cabin
Differential Pressure
Indicator and will be noted
on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
SYSTEM &
SEQUENCE
NUMBERS
21. AIR CONDITIONING
PAGE NUMBER: 21-3
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
Determine Delta P:
Input
Aircraft Alt (ft)
psia
51000
Cabin Alt (ft)
8000
Output
1.603 Delta P (psia)
9.313
10.916
Determine Cabin Altitude:
Input
Aircraft Alt (ft)
51000
Delta P (psia)
10.694
psia
Output
1.603 Cabin Alt (ft)
4848.8
Determine Aircraft Altitude:
Input
Cabin Alt (ft)
4848.8
Delta P (psia)
10.694
psia
12.297 Aircraft Alt (ft)
Output
50997.7
PROCEDURE
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
3.
Cabin Rate of Climb
Indicator
D
1
0
4.
Automatic
Pressurization
Control Systems
B
2
0
(continued)
PAGE NUMBER: 21-4
MMEL REV. NO.: 8
(O) Except for ER operations, may be
inoperative provided:
a) Manual Pressurization Control
System is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative, and
e) Airplane is operated in accordance
with AFM Limitations.
None required.
None required.
An Inoperative Placard will
be placed adjacent to Cabin
Rate of Climb Indicator and
will be noted on ADLS.
None required.
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. AFM, Section 2,
Normal Procedures, Before
Starting Engines. Flight crew
will operate airplane in
accordance with AFM, Section
1, Limitations, Cabin
Pressurization Control and
Section 3, Abnormal
Procedures, Loss of Automatic
Pressurization Control. For
Taxi, Takeoffs and Landings Max Cabin Pressure Differential
0.3 psi.
To
operate
the
airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air
ON.
Monitor
cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard
stating “AUTO INOP” will
be placed above FAULT /
MANUAL Switch and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 21-5
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
4.
Automatic
Pressurization
Control Systems
(continued)
B
2
0
(O) Except for ER operations, may be
inoperative provided airplane is operated
in unpressurized configuration.
5.
Manual Pressurization
Control System
C
1
0
6.
Semi-Auto
Pressurization
Control System
C
1
0
None required
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air ON. Monitor cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard
stating "AUTO INOP" will
be placed above FAULT/
MANUAL Switch and will
be noted on ADLS.
May be inoperative provided both
None required.
Automatic Pressurization Control Systems
are operative.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
8.
Pressurization Outflow
Valve Position Indicator
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
Cabin Altitude Pressure
Warning System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
7.
PAGE NUMBER: 21-6
MMEL REV. NO.: 8
C
1
0
May be inoperative provided:
a) Cabin Altitude and Differential
Pressure Indicators are operative,
b) Cabin Oxygen On Warning System
is operative, and
c) Airplane is operated in accordance
with AFM Limitations.
C
1
0
C
1
0
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by the
flight crew and will be noted
on ADLS.
(O) May be inoperative provided airplane None required.
is operated in unpressurized configuration.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air ON. Monitor cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard will
be placed in a prominent
position to be seen by the
flight crew and will be noted
on ADLS.
May be inoperative provided all other
components of the Cabin Pressure Control
Panel and Cabin Pressure Indicator are
operative.
None required.
An Inoperative Placard will
be placed on Outflow Valve
Position Indicator and will be
noted on ADLS.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
Cockpit Zone
Temperature Control
System & Cabin Zone
Temperature Control
Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
9.
PAGE NUMBER: 21-7
MMEL REV. NO.: 8
C
3
2
C
3
1
(O) May be inoperative provided:
a) Ram Air system is operative, and
b) Airplane is operated in
unpressurized configuration.
None required.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air ON. Monitor cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard will
be placed adjacent to
Cockpit/Cabin Temperature
Indicator and will be noted on
ADLS.
1) Automatic System
C
3
0
May be inoperative provided:
a) Associated manual control system
is operative, and
b) Associated temperature indicator is
operative.
None required.
None required.
An Inoperative Placard will
be placed on AUTO half of
capsule of Cockpit/Cabin
Temperature Selectors and
will be noted on ADLS.
2) Manual Systems
C
3
0
May be inoperative provided:
a) Associated automatic control
system is operative, and
b) Associated temperature indicator is
operative.
None required.
None required.
An Inoperative Placard will
be placed on MANUAL half
of capsule of Cockpit/Cabin
Temperature Selectors and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
11.
Duct Temperature
Indicators
(Overhead Panel)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
Cockpit/Cabin Zone
Temperature Indicators
(Overhead Panel)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
10.
PAGE NUMBER: 21-8
MMEL REV. NO.: 8
D
3
0
May be inoperative provided associated
None required.
Automatic Temperature Control System is
operative.
None required.
An Inoperative Placard will
be placed on affected
Temperature Indicator face
and will be noted on ADLS.
D
3
0
May be inoperative provided associated
zone temperature is available on EICAS
Synoptic display.
None required.
None required.
An Inoperative Placard will
be placed on affected
Temperature Indicator face
and will be noted on ADLS.
D
3
0
May be inoperative provided associated
Manual Temperature Control System is
operative.
None required.
None required.
An Inoperative Placard will
be placed on affected
Temperature Indicator face
and will be noted on ADLS.
D
3
0
None required.
None required.
An Inoperative Placard will
be placed on overhead panel
below the Zone/Duct Switch
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
12.
PAGE NUMBER: 21-9
MMEL REV. NO.: 8
Environmental Control
System (ECS) Packs
1) Pressurized
Configuration
C
2
1
Except for ER operations, may be
inoperative provided:
a) Inoperative ECS Pack is selected
OFF,
b) Bleed Air Isolation Valve is
CLOSED and OPERATIVE,
c) Right Main TRU is operative,
d) Airplane is operated at or below
FL410, and
e) Authothrottle must be operative and
engaged at or above FL400.
None required.
None required.
An Inoperative Placard will
be placed adjacent to affected
"ECS PACK" Switch and will
be noted on ADLS.
2) Unpressurized
Configuration
C
2
0
Except for ER operations, may be
inoperative provided outflow valve is
operative.
None required.
None required.
An Inoperative Placard will
be placed adjacent to affected
"ECS PACK" Switches and
will be noted on ADLS.
C
1
0
May be inoperative provided primary
Cabin Altitude and primary Cabin
Differential Pressure Indicators are
operative either in the overhead panel or
on the Synoptic Display.
None required.
None required.
An Inoperative Placard will
be placed on Three-In-One
Cabin Pneumatic
Pressurization Monitoring
Instrument face and will be
noted on ADLS.
13. Three-In-One Cabin
*** Pneumatic
Pressurization
Monitoring Instrument
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 21-10
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
14.
Air Conditioning
System Pack Inlet
Valves
C
2
1
(M) Except for ER operations, may be
inoperative provided:
a) Affected Valve is CLOSED and
deactivated electrically,
b) Associated Air Conditioning Pack
is selected OFF, and
c) Airplane is operated in accordance
with AFM Limitations.
Maintenance will ensure affected
Valve is "CLOSED" and electrically
deactivated when associated Air
Conditioning Pack switch is selected
"OFF". Associated Air Conditioning
CB must NOT be pulled. Refer to
AMM, Chapter 21-21-00. Flight
crew may perform maintenance
function if maintenance is
unavailable.
Flight crew may accomplish this task
if properly qualified and authorized.
CAUTION: Pulling (de-energizing)
associated Air Conditioning CB will
cause valve to open, allowing airflow
to restart.
None required.
An Inoperative Placard will
be placed on or below
affected ECS Pack Switch
and will be noted on ADLS.
15.
Outflow Valve System
C
1
0
(M) (O) May be inoperative provided:
a) Outflow valve is positioned to full
OPEN position and electrically
isolated,
b) Airplane is operated in
unpressurized configuration, and
c) Extended overwater operations are
not conducted.
Maintenance will ensure Outflow
Valve is positioned to full OPEN
position and electrically de-energized
by pulling the Cab Press Man Cont
breaker LEER E-8.
To operate the airplane
unpressurized, refer to AFM
Section 3-21-90. Also refer to
AFM Section 4-22-30 in the
event that smoke is detected oin
the baggage compartment.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
May be inoperative provided:
a) DC motor is operative, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1) AC Motors
C
2
1
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
Pressure Relief
Valve
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
16.
PAGE NUMBER: 21-11
MMEL REV. NO.: 8
C
1
0
(O) May be inoperative provided:
a) Cabin differential pressure and
cabin altitude displays are
operative,
b) Selected cabin altitude is 1,000 feet
higher than normal cabin altitude
for the cruise flight level, and
c) Flight crew monitors actual cabin
differential pressure and maintains
it at or below 9.5 psi.
None required.
Flight Crew will ensure:
a) Cabin Differential Pressure
and Cabin Altitude Displays
are operative.
b) Select Semi-Auto Operation
and selected Cabin Altitude is
1,000 feet higher than normal
Cabin Altitude for cruise
flight level.
c) Monitor actual Cabin
Differential Pressure and
maintain it at or below 9.5 psi.
An Inoperative Placard will
be placed on Cabin Pressure
Control Panel and will be
noted on ADLS.
C
1
0
(O) May be inoperative provided airplane
is operated in unpressurized
configuration.
None required.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air ON. Monitor cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard will
be placed on Cabin Pressure
Control Panel and will be
noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
17.
PAGE NUMBER: 21-12
MMEL REV. NO.: 8
Cabin Pressure
Indicator and
Control Panel
C
1
0
None required.
None required.
An Inoperative Placard will
be placed on Control Panel
and will be noted on ADLS.
1) Manual Light
C
1
0
None required.
None required.
An Inoperative Placard will
be placed on Control Panel
and will be noted on ADLS.
2) Control Knob
Deleted in Revision 7.
3) Flight/Landing Switch C
(Light Function Only)
1
0
None required.
None required.
An Inoperative Placard will
be placed on Control Panel
and will be noted on ADLS.
4) Fault/Manual Switch
(Light Function Only)
C
1
0
None required.
None required.
An Inoperative Placard will
be placed on Control Panel
and will be noted on ADLS.
5) Auto/Semi Switch
(Light Function Only)
C
1
0
None required.
None required.
An Inoperative Placard will
be placed on Control Panel
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 21-13
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
18.
Selector Panel
(Semi-Auto)
B
1
0
19.
Remote Filter
(Pressure Relief
Valve PRV)
B
1
0
20.
CPAM (Cabin
Pressure Acquisition
Module)
C
1
0
May be inoperative provided:
a) Auto system (Cabin Pressure
Control Panel) is operative, and,
b) Semi-auto mode is considered
inoperative.
May be inoperative provided both auto
systems are operative.
None required.
None required.
An Inoperative Placard will
be placed on Selector Panel
and will be noted on ADLS.
None required.
None required.
A Placard indicating filter is
removed will be displayed in
a prominent position to be
seen by flight crew and will
be noted on ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
21.
PAGE NUMBER: 21-14
MMEL REV. NO.: 8
Ram Air System
1) Pressurized
Configuration
C
1
0
May be inoperative provided:
None required.
a) Automatic Pressurization Control
System is operative,
b) Manual Pressurization Control
System is operative,
c) Bleed Air Pressure Regulating and
Shut-Off Systems are operative, and
d) Airplane is operated in accordance
with AFM Limitations and
Procedures.
None required.
An Inoperative Placard will
be placed adjacent to the Ram
Air Switch to be viewed by
the flight crew and will be
noted on the ADLS
2) Unpressurized
Configuration
C
1
0
(O) May be inoperative provided:
a) Aircraft is operated in
unpressurized configuration, and
b) Airplane is operated in accordance
with AFM Limitations and
Procedures.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON
if available. If not, select RAM
Air ON. Monitor cabin
differential pressure to be
nominally zero psid during the
flight.
An Inoperative Placard will
be placed adjacent to the Ram
Air Switch to be viewed by
the flight crew and will be
noted on the ADLS.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
21. AIR CONDITIONING
PSU Fan
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
22.
PAGE NUMBER: 21-15
MMEL REV. NO.: 8
C
1
0
(O) May be inoperative provided:
a) Ambient Temperature is 95 degrees
F (35 degrees C) or cooler,
b) TRU electrical loads are 50% or
less,
c) Right main TRU is operative, and
d) Both Environmental Control
System (ECS) Packs are operative.
None required.
Flight crew will:
a) Minimize ground operation
time, especially during hot
weather.
b) During Ground operation,
monitor TRU load – limit
load to 50%.
c) For ground operation
longer than 15 minutes
ensure main and baggage
doors are closed, APU air
is selected “ON” and
outflow valve is fully
OPEN.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
22. AUTO FLIGHT
1.
Autothrottle Systems
C
2
0
2.
Performance
Management Systems
(SmartPerf/TOLD)
(GV)
C
2
0
(GV-SP / GIV-X)
C
2
Control Wheel
Autopilot Disconnect
Buttons
C
2
3.
PAGE NUMBER: 22-1
MMEL REV. NO.: 8
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
May be inoperative provided Quick
Reference Handbook is immediately
available to the flight crew.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
0
May be inoperative provided Performance
Handbook is immediately available to the
flight crew.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1
May be inoperative provided:
a) Autopilot is not utilized below
1,500 feet AGL,
b) Approach minimums do not require
the use of the autopilot, and
c) Airplane is piloted from the side
with operative button.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
5.
6.
Autothrottle Engage /
Disengage Switches
(on Thrust Lever Stem)
Touch Control
Steering Switches
(TCS)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
22. AUTO FLIGHT
Autothrottle
Disconnect Buttons
(on Thrust Lever
Handles)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
4.
PAGE NUMBER: 22-2
MMEL REV. NO.: 8
C
2
1
C
2
0
C
2
1
C
2
0
D
2
0
May be inoperative provided Autothrottle
is not used.
May be inoperative provided Autothrottle
is not used.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed on Thrust Lever
Stem and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed on Thrust Lever
Stem and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed on Thrust Lever
Stem and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
22. AUTO FLIGHT
Autopilots (Flight
Guidance Computers
(FGC) / Flight
Directors)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
7.
PAGE NUMBER: 22-3
MMEL REV. NO.: 8
C
2
1
(M) (O) Except for ER operations or
where en route operations or approach
minimums require its use, may be
inoperative provided airplane is operated
in accordance with AFM Limitations in
the event operative FGC fails and Yaw
Damper is inoperative.
Maintenance will pull and reset the
affected IAC (GV) or MAU Channel
(GV-SP/GIV-X) and Guidance Panel
circuit breakers in attempt to reset the
AP/FGC. If AP/FGC does not
recover, no further action required.
Flight crew will observe AFM
limitations in the event the
operative AP/FGC fails and the
Yaw Damper is inoperative.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
Flight crew will ensure airplane
is operated in accordance with
AFM Limitations in the event
the operative Yaw Damper fails.
AN Inoperative Placard will
be displayed in a prominent
position to be viewed by the
flight crew and will be noted
on the ADLS.
NOTE: AP/FGC is required for MNPS,
RVSM, RNP and PRNAV operations.
8.
Yaw Damper Systems
C
2
1
(O) Except for ER operations, may be
inoperative provided airplane is operated
in accordance with AFM Limitations.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
22. AUTO FLIGHT
Takeoff/Go-Around
(TO/GA) Buttons (on
Power Lever Handles)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
9.
PAGE NUMBER: 22-4
MMEL REV. NO.: 8
C
2
1
May be inoperative provided approach
minimums do not require its use.
C
2
0
(O) May be inoperative provided:
None required.
a) Both power levers are operated
manually for takeoff and go-around,
and
b) Autopilot and Flight Director are
not used below 500 feet or MDA,
whichever is higher.
NOTE: Flight Director Takeoff and GoAround guidance and Autothrottles are
not available with both TO/GA switches
inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be viewed by the
flight crew and will be noted
on ADLS.
Flight Director and Autothrottle
are not available for Takeoff or
Go-Around with both TO/GA
buttons inoperative. Flight crew
shall use raw data and manual
throttles for takeoff and goaround. For takeoff, once
airborne and above 500 ft AGL,
pilot-not-flying (PNF) shall
select desired lateral mode
(HDG or LNAV) on guidance
panel as directed by pilot-flying
(PF). Additionally, PNF shall
select desired vertical mode
(FLCH or VS or FPA) and
engage autothrottle as directed
by PF. For go-around, after
flaps and landing gear have
been retracted and airplane is
above 500 ft AGL, PNF shall
select desired lateral mode
(HDG or LNAV) and vertical
mode (FLCH or VS or FPA) on
guidance panel and engage
autothrottle at direction of PF.
An Inoperative Placard will
be displayed in a prominent
position to be viewed by the
flight crew and will be noted
on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
22. AUTO FLIGHT
Mach Trim Systems
(GV-SP/GIV-X only)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
10.
PAGE NUMBER: 22-5
MMEL REV. NO.: 8
C
2
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be viewed by the
flight crew and will be noted
on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
Communications
Systems (VHF, UHF)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 23-1
MMEL REV. NO.: 8
D D-
0
Any in excess of those required by 14
CFR may be inoperative provided it is not
powered by the Emergency AC Bus,
Emergency DC Bus, Battery Bus, Battery
Direct Bus, or the DC Transfer Bus and
not required for emergency procedures.
None required.
None required.
NOTE: No. 1 VHF COMM
must be operative – powered by
the emergency bus.
An Inoperative Placard will
be placed adjacent to affected
Radio Frequency
Management Unit (GV) or
MCDU (GVSP/GIV-X) and
will be noted on ADLS.
NOTE: Comm 1, NAV 1 and ATC 1 are
powered by the Emergency Bus.
1)
VHF
Communication
Control Panels
***
a)
Frequency
Transer
Light
C
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
b)
Frequency
Transfer
Switch
C C-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
c)
Frequency
Selector
Knob
C C-
2
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
d)
Frequency
Indication
C C-
2
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
Cockpit Voice
Recorder (CVR)
(with Flight Data
Recorder (FDR)
Installed)
A A1
0
*** 1) Independent Power
Source
C C1
0
Cockpit Voice
Recorder (CVR)
(without Flight
Data Recorder
(FDR) Installed)
A A1
0
*** 1) Independent Power
Source
C C1
0
Cockpit Voice
Recorder (CVR)
(Operator Other
Than a Holder of
An Air Carrier or
Commercial Operator
Certificate)
A A1
0
*** 1) Independent Power
Source
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
2.
PAGE NUMBER: 23-2
MMEL REV. NO.: 8
May be inoperative provided:
a) Flight Data Recorder (FDR) is
operative, and
b) Repairs are made within three flight
days.
NOTE: Part 91 operators should refer to
14 CFR 91.609 for additional relief.
May be inoperative provided repairs are
made within three flight days.
NOTE: Part 91 operators should refer to
14 CFR 91.609 for additional relief
May be inoperative provided repairs are
made in accordance with applicable 14
CFRs.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Part 91 operators should refer to
14 CFR 91.609 for additional relief
C
C
1
0
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
Channels
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
1)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3. Selective Call
*** System (SELCAL)
PAGE NUMBER: 23-3
MMEL REV. NO.: 8
C
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
One crew member shall monitor
the appropriate frequency.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
May be inoperative provided procedures
do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will ensure:
a) SELCAL decoder monitors
audio from the VHF and
HF communications
transceivers,
b) Recognizes receipt of the
tone set assigned to the
airplane, and
c) Provides the flight
compartment with call alert
signals.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
May be inoperative provided procedures
do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
4.
PAGE NUMBER: 23-4
MMEL REV. NO.: 8
Emergency Locator
Transmitters (ELT)
*** 1)
Survival
Type ELTs
D
-
-
Any in excess of those required by 14
CFR may be inoperative or missing.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
*** 2)
Fixed ELTs
A
-
0
(M) May be inoperative provided:
a) System is deactivated, and
b) Repairs are made within 90 days.
Maintenance will pull and collar the
ELT circuit breaker.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
-
0
May be missing provided repairs are made None required.
within 90 days.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
-
(M) Any in excess of those required by 14
CFR may be inoperative provided system
is deactivated.
Maintenance will pull and collar the
ELT circuit breaker.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
-
Any in excess of those required by 14
CFR may be missing.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
5. Crewmember
*** Interphone System
PAGE NUMBER: 23-5
MMEL REV. NO.: 8
C
2
1
B
-
-
None required.
None required.
An Inoperative Placard will
be placed on Interphone
System and will be noted on
ADLS.
None required.
Flight crew may use the PA to
communicate with the cabin
crew or speak to the cabin crew
directly in either the cockpit or
cabin to pass information.
An Inoperative Placard will
be placed on Interphone
System and will be noted on
ADLS.
1) Passenger
Configuration
a) Flight Deck to
Cabin, Cabin to
Flight Deck
Functions
(O) May be inoperative provided:
a) Flight deck to cabin and cabin to
flight deck interphone functions
operate normally on at least 50% of
the cabin handsets,
b) On wide-body airplanes, flight deck
to cabin and cabin to flight deck
interphone function operates
normally at one door for each pair
of exit doors, and
c) Alternate communications
procedures between the affected
flight attendants station(s) are
established and used.
NOTE: Any station function(s) that is
operative may be used.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 23-6
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
5. Crewmember
*** Interphone System
(cont’d)
1) Passenger
Configuration
b) Cabin to Cabin
Functions
B
2
0
(O) May be inoperative provided alternate
communications procedures between the
affected Flight Attendants station(s) are
established and used.
None required.
Cabin crew may use the PA to
communicate with the cabin
crew or speak to the cabin crew
directly in either the cockpit or
cabin to pass information.
An Inoperative Placard will
be placed on Interphone
System and will be noted on
ADLS.
None required.
Flight crew may use the PA to
communicate with the cabin
crew or speak to the cabin crew
directly in either the cockpit or
cabin to pass information.
An Inoperative Placard will
be placed on Interphone
System and will be noted on
ADLS.
NOTE: Any station function(s) that is
operative may be used.
B
-
-
(O) May be inoperative provided:
a) Cabin to cabin interphone functions
operate normally on at least fifty
percent of the cabin handsets,
b) On wide-body airplanes, cabin to
cabin interphone function operates
normally at one door for each pair
of exit doors, and
c) Alternate communications
procedures between the affected
flight attendants stations are
established and used.
NOTE: Any station function(s) that is
operative may be used.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 23-7
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
5. Crewmember
*** Interphone System
(cont’d)
1) Passenger
Configuration
c) Flight Deck to
Ground
1) Large Turbojet
Powered Airplanes
Operating under
Part 121
(continued)
C
1
0
(O) Flight interphone flight deck to
None required.
ground/ground to flight deck function may
be inoperative provided:
a) Alternate procedures are established
and used, and
b) Nose gear/forward fuselage service
interphone jack operates normally.
Flight crew may use hand
An Inoperative Placard will
signals for communications with be placed on Interphone
ground crew.
System and will be noted on
ADLS.
C
1
0
(O) Service interphone flight deck to
None required.
ground/ground to flight deck function may
be inoperative provided:
a) Alternate procedures are established
and used, and
b) Nose gear/forward fuselage service
interphone jack operates normally.
Flight crew may use hand
An Inoperative Placard will
signals for communications with be placed on Interphone
ground crew.
System and will be noted on
ADLS.
B
-
0
(O) May be inoperative provided alternate
procedures are established and used.
Flight crew may use hand
An Inoperative Placard will
signals for communications with be placed on Interphone
ground crew.
System and will be noted on
ADLS.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 23-8
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
5. Crewmember
*** Interphone System
(cont’d)
1) Passenger
Configuration
c) Flight Deck to
Ground (cont’d)
2) All other Aircraft /
Operations
C
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew may use hand
An Inoperative Placard will
signals for communications with be placed on Interphone
ground crew.
System and will be noted on
ADLS.
D
-
0
May be inoperative provided procedures
do not require its use.
None required.
None required.
An Inoperative Placard will
be placed on Interphone
System and will be noted on
ADLS.
6. Interphone Systems
***
D
-
0
None required.
None required.
An Inoperative Placard will
be placed on Flitephone
System and will be noted on
ADLS.
7.
C
2
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Cockpit Speakers
May be inoperative provided:
a) Affected speaker is not required for
aural warnings, and
b) An operative headset is provided
for each person on cockpit duty.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 23-9
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
8. Passenger Address
*** Systems (PA)
1)
Passenger
Configuration
B
1
0
(O) May be inoperative provided:
a) Alternate, normal, and emergency
procedures, and/or operating
restrictions are established and
used, and
b) Flight attendant alerting system
(audio and visual) operates
normally.
None required.
Flight crew will coordinate with
cabin crew prior to the flight.
Flight crews may use the flight
deck-to-cabin interphone system
to pass information to the cabin
crew. Also, the flight crew may
speak to the cabin crew directly
in either the cockpit or cabin to
pass information.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
Flight crew will coordinate with
cabin crew prior to the flight.
Flight crews may use the flight
deck-to-cabin interphone system
to pass information to the cabin
crew. Also, the flight crew may
speak to the cabin crew directly
in either the cockpit or cabin to
pass information.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
Flight crew will ensure alternate
procedures are established and
used.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Any station function(s) that is
operative may be used.
C
1
0
(O) May be inoperative provided:
a) PA not required by 14 CFR, and
b) Alternate, normal and emergency
procedures, and/or operating
restrictions are established and
used.
NOTE: Any station function(s) that is
operative may be used.
a) Lavatory Speakers
(continued)
C
-
-
(O) May be inoperative provided alternate
procedures are established and used.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 23-10
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
8. Passenger Address
*** Systems (PA)
(cont’d)
2)
Cargo Only
Configuration (Courier
/ Supernumerary
Address System)
a) Lavatory Speakers
C
1
0
(O) May be inoperative provided
alternate, normal and emergency
procedures are established and used.
None required.
Flight crew will coordinate with
cabin crew prior to the flight.
Flight crews may use the flight
deck-to-cabin interphone system
to pass information to the cabin
crew. Also, the flight crew may
speak to the cabin crew directly
in either the cockpit or cabin to
pass information.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided procedures
do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will ensure alternate
procedures are established and
used.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided procedures
do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
9. Satellite
*** Communication
Systems
PAGE NUMBER: 23-11
MMEL REV. NO.: 8
D
-
0
May be inoperative provided procedures
do not require their use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
10. Prerecorded
*** Passenger
Announcement
Systems
D
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will comply with
proviso in remarks column by
using manual PA system to
inform passengers. In addition,
the flight crew or cabin crew
may give direct oral instructions
to the passengers.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
11.
C
-
0
May be inoperative provided associated
boom microphone operates normally.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
Any in excess of those required by
regulation may be inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight Deck Hand
Microphones
HOLDER OF AN AIR
CARRIER OR
COMMERCIAL
OPERATOR
CERTIFICATE
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
2) Headset Earphones
/ Headphones
3) Active Noise
Canceling /
Reduction Function
(continued)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
Flight Deck Headsets
Earphones /
Headphones and Boom
Microphones
HOLDER OF AN AIR
CARRIER OR
COMMERCIAL
OPERATOR
CERTIFICATE
1) Headset Boom
Microphones
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
12.
PAGE NUMBER: 23-12
MMEL REV. NO.: 8
A
-
0
May be inoperative provided:
None required.
a) Associated hand microphone is
installed and operates normally, and
b) Repairs are made within three (3)
flight days.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
-
Any in excess of those required by
regulation may be inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
1
May be inoperative provided associated
flight deck speaker operates normally.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
-
Any in excess of those required by
regulation may be inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
May be inoperative provided normal
audio function of headset is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
12.
PAGE NUMBER: 23-13
MMEL REV. NO.: 8
Flight Deck Headsets
D
Earphones /
Headphones and Boom
Microphones
OPERATOR OTHER
THAN A HOLDER OF
AN AIR CARRIER
OR COMMERCIAL
OPERATOR
CERTIFICATE
1) Headset Boom
A
Microphones
-
-
Any in excess of those required by
regulation may be inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
-
0
May be inoperative provided:
None required.
a) Associated hand microphone is
installed and operates normally, and
b) Repairs are made in accordance
with applicable regulations.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
-
Any in excess of those required by
regulation may be inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2) Headset Earphones
/ Headphones
C
-
1
May be inoperative provided associated
flight deck speaker operates normally.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3) Active Noise
Canceling /
Reduction Function
D
-
0
May be inoperative provided normal
audio function of headset is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
Right Side Radio
Frequency
Management
Unit (RFMU)
(GV)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 23-14
MMEL REV. NO.: 8
C
1
0
May be inoperative provided:
a) Cross-side tuning function of the
left RFMU is operative,
b) Radio tuning function of both
FMS’s are operative, and
c) Inoperative RFMU is selected OFF.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
a) Flight Deck Call
Visual Alerting
System
B
1
0
May be inoperative provided the flight
deck audio alerting system is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
b) Flight Attendant
Visual Alerting
System
B
Flight crew will coordinate with
the flight attendant prior to
departure. Alternate means
include use of the PA, internal
phone system, or a series of
chimes from the NO SMOKE /
SEAT BELT ON / OFF feature.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
14. Alerting Systems
*** (Audio/Visual)
*** 1) Passenger
Configuration
***
***
(continued)
NOTE: The flight deck audio alerting
must always be operative.
1
0
(O) May be inoperative provided:
None required.
a) PA system is operative,
b) If affected visual alerting system is
used for Lavatory Smoke Detector
Alerting, an alternate Lavatory
Smoke Detector Alert (audio or
visual) is installed and operative,
and
c) Alternate procedures for contacting
flight attendants are established and
used.
NOTE 1: Passenger to Attendant Call
System is considered a Non-Essential
Equipment and Furnishings (NEF).
NOTE 2: Any visual alerting system
function(s) that are operative may be used.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
***
15.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
14.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
***
PAGE NUMBER: 23-15
MMEL REV. NO.: 8
Alerting Systems
(Audio/Visual)
(continued)
c) Flight Attendant
Audio Alerting
System
B
-
0
(O) May be inoperative provided:
None required.
a) PA system is operative,
b) If affected audio alerting system is
used for Lavatory Smoke Detector
Alerting an alternate Lavatory
Smoke Detector Alert (visual or
audio) is installed and operative,
and
c) Alternate procedures for contacting
flight attendants are established and
used.
NOTE 1: Passenger to Attendant Call
System is considered a Non-Essential
Equipment and Furnishings (NEF).
NOTE 2: Any audio alerting system
function(s) that are operative may be used.
Flight crew will coordinate with
the flight attendant prior to
departure. Alternate means
include use of the PA, internal
phone system, or a series of
chimes from the NO SMOKE /
SEAT BELT ON / OFF feature.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
(O) May be inoperative provided:
None required.
a) Flight deck to cabin communication
is operative, and
b) Alternate procedures are established
and used.
Flight crew will use the PA or
direct oral communications as
necessary.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided procedures
do not require its use.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Handset Systems
1) Passenger
Configuration
a) Flight Deck
(continued)
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
Handset Systems
1) Passenger
Configuration
b) Cabin
B
-
-
(O) May be inoperative provided:
a) Fifty percent of cabin handsets
operate normally,
b) On wide-body airplanes, one
handset must operate normally at
each pair of exit doors, and
c) Alternate communication
procedures between the affected
flight attendants station(s) are
established and used.
NOTE 1: An operative handset at an
inoperative flight attendant seat shall not
be counted to satisfy the fifty percent
requirement.
NOTE 2: Any handset(s) function(s) that
is operative may be used.
16.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
15.
PAGE NUMBER: 23-16
MMEL REV. NO.: 8
Radio Tuning
Functions
(GV-SP, GIV-X)
See item 34-45 MCDU for GV-SP, GIVX Radio Tuning Functions relief.
None required.
Flight crew will ensure alternate
procedures are established and
used.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
High Frequency (HF)
Communication
Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
17.
PAGE NUMBER: 23-17
MMEL REV. NO.: 8
D
-
-
Any in excess of those required by 14
CFR may be inoperative.
None required.
C
2
1
(O) May be inoperative while conducting None required.
operations that require two LRCS
provided:
a) SATCOM Voice or Data Link
operates normally,
b) Alternate procedures are established
and used,
c) SATCOM Voice coverage is
available over the intended route of
flight, and
d) If SATCOM Voice is to be used
over the intended route of flight,
SATCOM Voice short codes
(INMARSAT) or direct dial
commercial numbers (IRIDIUM)
must be available. If not available,
prior coordination with appropriate
ATS (FIR) facility is required.
None required.
An Inoperative Placard will
be placed adjacent to affected
Interphone System and will
be noted on ADLS.
The flight crew shall perform
the SATCOM preflight test on
the Datalink Manager menu.
Refer to the OM for additional
details. For GV, the crew will
perform a Satcom datalink and
voice call prior to departure.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: SATCOM Voice is to be used
only as a backup to normal HF
Communications.
18.
NAVCOM Radio
(GV-SP, GIV-X)
C
1
0
May be inoperative provided operations
do not require its use.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
19.
PAGE NUMBER: 23-18
MMEL REV. NO.: 8
Audio Interface Units
(AIUs) (GV only)
B
2
1
May be inoperative provided flight does
not require use of HF radio.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
20. Datalink System (GV)
***
C
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will use voice over
VHF/HF to relay pertinent
information to the air traffic
management system.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE 1: Data link system is required for
ADS-C and/or CPDLC operations.
NOTE 2: Datalink must be operative
whenever flights in RNP 4 airspace are
conducted.
D
-
0
May be inoperative provided routine
procedures do not require its use.
NOTE 1: Data link system is required for
ADS-C and/or CPDLC operations.
NOTE 2: Datalink must be operative
whenever flights in RNP 4 airspace are
conducted.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
Modular Radio Cabinet
(MRC) Power Supplies
(GV-SP, GIV-X)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
21.
PAGE NUMBER: 23-19
MMEL REV. NO.: 8
A
2
1
May be inoperative provided:
a) Associated Comm and Nav radios
and opposite ATC are operative,
and
b) Repairs are made within one flight
day.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Dispatch is acceptable with a
MRC 1 or MRC 2 failed and EICAS blue
messages “APM FAIL” and “ASCB
FAIL” displayed.
22.
Headsets
Combined with Item 12 in Rev. 8
23.
Flight Deck Hand
D
Microphones
OPERATOR OTHER
THAN A HOLDER
OF AN AIR CARRIER
OR COMMERCIAL
OPERATOR
CERTIFICATE
-
0
Any in excess of those required by
regulations may be inoperative.
C
-
0
May be inoperative provided associated
boom microphone operates normally.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
23. COMMUNICATIONS
24.
***
PAGE NUMBER: 23-20
MMEL REV. NO.: 8
Communications
C
Management Function
/ CMF (GV-SP/GIV-X)
-
0
(O) May be inoperative provided alternate None required.
procedures are established and used.
NOTE 1: Data Link system is required for
ADS-C and / or CPDLC operations.
Flight crew will use voice over
VHF/HF to relay pertinent
information to the air traffic
management system.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE 2: Datalink must be operative
whenever flights in RNP 4 airspace are
conducted.
D
-
0
May be inoperative provided routine
procedures do not require its use.
None required.
NOTE 1: Data Link system is required for
ADS-C and / or CPDLC operations.
NOTE 2: Datalink must be operative
whenever flights in RNP 4 airspace are
conducted.
25. Controller Pilot Data
*** Link Communications
(CPDLC)
1)
ATN B1
*** (PM-CPDLC/Link
2000+)
D
1
0
(O) May be inoperative provided alternate None required.
procedures do not require its use.
Flight crew will use voice over
VHF/HF or SATCOM to relay
pertinent information to the air
traffic management system.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2)
FANS 1/A
*** (ADS-C/CPDLC)
D
1
0
(O) May be inoperative provided enroute
operations do not require its use.
Flight crew will use voice over
VHF/HF or SATCOM to relay
pertinent information to the air
traffic management system.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
1.
PAGE NUMBER: 24-1
MMEL REV. NO.: 8
Engine Generators
(GV, GV-SP)
B
2
1
Except for ER operations, may be
inoperative provided:
a) APU Generator is used for all
phases of flight,
b) Airplane is operated at or below FL
450, and
c) Standby Electrical System is
operative.
None required.
None required.
An Inoperative Placard will
be placed above affected
Generator Switch on Electric
Power Control Panel (EPCP)
and will be noted on ADLS.
(GIV-X)
B
2
1
(O) Except for ER operations, may be
inoperative provided:
a) APU Generator is used for all
phases of flight,
b) Airplane is operated at or below FL
450,
c) Standby Electrical System is
operative, and
d) FSECU SPOST is performed
manually prior to the first flight of
the day for aiplanes equipped with
ASC 086 and dispatching with the
left generator inoperative.
None required.
See (O) procedure on next page.
An Inoperative Placard will
be placed above affected
Generator Switch on Electric
Power Control Panel (EPCP)
and will be noted on ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
PAGE NUMBER: 24-2
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
24. ELECTRICAL POWER
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
(GIV-X) (cont’d)
(O) Flight crew will:
a) On the Aircraft Maintenance Test Panel place the 'MAINT TEST Switch' and 'Flap Rig Switch' to the ON position,
b) In CMC, Select SYSTEM DIAGNOSTICS -> ATA 27 (Flight Controls) -> 41 (Flap / Stabilizer Controller Command Lane) -> TEST: MANUAL FHCM / HSEMU TEST,
c) Verify FHCM/HSEMU Manual Test page 1 of 3 is displayed and read and comply with all warnings, cautions, and notes,
d) Select confirm and verify FHCM/HSEMU Manual Test page 2 of 3 is displayed,
e) Verify the following is displayed on FHCM/HSEMU Manual Test page 2/3:
EXPECTED RESULTS
INITIAL
DGIO 1
DGIO 2
CONDITIONS
FSECU CMD
FSECU MON
A/C On Ground
TRUE
TRUE
Airspeed <45 KTS
TRUE
TRUE
Flap/Stab Rig SW ON
TRUE
TRUE
CMC COMM Active
FALSE
FALSE
HYDRAULIC STATUS
PROC1
PROC4
L HYD >2400 PSI
TRUE
TRUE
AUX HYD >2400 PSI
FALSE
FALSE
f)
g)
Select the “Initialize” softkey on FHCM/HSEMU Manual Test page 2/3,
Verify the following FHCM/HSEMU Manual Test page 2/3:
INITIAL
CONDITIONS
A/C On Ground
Airspeed <45 KTS
Flap/Stab Rig SW ON
CMC COMM Active
HYDRAULIC STATUS
L HYD >2400 PSI
AUX HYD >2400 PSI
EXPECTED RESULTS
DGIO 1
FSECU CMD
TRUE
TRUE
TRUE
TRUE
PROC1
TRUE
FALSE
DGIO 2
FSECU MON
TRUE
TRUE
TRUE
TRUE
PROC4
TRUE
FALSE
Note: Several seconds will be required after selecting the “Initialize” softkey before CMC COMM Active becomes “True”.
(continued on next page)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
SYSTEM &
SEQUENCE
NUMBERS
24. ELECTRICAL POWER
PAGE NUMBER: 24-3
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
(GIV-X) (cont’d)
(O) (continued)
h)
i)
j)
Select Confirm and verify FHCM/HSEMU Manual Test page 3/3 is displayed,
Select the “FHCM/HSEMU Test” softkey,
Verify that “FHCM/HSEMU Test In Progress” becomes active approximately 20 seconds,
Note: Flap/Stab Maintenance Required (Blue) will also be displayed in CAS while “FHCM/HSEMU Test In Progress” is active.
k)
Verify the following is displayed on FHCM/HSEMU Manual Test page 3/3:
Maintenance Messages
Expected
FHCM/HSEMU Test In Progress
INACTIVE
FHCM/HSEMU Test Abort – 115 VAC
INACTIVE
FHCM/HSEMU Test Abort – Left Hyd
INACTIVE
FHCM/HSEMU Test Abort – OGS
INACTIVE
FHCM/HSEMU Test Abort – Switches
INACTIVE
l) Select Done to complete the test,
m) On the Aircraft Maintenance Test Panel place the ‘Flap Rig Switch’ and ‘MAINT TEST Switch’ to the OFF position, and
n) Verify that ‘Flaps Failed’(A), ‘Stab Failed’(A), and ‘Flap/Stab Maint Reqd’(B) are NOT displayed in CAS.
PROCEDURE
PROCEDURE
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
3.
Transformer-Rectifier
Units (TRUs)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
APU Generator
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
2.
PAGE NUMBER: 24-4
MMEL REV. NO.: 8
B
1
0
(M) (O) Except for ER operations, may be
inoperative provided:
a) Both Engine Generators are
operative, and
b) Standby Electrical System is
operative.
Maintenance will pull and collar
APU GCU PWR circuit breaker on
left EER G-11.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will ensure:
a) BOTH Engine Driven
Generators are operative by
reference to the AC
synoptic and the absence of
failure message on CAS.
b) Standby Electrical System
is operative. (see QRH)
An Inoperative Placard will
be placed above AUX PWR
Switch on EPCP and will be
noted on ADLS.
C
1
0
(M) Except for ER operations, may be
inoperative provided APU is not used.
Maintenance will pull and collar
APU CONT #1 – left EER C-13 and
APU CONT #2 – right EER C-11.
Flight crew may accomplish this task
if properly qualified and authorized.
None required.
An Inoperative Placard will
be placed above AUX PWR
Switch on EPCP and will be
noted on ADLS.
B
5
4
(M) May be inoperative provided:
a) Both Generators are operative,
b) Both essential TRUs are operative,
c) Auxiliary TRU is operative,
d) APU Generator is operative,
e) Both Battery chargers are operative,
f) Both Main Airplane Batteries are
operative, and
g) Inoperative TRU circuit breaker on
the Power Distribution Box is
pulled and collared.
Maintenance will pull and collar
affected TRU CONTROL CB on
Power Distribution Box (PDB).
Maintenance will ensure AUX TRU
is operative and both essential TRUs
are operative.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
5.
Main Airplane
Batteries
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
Battery Chargers
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
4.
PAGE NUMBER: 24-5
MMEL REV. NO.: 8
B
2
1
(M) May be inoperative provided:
a) Both Engine Generators are
operative,
b) APU Generator is operative,
c) Associated Battery Charger circuit
breaker on the Power Distribution
Box is pulled and collared, and
d) Standby Electrical System is
operative.
Maintenance will:
None required.
a) Pull and collar CB of associated
Battery Charger (located on
PDB), and
b) Verify associated Battery
Charger by utilizing Operational
Test located in AMM Chapter
24-34-03.
An Inoperative Placard will
be placed above Battery
Charger Circuit Breakers and
will be noted on ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
B
2
1
(M) May be inoperative provided:
a) There are no other electrical power
source failures,
b) Associated Battery cables are
disconnected and secured,
c) Associated Battery Charger circuit
breaker on the Power Distribution
Box is pulled and collared, and
d) Associated battery circuit breaker is
pulled and collared.
Maintenance will ensure:
a) Standby Electrical System is
operative,
b) Pull and collar associated
"BATT CHGR" and "BATT
CONT" CB, and
c) Associated battery cables will
be disconnected and secured.
Refer to AMM Chapter 24-3400.
None required.
An Inoperative Placard will
be placed on affected "BATT
1, BATT 2" Master Switch on
the Electric Master Panel and
will be noted on ADLS.
B
2
1
(M)(O) May be inoperative provided:
a) Airplane is operated in day VMC,
b) Standby Electrical System is
operative,
c) Associated Battery cables are
disconnected and secured,
d) Associated Battery Charger circuit
breaker on the Power Distribution
Box is pulled and collared, and
e) Associated battery circuit breaker is
pulled and collared.
Maintenance will pull and collar
associated "BATT CHGR" and
"BATT CONT" CB. In addition,
associated battery cables will be
disconnected and secured. Refer to
AMM Chapter 24-34-00.
Flight crew will ensure airplane
is operated in day VMC only.
An Inoperative Placard will
be placed on affected "BATT
1, BATT 2" Master Switch on
the Electric Master Panel and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
7.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
Battery Ammeters
(Overhead Panel)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
6.
PAGE NUMBER: 24-6
MMEL REV. NO.: 8
C
2
0
May be inoperative provided:
a) Associated voltmeter is operative,
and
b) Both battery charger fail messages
are operative.
None required.
None required.
An Inoperative Placard will
be placed on affected Battery
Ammeter and will be noted
on ADLS.
C
2
0
May be inoperative provided battery
ammeter indications are available in
EICAS.
None required.
None required.
An Inoperative Placard will
be placed on affected Battery
Ammeter and will be noted
on ADLS.
(EICAS Indication)
C
2
0
May be inoperative provided the battery
ammeters in overhead panel are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Battery Voltmeters
(Overhead Panel)
C
2
0
May be inoperative provided associated
ammeter is operative.
None required.
None required.
An Inoperative Placard will
be placed on Voltmeter and
will be noted on ADLS.
C
2
0
May be inoperative provided Battery
Voltmeter indications are available on
EICAS.
None required.
None required.
An Inoperative Placard will
be placed on Voltmeter and
will be noted on ADLS.
C
2
0
May be inoperative provided Battery
Ammeters indications are available on
EICAS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
2
0
May be inoperative provided Battery
Voltmeters in the overhead panel are
operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(EICAS Indication)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
8.
PAGE NUMBER: 24-7
MMEL REV. NO.: 8
Electrical Power
System
EICAS Displays
1) L Gen Voltmeter
C
1
0
May be inoperative if the frequency and
loadmeter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2) L Gen Frequency
Meter
C
1
0
May be inoperative if the voltmeter and
loadmeter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3) L Gen Loadmeter
C
1
0
May be inoperative if the voltmeter and
frequency meter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4) R Gen Voltmeter
C
1
0
May be inoperative if the frequency and
loadmeter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
5) R Gen Frequency
Meter
C
1
0
May be inoperative if the voltmeter and
loadmeter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
8.
PAGE NUMBER: 24-8
MMEL REV. NO.: 8
Electrical Power
System
EICAS Displays
(continued)
6) R Gen Loadmeter
C
1
0
May be inoperative if the voltmeter and
frequency meter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7) APU Voltmeter
C
1
0
May be inoperative if the frequency meter
and loadmeter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
8) APU Frequency
Meter
C
1
0
May be inoperative if the voltmeter and
loadmeter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
9) APU Loadmeter
C
1
0
May be inoperative if the voltmeter and
frequency meter are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
11) Ext AC Pwr
Frequency Meter
12) Ext AC Loadmeter
(continued)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
Electrical Power
System
EICAS Displays
(continued)
10) Ext AC Pwr
Voltmeter
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
PAGE NUMBER: 24-9
MMEL REV. NO.: 8
D
1
0
May be inoperative provided:
a) the frequency meter and loadmeter
are operative, and
b) External AC power is not used.
None required.
None required.
D
1
0
May be inoperative if external AC power
is not used.
None required.
None required.
D
1
0
May be inoperative if the voltmeter and
loadmeter are operative.
None required.
None required.
D
1
0
May be inoperative if external AC power
is not used.
None required.
None required.
D
1
0
May be inoperative if the frequency and
voltmeter are operative.
None required.
None required.
D
1
0
May be inoperative if external AC power
is not used.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
8.
PAGE NUMBER: 24-10
MMEL REV. NO.: 8
Electrical Power
System
EICAS Displays
(continued)
13) Main, Essential and
AUX TRU
Voltmeters
C
5
0
May be inoperative if loadmeters are
operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
14) Main, Essential and
AUX TRU
Loadmeters
(GV-SP, GIV-X)
C
5
0
May be inoperative if the voltmeters are
operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
5
0
May be inoperative provided:
a) Voltmeters are operative, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative if the loadmeter is
operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative if external DC power
is not used.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(GV)
15) Ext DC Pwr
Voltmeter
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
8.
PAGE NUMBER: 24-11
MMEL REV. NO.: 8
Electrical Power
System
EICAS Displays
(continued)
16) Ext DC Pwr
Loadmeter
D
1
0
May be inoperative if the voltmeter is
operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative if external DC power
is not used.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
4
3
May be inoperative provided associated
AC loadmeter and voltmeter are operative
and selected for monitoring on the AC
Synoptic.
None required.
None required.
An Inoperative Placard will
be placed on affected Master
Power Switch and will be
noted on ADLS.
10. Battery Temperature
*** Indicating System
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
11.
C
1
0
None required.
None required.
An Inoperative Placard will
be placed adjacent to Standby
Electrical Master System and
will be noted on ADLS.
9.
Master Power Switch
Lights (Left, Right,
APU, EXT)
Standby Electrical
System
May be inoperative provided both engine
driven generators and APU generator are
operative.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
External Power System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
12.
PAGE NUMBER: 24-12
MMEL REV. NO.: 8
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
13. Low Battery Power
*** Audible Warning
System (Sonalert)
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
14.
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
15. 50Hz/60Hz AC
*** Electrical Power
Systems
D
-
0
(M)(O) May be inoperative provided
affected circuit breaker is pulled and
collared.
Maintenance will pull and collar
affected circuit breaker.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will brief the
passengers on the items that are
inoperative with the failure of
the power source for cabin
entertainment.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
16.
A
2
0
May be inoperative provided:
a) Airplane is operated in day VMC
conditions, and
b) Repairs are made within one (1)
flight day.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
2
0
May be inoperative provided:
a) All other components of the
Electrical Power system are
operative, and
b) Repairs are made within one (1)
flight day.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Ground Service Bus
System
IRU Back Up
Batteries (GV)
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
16.
PAGE NUMBER: 24-13
MMEL REV. NO.: 8
IRU Back Up
Batteries (continued)
(GV-SP, GIV-X)
B
2
1
(M) May be inoperative provided that the
affected battery is located in the #2 or #3
IRU back up battery position.
Maintenance will move affected
battery to the #2 or #3 position.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
2
0
May be inoperative provided:
a) Airplane is operated in day VMC
conditions, and
b) Repairs are made within one (1)
flight day.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: EICAS message “IRU Sec Pwr
Fail” will be displayed.
A
2
0
May be inoperative provided:
a) All other components of the
Electrical Power system are
operative, and
b) Repairs are made within one (1)
flight day.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
D
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
-
-
As required by 14 CFR.
None required.
None required.
If installed, an Inoperative
Placard will be placed in a
prominent position to be seen
by flight crew and will be
noted on ADLS.
May be inoperative provided:
None required.
a) Seat does not block an Emergency
Exit,
b) Seat does not restrict any passenger
from access to the main airplane
aisle, and
c) The affected seat(s) are blocked and
placarded "DO NOT OCCUPY".
None required.
A "Do Not Occupy" Placard
will be placed on affected
seat and will be noted on
ADLS.
NOTE: See 14 CFR 91.205, 91.509 or
135.167.
2.
Passenger Seats
D
-
-
NOTE 1: A seat with an inoperative seat
belt is considered inoperative.
NOTE 2: Inoperative seats do not affect
the required number of Flight Attendants.
NOTE 3: Affected seat(s) may include the
seat(s) behind and/or adjacent outboard
seats.
(continued)
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
Overwater Equipment
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 25-1
MMEL REV. NO.: 8
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
2.
PAGE NUMBER: 25-2
MMEL REV. NO.: 8
Passenger Seats
(continued)
1)
*** 2)
Recline
Mechanism
Underseat
Baggage
Restraining Bars
(continued)
D
-
-
(M) May be inoperative and seat occupied
provided seat back is secured in the full
upright position.
Maintenance will ensure seat back is
secured in full upright position.
None required.
A "Do Not Occupy" Placard
will be placed of affected seat
not secured in up-right
position and will be noted on
ADLS.
D
-
-
May be inoperative and seat occupied
provided seat back is immovable in full
upright position.
None required.
None required.
A "Do Not Occupy" Placard
will be placed of affected seat
not secured in up-right
position and will be noted on
ADLS.
C
-
-
(O) May be inoperative provided:
a) Baggage is not stowed under seat
with inoperative restraining bar,
b) Associated seat is placarded “DO
NOT STOW BAGGAGE UNDER
THIS SEAT”, and
c) Procedures are established to alert
Cabin Crew of inoperative
restraining bars.
None required.
Flight crew will advise cabin
crew which seat is affected and
mark this seat with a tag or
placard visible to crew and
passengers.
A "Do Not Stow Baggage
Under This Seat" Placard will
be placed of affected seat and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
2.
PAGE NUMBER: 25-3
MMEL REV. NO.: 8
Passenger Seats
(continued)
3)
a)
Armrests
Armrests with
Recline
Mechanism
b)
Armrest without
Recline
Mechanism
4)
Swivel
Mechanism
(continued)
D
-
-
(M) May be inoperative or missing and
Maintenance will ensure seat is
seat occupied provided:
secured in the full upright position if
a) Armrest does not block an
armrest is missing.
Emergency Exit,
b) Armrest does not restrict any
passenger from access to the main
airplane aisle, and
c) If armrest is missing, seat is secured
in the full upright position.
None required.
A "Do Not Occupy" Placard
will be placed of affected seat
not secured in up-right
position and will be noted on
ADLS.
D
-
-
May be inoperative or missing and seat
occupied provided:
a) Armrest does not block an
Emergency Exit, and
b) Armrest does not restrict any
passenger from access to the main
airplane aisle.
None required.
None required.
A "Do Not Occupy" Placard
will be placed of affected seat
and will be noted on ADLS.
C
-
-
May be inoperative and seat occupied
None required.
provided:
a) Associated seat does not block an
Emergency Exit,
b) Associated seat does not restrict any
passenger from access to the main
airplane aisle, and
c) Associated seat remains in takeoff
position.
None required.
A "Do Not Occupy" Placard
will be placed of affected seat
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
Passenger Seats
(continued)
5)
Divan High
Backs
C
-
-
May be inoperative and seat occupied
None required.
provided:
a) Associated seat does not block an
Emergency Exit,
b) Associated seat does not restrict any
passenger from access to the main
airplane aisle, and
c) Associated seat remains in takeoff
position.
None required.
A "Do Not Occupy" Placard
will be placed of affected seat
and will be noted on ADLS.
Electrical /
Electronic
Systems /
Components
C
-
-
(M) May be inoperative and seat occupied
provided associated component(s) is
deactivated.
Maintenance will disconnect bag and
stow the electrical connectors.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Crewmember Shoulder
Harnesses
B
Any in excess of those required by flight
deck crewmembers (including official
observer in observer's seat) may be
inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***6)
3.
MMEL DATE: 11/07/2014
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
2.
PAGE NUMBER: 25-4
MMEL REV. NO.: 8
-
-
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
4.
PAGE NUMBER: 25-5
MMEL REV. NO.: 8
Observer Seat(s)
1) Primary Observer
Seat (including
associated
equipment)
A
A
-
-
-
-
May be inoperative provided:
a) A passenger seat in the passenger
cabin is made available to an FAA
inspector for the performance of
official duties, and
b) Repairs are made within two (2)
flight days.
None required.
May be inoperative provided:
a) Required minimum safety
equipment (safety belt and oxygen)
is available,
b) Seat is acceptable to the FAA
inspector for performance of
official duties, and
c) Repairs are made within two (2)
flight days.
None required.
NOTE 1: These provisos are intended to
provide for occupancy of the above seats
by an FAA inspector when the minimum
safety equipment (oxygen and safety belt)
is functional and the inspector determines
the conditions to be acceptable.
NOTE 2: The pilot-in-command will
determine if the minimum safety
equipment is functional for other persons
authorized to occupy any observer seat(s).
(continued)
None required.
A "Do Not Occupy" Placard
will be placed on affected
seat and will be noted on
ADLS.
NOTE: Does not apply to
Part 91 operators.
None required.
A "Do Not Occupy" Placard
will be placed on affected
seat and will be noted on
ADLS.
NOTE: Does not apply to
Part 91 operators.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
4.
PAGE NUMBER: 25-6
MMEL REV. NO.: 8
Observer Seat(s)
(continued)
2) Observer Seat Not
Required by 14
CFR (including
associated
equipment)
5. Megaphones
***
D
-
0
NOTE: The pilot-in-command will
determine if the minimum safety
equipment is functional for other persons
authorized to occupy any observer seat(s).
None required.
None required.
A "Do Not Occupy" Placard
will be placed on affected
seat and will be noted on
ADLS.
NOTE: Does not apply to
Part 91 operators.
D
-
-
Any in excess of those required by 14
CFR may be inoperative or missing
provided:
a) Inoperative megaphone is removed
from passenger cabin,
b) Associated placard is removed or
obscured, and
c) Required distribution is maintained.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE 1: Megaphones are available to
meet 14 CFR 91.513 distribution
requirements.
NOTE 2: Not required for all Cargo
Operations.
6.
Flotation Devices
D
-
-
Any in excess of those required by 14
CFR may be inoperative. Inoperative
equipment will be removed from airplane.
NOTE: Flotation Devices are available to
meet 14 CFR 91.205, 91.509 or 135.167
distribution requirements.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
7.
"Fasten Seat Belt
*** While Seated”
Signs or Placards
C
-
-
One or more signs or placards may be
None required.
illegible or missing provided a legible sign
or placard is readable from each occupied
passenger seat.
8.
Storage Bins/Cabin,
*** Galley and Lavatory
Storage Compartment /
Closets
C
-
-
(M) May be inoperative provided:
a) Procedures are established to secure
the affected bin, compartment or
closet in the closed position,
b) Associated bin, compartment or
closet is prominently placarded DO
NOT USE,
c) Any emergency equipment located
in affected compartment is
considered inoperative, and
d) Affected bin, compartment or closet
is not used for storage of any items
except for those permanently
affixed.
NOTE: For overhead bins, if no partitions
are installed, the entire overhead bin is
considered inoperative.
(continued)
PAGE NUMBER: 25-7
MMEL REV. NO.: 8
None required.
A "Do Not Occupy" Placard
will be placed on any affected
seat from which signs are not
readable and will be noted on
ADLS.
Maintenance will verify that no
None required.
emergency equipment is stored in the
compartment, secure the
compartment CLOSED and placard it
against use for storage of any
equipment.
An Inoperative Placard will
be placed on affected Storage
Bins/Cabin, Galley and
Lavatory Storage
Compartment / Closets and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
C
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
Storage Bins/Cabin,
*** Galley and Lavatory
Storage Compartment /
Closets (continued)
PAGE NUMBER: 25-8
MMEL REV. NO.: 8
-
-
(M)(O) May be inoperative provided:
a) For non-retractable door, affected
doors is removed,
(continued)
b) For retractable doors, affected door
is removed or secured in the
retracted (fully open) position,
c) Affected bin, compartment or closet
is not used for storage of any items,
except those permanently affixed,
d) Affected bin, compartment or closet
is prominently placarded DO NOT
USE,
e) Procedures are established and used
to alert crew members and
passengers of inoperative bins,
compartments or closets, and
f) Passengers are briefed that
associated bin, compartment or
closet is not used.
Maintenance will verify that no
Flight crew will ensure
emergency equipment is stored in the passengers are briefed that bin
compartment, secure the
or compartment is not used.
compartment CLOSED and placard it
against use for storage of any
equipment.
An Inoperative Placard will
be placed on affected Storage
Bins/Cabin, Galley and
Lavatory Storage
Compartment / Closets and
will be noted on ADLS.
Maintenance will verify that no
None required.
emergency equipment is stored in the
compartment, secure the
compartment CLOSED and placard it
against use for storage of any
equipment.
An Inoperative Placard will
be placed on affected Storage
Bins/Cabin, Galley and
Lavatory Storage
Compartment / Closets and
will be noted on ADLS.
NOTE 1: For overhead bins, if no
partitions are installed, the entire overhead
bin is considered inoperative.
NOTE 2: Any emergency equipment
located in the affected bin, compartment
or closet (permanently affixed) is
available for use.
***
1) Storage
Compartment
Key Locks
D
-
0
(M) May be inoperative in unlocked
position provided doors can be secured by
other means.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
C
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
A
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
9.
Cargo Restraint
*** Systems
PAGE NUMBER: 25-9
MMEL REV. NO.: 8
-
-
-
-
(M) May be inoperative, or missing
provided:
a) Acceptable cargo loading limits
from an approved source, i.e., an
Approved Cargo Loading Manual,
or Weight and Balance Document
are observed, and
b) Repairs are made prior to the
completion of the next heavy
maintenance visit.
Maintenance will provide acceptable
cargo loading limits from an
approved source, i.e., an Approved
Cargo Loading Manual, or Weight
and Balance Document are observed.
May be inoperative, or missing provided
cargo compartment remains empty.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
1
0
(M)(O) Flight Attendant seat may be
inoperative provided:
a) Affected seat not occupied,
b) Flight Attendant displaced by
inoperative seat occupies the
passenger seat most accessible to
the inoperative seat,
c) Alternate procedures are established
and used as published in
crewmember manuals,
d) Folding type seat is stowed or
secured in the retracted position,
e) Passenger seat assigned to flight
attendant is placarded “FOR
FLIGHT ATTENDANT ONLY”,
and
f) Repairs are made within two (2)
flight days.
NOTE 1: An automatic folding seat that
will not stow automatically is considered
inoperative.
NOTE 2: A seat position with an
inoperative or missing restraint is
considered inoperative.
(continued)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
A
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
10. Flight Attendant
*** Seat Assembly
PAGE NUMBER: 25-10
MMEL REV. NO.: 8
NOTE 3: The above provisos apply to
flight attendant seats. Individual operators,
when operating with inoperative seats,
will consider the locations and
combinations of seats to ensure that the
proximity to exits and distribution
requirements of applicable regulations are
met.
Maintenance will ensure:
a) Folding type seat is stowed or
secured in the retracted position,
b) Passenger seat assigned to flight
attendant is placarded “FOR
FLIGHT ATTENDANT ONLY”
and
c) Repairs are made within two (2)
flight days.
Flight crew will ensure:
a) Affected seat or seat
assembly is not occupied,
b) Flight attendant displaced
by inoperative seat occupies
the passenger seat most
accessible to the inoperative
seat, and
c) Alternate procedures are
established and used as
published in crewmember
manuals.
An Inoperative Placard will
be placed on affected Flight
Attendant Seat and will be
noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
D
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
10. Flight Attendant
*** Seat Assembly
(continued)
PAGE NUMBER: 25-11
MMEL REV. NO.: 8
1
0
(M) May be inoperative provided:
a) Flight Attendant is not required by
14 CFR,
b) Affected seat is not occupied, and
c) Folding type seat stows
automatically or is secured in the
retracted position.
Maintenance will ensure:
a) Folding type seat is stowed or
secured in the retracted position,
and
b) Passenger seat assigned to flight
attendant is placarded “FOR
FLIGHT ATTENDANT
ONLY”.
None required.
An Inoperative Placard will
be placed on affected Flight
Attendant Seat and will be
noted on ADLS.
Maintenance will ensure:
a) Folding type seat is stowed or
secured in the retracted position,
and
b) Passenger seat assigned to flight
attendant is placarded “FOR
FLIGHT ATTENDANT
ONLY”.
Flight crew will ensure:
a) Affected seat is not
occupied, and
b) Flight attendant displaced
by inoperative seat occupies
the passenger seat most
accessible to the inoperative
seat.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE 1: An automatic folding seat that
will not stow automatically is considered
inoperative.
NOTE 2: A seat position with an
inoperative or missing restraint system is
considered inoperative.
For Operators Other
Than Holders of an
Air Carrier or
Commercial
Operator Certificate
(continued)
D
1
0
(M)(O) May be inoperative provided:
a) Affected seat is not occupied,
b) Flight Attendant displaced by
inoperative seat occupies the
passenger seat most accessible to
the inoperative seat,
c) Folding type seat is stowed or
secured in the retracted position,
and
d) Passenger seat assigned to flight
attendant is placarded “FOR
FLIGHT ATTENDANT ONLY”.
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 25-12
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
For Operators Other
Than Holders of an
Air Carrier or
Commercial
Operator Certificate
(continued)
NOTE 1: An automatic folding seat that
will not stow automatically is considered
inoperative.
NOTE 2: A seat position with an
inoperative or missing restraint system is
considered inoperative.
NOTE 3: If one side of a dual seat
assembly is inoperative and a flight
attendant is displaced to the adjacent seat,
the adjacent seat must be operative.
11.
Galley/Cabin Waste
Receptacles Access
Doors/Covers
C
-
-
(M)(O) May be inoperative provided:
a) The container is empty and the
access is secured to prevent waste
introduction into the compartment,
and
b) Procedures are established to ensure
that sufficient galley/cabin waste
receptacles are available to
accommodate all waste that may be
generated on a flight.
Maintenance will ensure container is
empty and the access is secured to
prevent waste introduction into the
compartment.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will ensure
procedures are established to
ensure that sufficient galley /
cabin waste receptacles (trash
bags are considered receptacles)
are available to accommodate
all waste that may be generated.
An Inoperative Placard will
be placed on affected Galley /
Cabin Waste Receptacles
Access Doors/Covers and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 25-13
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
12. Exterior Lavatory
*** Door Ashtrays
1)
Airplanes with
multiple exterior
lavatory door
ashtray installed
A
-
-
Up to and including 50 percent may be
missing or inoperative for 10 days.
None required.
None required.
An Inoperative Placard will
be placed on affected Exterior
Lavatory Door Ashtray and
will be noted on ADLS.
A
-
-
More than 50 percent may be missing or
inoperative for 3 days.
None required.
None required.
An Inoperative Placard will
be placed on affected Exterior
Lavatory Door Ashtray and
will be noted on ADLS.
None required.
None required.
An Inoperative Placard will
be placed on affected Exterior
Lavatory Door Ashtray and
will be noted on ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Crew lavatories are included in
total aircraft exterior lavatory door ashtray
count.
2)
Airplanes with
only one exterior
lavatory door
ashtray installed
A
1
-
13. External Camera
*** System
D
1
0
14. Emergency Vision
*** Assurance System
(EVAS) STC No.
SA00892LA
D
-
0
May be missing or inoperative for 10
days.
May be inoperative.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
15.
PAGE NUMBER: 25-14
MMEL REV. NO.: 8
Pilot Seat(s)
1)
Vertical
Adjustment
C
-
-
(M) May be inoperative provided:
a) Seat is secured at the individual
crewmember’s requirements, and
b) Fore-aft adjustment is operative.
Maintenance will secure seat as
required by proviso a) and ensure
that seat is able to move full fore and
aft on its track.
None required.
An Inoperative Placard will
be placed on vertical
adjustment handle and will be
noted on ADLS.
2)
Armrest
C
-
-
(M) May be inoperative provided:
a) Affected armrest is in the upright
position or removed, and
b) Seat is acceptable to the affected
crewmember.
Maintenance will ensure armrest is in None required.
the up position or removed.
An Inoperative Placard will
be placed on affected arm rest
and will be noted on ADLS.
3)
Recline
Adjustment
C
-
-
(M) May be inoperative provided:
a) Seat is secured at a position
acceptable to the affected
crewmember, and
b) Seat is able to move full Fore-Aft
on its track.
Maintenance will secure seat as
required by proviso a) and ensure
that seat is able to move full fore and
aft on its track.
None required.
An Inoperative Placard will
be placed on recline
adjustment handle and will be
noted on ADLS.
4)
Lumbar Support
C
-
-
May be inoperative provided seat is
acceptable to the affected crewmember.
None required.
None required.
An Inoperative Placard will
be placed on the pilot’s seat
adjustment to lumbar support
area and will be noted on
ADLS.
5)
Thigh Support
C
-
-
May be inoperative provided seat is
acceptable to the affected crewmember.
None required.
None required.
An Inoperative Placard will
be placed on the pilot’s seat
adjustment to thigh support
area and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
16.
Rudder Pedal
Adjustment
17.
Cockpit Convenience
Items (Expired on
April 30, 2008)
18.
Keyed Locks
D
-
0
19.
Airplane Ladders
C
-
0
1)
D
-
0
Ladder Hardware
(Pit Pins,
Lanyards, etc.)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
C
PAGE NUMBER: 25-15
MMEL REV. NO.: 8
2
0
(M) May be inoperative provided:
a) Adjustments can be secured in a
position that suits individual
pilot(s), and
b) Position of pedal(s) permits normal
full flight control movement.
Maintenance will ensure adjustments
can be secured in a position that suits
individual pilot(s) requirements and
position of pedal(s) permits normal
full flight control movement. Flight
crew may perform (M) procedures if
maintenance is not available.
None required.
An Inoperative Placard will
be on the rudder pedal
adjustment handle and will be
noted on ADLS.
May be inoperative provided the
associated access panel, door,
compartment, or cap is verified secure
before each departure.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(O) May be inoperative or removed.
None required.
Flight crew will ensure
An Inoperative Placard will
inoperative ladder is secured or be displayed in a prominent
removed prior to each departure. position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
Deleted in Rev. 7
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 25-16
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
20. Baggage Compartment
*** Shelves
***
1)
Shelf Stowage
Straps
D
-
0
May be inoperative or removed provided
the shelves remain in the down position.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
2)
Shelf Support
Straps
D
-
0
May be inoperative or removed provided
the shelves remain in the stowed (up)
position and are not used.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
21.
Crewmember
Flashlight Holder
Assemblies (including
Flashlight)
C
-
0
May be inoperative or missing provided
None required.
crewmember has a flashlight of equivalent
characteristics readily available.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
***
1)
Passenger
Convenience
Itmes
(Expired on
April 30, 2008)
***
2)
Non-Essential
D
Equipment and
Furnishings (NEF)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
Non-Essential
Equipment
& Furnishings NEF
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
22.
PAGE NUMBER: 25-17
MMEL REV. NO.: 8
Deleted in Rev. 7
-
0
May be inoperative, damaged or missing
provided item(s) is deferred in accordance
with operator’s NEF deferral program.
The NEF program, procedures and
processes are outlined in the operator’s
(insert name) Manual. (M) and (O)
procedures, if required, must be available
to flight crew and included in appropriate
operator’s document.
NOTE: Exterior lavatory door ash trays
are not considered NEF items.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
24.
***
Emergency Medical
Kit (EMK) and/or
Associated Equipment
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
Automatic External
Defibrillator (AED)
and/or Associated
Equipment
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
23.
***
PAGE NUMBER: 25-18
MMEL REV. NO.: 8
A
-
0
(O) May be incomplete, missing or
inoperative provided:
a) AED is resealed in a manner that
will identify it as a unit that cannot
be mistaken for a fully serviceable
unit, and
b) Repairs are made within 1 flight.
None required.
Flight crew will ensure AED
unit is placarded “DO NOT
USE THIS UNIT. SOME
REQUIRED ITEMS MAY BE
MISSING.”, and repairs are
made within 1 flight.
An Inoperative Placard will
be will be placed on
Automatic External
Defibrillator and/or
Associated Equipment and
will be noted on ADLS.
D
-
-
Any in excess of those required by 14
CFR may be incomplete, missing, or
inoperative.
None required.
None required.
An Inoperative Placard will
be will be placed on
Automatic External
Defibrillator and/or
Associated Equipment and
will be noted on ADLS.
A
-
0
(O) May be incomplete, missing or
inoperative provided:
a) EMK is resealed in a manner that
will identify it as a unit that cannot
be mistaken for a fully serviceable
unit, and
b) Repairs or replacements are made
within 1 flight.
None required.
Flight crew will ensure EMK
unit is placarded “DO NOT
USE THIS UNIT. SOME
REQUIRED ITEMS MAY BE
MISSING.”, and repairs are
made within 1 flight.
An Inoperative Placard will
be will be placed on
Emergency Medical Kit
(EMK) and/or Associated
Equipment and will be noted
on ADLS.
D
-
-
Any in excess of those required by 14
CFR may be incomplete missing, or
inoperative.
None required.
None required.
An Inoperative Placard will
be will be placed on
Emergency Medical Kit
(EMK) and/or Associated
Equipment and will be noted
on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
First Aid Kit (FAK)
and/or Associated
Equipment
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
25.
PAGE NUMBER: 25-19
MMEL REV. NO.: 8
A
-
-
(O) If more than one is required by 14
None required.
CFR, only one of the required first aid kits
may be incomplete, missing or inoperative
provided:
a) FAK is resealed in a manner that
will identify it as a unit that cannot
be mistaken for a fully serviceable
unit, and
b) Repairs or replacements are made
within three (3) flight cycles.
D
-
-
Any in excess of those required by 14
CFR may be incomplete, missing or
inoperative.
None required.
Flight crew will ensure FAK
unit is placarded “DO NOT
USE THIS UNIT. SOME
REQUIRED ITEMS MAY BE
MISSING.”, and repairs are
made within three (3) flight
cycles.
An Inoperative Placard will
be will be placed on First Aid
Kit and/or Associated
Equipment and will be noted
on ADLS.
None required.
An Inoperative Placard will
be will be placed on First Aid
Kit and/or Associated
Equipment and will be noted
on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
26. FIRE PROTECTION
Portable Fire
Extinguishers
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 26-1
MMEL REV. NO.: 8
D
-
-
Any in excess of those required by 14
None required.
CFR may be inoperative or missing
provided:
a) Inoperative fire extinguisher is
tagged inoperative, removed from
the installed location, and placed
out of sight so it cannot be mistaken
for a functional unit, and
b) Required distribution is maintained.
None required.
If installed, an Inoperative
Placard will be placed on
Pressure Charge Gauge of
affected extinguisher and will
be noted on ADLS.
None required.
An Inoperative Placard will
be placed adjacent to affected
Wing Anti-Ice Switch and
will be noted on ADLS.
NOTE: Flight crew will ensure operative
fire extinguishers are available to meet 14
CFR 91.513 or 135.155 distribution
requirements, i.e., one near cockpit, one in
cabin, are required for dispatch.
2.
Wing Overheat
Warning Systems
C
2
0
Except for ER operations, may be
inoperative provided:
a) Wing Anti-ice is not used, and
b) Airplane is not operated in known
or forecast icing conditions.
None required.
3.
APU Fire Detection
System
C
1
0
(M) Except for ER operations, may be
inoperative provided:
a) APU is not used, and
b) APU CONT #1 and APU CONT #2
circuit breakers are pulled and
collared.
Maintenance will ensure APU CONT None required.
#1 and APU CONT #2 circuit
breakers are pulled and collared.
Flight crew may accomplish this task
if properly qualified and authorized.
An Inoperative Placard will
be placed on APU
"MASTER" Switch and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
26. FIRE PROTECTION
Rear Baggage
Compartment Smoke
Detector Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
4.
PAGE NUMBER: 26-2
MMEL REV. NO.: 8
C
-
0
May be inoperative provided:
a) Internal baggage door remains
OPEN, and
b) Airplane is operated at or below FL
400.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
May be inoperative provided:
a) Rear baggage compartment is not
used,
b) Internal baggage door remains
CLOSED,
c) Flight crew investigates baggage
compartment for possible fire in the
event the "BAG EER HOT"
message displays, and
d) Airplane is operated in accord-ance
with AFM Limitations.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
26. FIRE PROTECTION
5. Lavatory Smoke
*** Detection Systems
PAGE NUMBER: 26-3
MMEL REV. NO.: 8
C
-
-
(M)(O) For each lavatory, the lavatory
smoke detection system may be
inoperative provided:
a) Lavatory waste receptacle is empty,
b) Associated lavatory door is
LOCKED, CLOSED and placarded,
"INOPERATIVE - DO NOT
ENTER", and
c) Lavatory is used only by
crewmembers.
NOTE 1: These provisos are not intended
to prohibit lavatory use or inspections by
crewmembers.
NOTE 2: Lavatory Smoke Detection
System is not required for all-cargo
operations.
Maintenance will ensure Lavatory
Smoke Detector CB is pulled and
collared.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will inspect lavatory
to ensure Lavatory Waste
Receptacle is empty and
Lavatory Door is LOCKED
CLOSED. In addition, flight
crew will ensure Lavatory is
NOT used for any purpose.
An Inoperative Placard will
be placed on Lavatory Door
stating "Inoperative - Do Not
Enter" and will be noted on
ADLS.
NOTE: These provisos are
not intended to prohibit
lavatory use or inspections by
crewmembers. In addition,
Lavatory Smoke Detection
System is not required for all
cargo operations.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
26. FIRE PROTECTION
6. Lavatory Fire
*** Extinguisher Systems
PAGE NUMBER: 26-4
MMEL REV. NO.: 8
C
-
-
For each lavatory, the lavatory fire
extinguisher system may be inoperative
provided Lavatory Smoke Detector
system is operative.
None required.
None required.
An Inoperative Placard will
be placed on the Lavatory
Fire Extinguisher and will be
noted on ADLS.
C
-
-
(M)(O) For each lavatory, the lavatory fire
extinguisher system may be inoperative
provided:
a) Lavatory waste receptacle is empty,
b) Associated lavatory door is
LOCKED, CLOSED and placarded,
"INOPERATIVE - DO NOT
ENTER", and
c) Lavatory is used only by
crewmembers.
Maintenance will verify Lavatory
Waste Receptacle is empty.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will inspect lavatory
to ensure Lavatory Waste
Receptacle is empty and
Lavatory Door is LOCKED
CLOSED. In addition, flight
crew will ensure Lavatory is
NOT used for any purpose.
An Inoperative Placard will
be placed on Lavatory Door
stating "Inoperative Do Not
Enter" and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed on Galley Smoke
Detector and will be noted on
ADLS.
NOTE 1: These provisos are not intended
to prohibit lavatory use or inspections by
crewmembers.
NOTE 2: A Lavatory Fire Extinguisher
System is not required for all-cargo
operations.
7. Galley Smoke
*** Detection Systems
D
-
0
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
8. Galley Fire
*** Extinguishing Systems
D
-
0
9.
C
2
1
10. Flame Detectors
***
D
-
11.
C
D
12. Passenger
*** Compartment
Closet Smoke
Detectors
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
26. FIRE PROTECTION
Electronic Equipment
Rack Overheat
Warning System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
Engine Fire
Detection Systems
PAGE NUMBER: 26-5
MMEL REV. NO.: 8
None required.
None required.
An Inoperative Placard will
be placed on Galley Fire
Extinguisher and will be
noted on ADLS.
None required.
None required.
An Inoperative Placard is
placed next to either A or B
Switch/Light and will be
noted on ADLS.
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
-
0
May be inoperative provided door remains None required.
OPEN for visual check from crew
stations.
None required.
An Inoperative Placard will
be placed on Passenger
Compartment Closet Smoke
Detectors and will be noted
on ADLS.
Except for ER operations, one complete
loop (A or B) may be inoperative
provided the Fault Switch/ Light is
pressed to isolate the faulty loop and
illuminate the OFF portion of the switch
light.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 26-6
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
26. FIRE PROTECTION
13. Entranceway Baggage
*** Compartment Smoke
Detectors
D
-
-
May be inoperative provided door remains None required.
OPEN for visual check from crew
stations.
None required.
An Inoperative Placard will
be placed on Entranceway
Baggage Compartment
Smoke Detectors and will be
noted on ADLS.
14. Cargo Compartment
*** Fire Detection /
Suppression Systems
C
-
0
(O) May be inoperative provided
procedures are established and used to
ensure the associated cargo compartment
remains empty, or is verified to contain
only empty cargo handling equipment,
ballast (ballst may be loaded in ULDs)
and/or fly away kits.
Flight crew will verify that
cargo compartment remains
empty, or is verified to contain
only empty cargo handling
equipment, ballast, and/or fly
away kits.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE 1: Operators MELs should define
which items are approved for inclusion in
the fly away kits, and which materials can
be used as ballast. (Does not preclude the
Carriage of empty cargo containers,
pallets, ballast, etc.)
NOTE 2: Class E cargo compartments
require only the installation of smoke or
fire detection systems (not suppression).
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
26. FIRE PROTECTION
15. APU Fire Bottle
***
PAGE NUMBER: 26-7
MMEL REV. NO.: 8
C
1
0
(M)(O) Except for ER operations, may be
inoperative provided:
a) APU is considered inoperative,
b) Both engine driven generators are
operative,
c) Standby electrical system is
operative, and
d) APU CONT #1 and APU CONT #2
circuit breakers are pulled and
collared.
Maintenance will pull and collar
APU CONT #1 and APU CONT #2
circuit breakers.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will ensure:
a) Maintenance procedures
are accomplished if
maintenance personnel are
not available. AFM
Normal Procedures.
b) Both Engine Generators
are operative.
c) Standby Electrical Power
System is operative. AFM
Emergency Procedures.
An Inoperative Placard will
be placed on APU Fire Bottle
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 27-1
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
27. FLIGHT CONTROLS
1.
Rudder Limit
Indication System
C
1
0
May be inoperative provided Single
Rudder Indication System is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2.
Single Rudder
Indication System
C
1
0
May be inoperative provided Rudder
Limit Indication System is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3.
Automatic Ground
Spoiler System
C
1
0
(O) May be inoperative provided airplane
is operated in accordance with AFM
Limitations.
None required.
Flight crew will ensure airplane
is operated in accordance with
AFM, Section 1, Limitations,
and Automatic Ground
Spoilers. (Ground Spoiler may
be inoperative for takeoff
provided Anti-Skid is operative
and 20 degrees flaps are used
for takeoff and cowl/wing antiice isn’t used for takeoff.)
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4.
Electric Elevator Trim
System
C
1
0
(O) May be inoperative provided:
a) Electric Elevator Trim remains
OFF,
b) Both Flap/Stabilizer Control
Channels are operative, and
c) Airplane is operated in accordance
with AFM Limitations.
None required.
Flight crew will ensure
Electric Pitch Trim remains
"OFF", both Flap/ Stabilizer
Control Channels are operative
(no messages on CAS), and
airplane is operated in
accordance with AFM, Section
1, Limitations, Airspeed
Limitations. (Maximum
Operating Limit Speed is 0.80
Mt.)
An Inoperative Placard will
be placed next to Pitch Trim
Switch and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 27-2
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
27. FLIGHT CONTROLS
5.
Control Wheel Elevator C
Trim Switches
2
1
(O) May be inoperative provided pilot
flying has operative switch.
None required.
In the event that the operative
Elevator Trim Switch fails after
dispatch, the crew shall comply
with the Jammed Stabilizer
procedure in Section 3 –
Abnormal Procedures of the
applicable AFM. Maximum
flap selection is 20 degrees
during the approach and
landing.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
6.
Flap/Stabilizer
Control Channels
B
2
1
Channel may be inoperative provided:
a) Electric Pitch Trim System is
operative, and
b) Alternate control is verified
operative before each departure.
None required
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7.
Single Speed Brake
Indication System
C
1
0
May be inoperative provided Single
Rudder Indication System is operative.
None required.
None required
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
2
0
(M)(O) May be inoperative provided
affected circuit breaker(s) are pulled and
collared.
Maintenance will ensure affected
circuit breaker(s) are pulled and
collared.
Flight crew will ensure
maintenance procedures are
accomplished if maintenance
personnel are not available.
An Inoperative Placard will
be placed next to Elevator
Trim Actuator Switch and
will be noted on ADLS.
8. Elevator Trim
*** Actuator Heater
Systems
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
Autopilot Elevator
Servos
(GV-SP, GIV-X)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
C
1
0
(M)(O) May be inoperative provided
affected circuit breaker(s) are pulled and
collared.
Maintenance will ensure affected
circuit breaker(s) are pulled and
collared.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will ensure
maintenance procedures are
accomplished if maintenance
personnel are not available.
An Inoperative Placard will
be placed next to Aileron
Trim Wheel and will be noted
on ADLS.
C
2
1
(M) May be inoperative provided the
inoperative servo circuit breaker(s) is
pulled and collared.
Maintenance will ensure inoperative
servo circuit breaker(s) is pulled and
collared.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
11.
Autopilot Pitch Trim
Servos
(GV-SP, GIV-X)
C
2
1
(M) May be inoperative provided the
inoperative servo circuit breaker(s) is
pulled and collared.
Maintenance will ensure inoperative
servo circuit breaker(s) is pulled and
collared.
Flight crew may accomplish this task
if properly qualified and authorized.
12.
Autopilot Aileron
Servos
(GV-SP, GIV-X)
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
27. FLIGHT CONTROLS
10.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
9. Aileron Trim
*** Actuator Heater
PAGE NUMBER: 27-3
MMEL REV. NO.: 8
C
2
1
(M) May be inoperative provided the
inoperative servo circuit breaker(s) is
pulled and collared.
Maintenance will ensure inoperative
servo circuit breaker(s) is pulled and
collared.
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
C
2
1
(M) May be inoperative provided the
inoperative servo circuit breaker(s) is
pulled and collared.
Maintenance will ensure inoperative
servo circuit breaker(s) is pulled and
collared.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Prior to dispatch, the flight crew
will discuss the dispatch
situation with the stall barrier
inoperative and crew procedures
in the event the remaining
operative stall barrier fails. If
the remaining stall barrier fails,
the minimum speed shall be no
less than Vref (1.3 Vs) for all
phases of flight. This minimum
speed shall be cross-referenced
to Normalized Angle of Attack
to 0.59 as displayed on the PFD.
Weather conditions at the
departure and destination
airports shall be considered. If
there are known or forecast
windshear at the departure of
destination airport, the crew
shall consider delaying the
takeoff or approach and landing
until such conditions cease to
exist or consider deviation to an
alternate airport in the approach
and landing case.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
14.
Stall Barrier
Systems
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
27. FLIGHT CONTROLS
Autopilot Yaw Damper
Servos
(GV-SP, GIV-X)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 27-4
MMEL REV. NO.: 8
A
2
1
(M)(O) May be inoperative provided:
a) Angle of Attack indication is
available on both PFD’s,
b) Alternate procedures are established
and used,
c) The inoperative stall barrier system
is electrically disabled, and
d) Repairs are made within two (2)
flight days.
Maintenance will pull and collar the
circuit breakers for the Stall Barrier
Valve and Stick Shaker associated
with the failed system.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
27. FLIGHT CONTROLS
16.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
15.
PAGE NUMBER: 27-5
MMEL REV. NO.: 8
Flight Control Synoptic
Display (GV)
C
1
0
May be inoperative provided the affected
control surface is visually checked for
full, free and correct movement prior to
each flight.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(GV-SP, GIV-X)
C
-
0
May be inoperative provided the affected
control surface is visually checked for
full, free and correct movement prior to
each flight.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Gust Lock
C
1
0
(O) May be inoperative provided flight
controls are secured in an alternate
manner.
None required.
Flight crew will ensure affected
surfaces by using rope or some
other means to secure the rudder
pedals and control yoke from
moving between flights. Refer
to GAC-OIS-14.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
(O) May be inoperative provided airplane
is parked in sheltered area unaffected by
atmospheric conditions.
None required.
Flight crew will park the
airplane in a sheltered area
(hangar) or determine via
weather forecast that the rudder,
elevator and ailerons won’t be
exposed to windy conditions.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
28. FUEL
2.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 28-1
MMEL REV. NO.: 8
Fuel Tank
Temperature Systems
(GV, GV-SP)
C
2
0
(O) May be inoperative provided:
a) Total Air Temperature is used as an
indication of fuel temperature, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
Flight crew will ensure Total
Air Temperature (TAT) is used
as indication of fuel temperature
and airplane is operated in
accordance with AFM, Section
1, Limitations, Powerplant
EICAS Indications.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Fuel Tank
Temperature System
(GIV-X)
C
1
0
(O) May be inoperative provided:
a) Total Air Temperature is used as an
indication of fuel temperature, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
Flight crew will ensure Total
Air Temperature (TAT) is used
as indication of fuel temperature
and airplane is operated in
accordance with AFM, Section
1, Limitations, Powerplant
EICAS Indications.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
EICAS or Standby
RFMU (GV) / MCDU
(GV-SP, GIV-X) Fuel
Quantity Indicating
Systems
C
2
1
(M)(O) May be inoperative provided
associated Standby Fuel Quantity
Indicating System or EICAS Fuel
Quantity Indicating System is operative.
Maintenance will ensure tanks are
filled using Standby Fuel Quantity
Indicating System or EICAS Fuel
Quantity Indicating System.
Flight crew will ensure
associated Standby Fuel
Quantity Indicating System or
EICAS Fuel Quantity Indicating
System is operative.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
28. FUEL
EICAS or Standby
RFMU (GV) / MCDU
(GV-SP, GIV-X) Fuel
Quantity Indicating
Systems (continued)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
2.
PAGE NUMBER: 28-2
MMEL REV. NO.: 8
C
C
2
2
1
1
(M)(O) Except for ER operations, either
Left or Right Fuel Quantity display may
be inoperative provided:
a) Both tanks are completely filled
using overwing refueling,
b) Both fuel flow meters are operative,
c) After takeoff, power is set by
matching fuel flow indications on
both engines, and
d) Flight crew maintains a log of fuel
burned.
Maintenance will ensure BOTH
tanks are completely filled using
overwing method of refueling.
NOTE: Do not pull Fuel Qty circuit
breaker as this disables Fuel Level
Low caution message.
(M)(O) Except for ER operations, either
Left or Right Fuel Quantity display may
be inoperative provided:
a) Affected tank is defueled before
each refueling,
b) Affected tank is fueled with a
known quantity of fuel,
c) Both fuel flow meters are operative,
d) After takeoff, power is set by
matching fuel flow indications on
both engines, and
e) Flight crew maintains a log of fuel
burned.
Maintenance will Defuel affected
tank before each refueling and refuel
it with Known quantity of fuel.
NOTE: Total fuel indication will be
invalid with an inoperative indicator.
Flight crew will ensure:
a) Both Fuel Flow Indicating
Systems are operative.
b) After takeoff, power is set
by matching Fuel Flow
indications on both
engines.
c) A log of fuel burned is
maintained.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Total Fuel indication
will be INVALID with
inoperative indicator.
Flight crew will ensure:
a) Both fuel flow meters are
operative,
b) After takeoff, power is set
by matching fuel flow
indications on both
engines, and
c) A log of fuel burned is
maintained.
NOTE: Total fuel indication
will be INVALID with
inoperative indicator.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 28-3
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
28. FUEL
3.
Fuel Low Quantity
Warning Systems
C
2
0
(O) May be inoperative provided:
a) Both Fuel Quantity Indicating
Systems are operative,
b) All Fuel Boost Pumps are
operative, and
c) Fuel Crossflow Valve is OPENED
when either wing tank contains
2,000 pounds or less fuel.
None required.
Flight crew will ensure:
a) BOTH Fuel Quantity
Indicating Systems and all
Fuel Boost Pumps are
operative. (AFM, Section
2, Normal Procedures,
Before Starting Engines,
Normal Engine Ground
Start and After Starting
Engines)
b) Fuel Crossflow Valve is
OPENED when either
wing tank contains 2,000
pounds or less fuel.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4.
Fuel Boost Pumps
C
4
3
(O) Except for ER operations, may be
inoperative provided:
a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning
Systems are operative, and
d) Airplane is operated in accordance
with AFM Limitations.
None required.
Flight crew will ensure:
a) Fuel Crossflow Valve and
Intertank Valve are
operative. AFM, Section 2,
Normal Procedures, Before
Starting Engines.
b) BOTH Fuel Low Quantity
Warning Systems are
operative. AFM, Section 2,
Normal Procedures, Before
Starting Engines.
c) Verify compliance with
AFM, Section 3, Abnormal
Procedures, Fuel Boost
Pump Failure.
An Inoperative Placard will
be placed on Affected Fuel
Boost Pump "ON/OFF"
Switch and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
28. FUEL
Fuel Intertank
Valve
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5.
PAGE NUMBER: 28-4
MMEL REV. NO.: 8
C
1
0
(M) Except for ER operations, may be
inoperative provided:
a) All Fuel Boost Pumps are
operative,
b) Fuel Crossflow Valve is operative,
c) Fuel Quantity Indicating System is
operative, and
d) Intertank Valve is verified
CLOSED and electrically
deactivated.
Maintenance will deactivate the
intertank valve by pulling and
collaring appropriate Fuel Intertank
circuit breaker.
None required.
An Inoperative Placard will
be placed on Fuel Intertank
Valve Switch and will be
noted on ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
NOTE: With Fuel Intertank Valve
CLOSED and fuel temperature below 0
degrees C, fuel balancing capabilities may
be affected.
6.
Heated Fuel Return
System (HFRS)
(GV, GV-SP)
C
2
0
May be inoperative provided:
a) Flight crew monitors fuel tank
temperature, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7.
Fuel Boost Pump
Warning Systems
C
4
3
(O) Except for ER operations, may be
inoperative provided:
a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
and
c) Airplane is operated in accordance
with AFM Limitations.
None required.
The flight crew will ensure the
Fuel Crossflow Valve and Fuel
Intertank is operative; AFM,
Section 2, Normal Procedures,
Before Starting Engines and
Fuel Synoptic and that AFM,
Section 3, Abnormal
Procedures, Fuel Boost Pump
Failure are complied with.
An Inoperative Placard will
be placed on affected Boost
Pump Warning Annunciator
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
1)
Failed CLOSED
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
28. FUEL
Fuel Crossflow Valve
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
PAGE NUMBER: 28-5
MMEL REV. NO.: 8
C
1
0
(O) Except for ER operations, may be
None required.
inoperative provided:
a) All Fuel Boost Pumps are
operative,
b) Fuel Intertank Valve is operative,
c) Fuel Quantity Indicating System is
operative,
d) Fuel Intertank Valve is OPEN when
either wing tank contains 2,000
pounds or less fuel, and
e) Airplane is operated in accordance
with AFM Limitations.
Flight crew will comply with
provisos a), b) and c) using
AFM Section 2, Normal
Procedures and Fuel Synoptic.
Flight crew will OPEN Fuel
Intertank Valve when either
wing tank contains 2000 lb or
less fuel. Airplane is operated in
accordance with AFM, Section
1, Limitations, Fuel Balance
(1000 lb takeoff, 2000 lb
enroute).
An Inoperative Placard will
be placed on Fuel Crossflow
Valve Switch and will be
noted on ADLS.
Flight crew will use Normal
Procedures and Fuel Synoptic to
ensure:
a) All Fuel Boost Pumps are
operative,
b) Fuel Intertank Valve is
operative,
c) Fuel Quantity Indicating
System is operative.
d) Fuel tank temperature
system is operative.
An Inoperative Placard will
be placed on Fuel Crossflow
Valve Switch and will be
noted on ADLS.
NOTE: Avoid uncoordinated maneuvers
when Fuel Intertank Valve is OPEN.
2)
Failed OPEN
C
1
0
(O) Except for ER operations, may be
inoperative provided:
a) All Fuel Boost Pumps are
operative,
b) Fuel Intertank Valve is operative,
c) Fuel Quantity Indicating System is
operative,
d) Airplane is operated in accordance
with AFM Limitations, and
e) Fuel tank temperature system must
be operative.
NOTE: Avoid uncoordinated maneuvers
when Fuel Intertank Valve is OPEN.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 28-6
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
28. FUEL
9.
Pressure Fueling
System (Single
Point Refueling)
D
1
0
10.
Ground Service
Control Panel
D
1
11.
Automatic Fueling
System
D
12.
Fuel Cap Chains
D
(M) May be inoperative provided
procedures are established to deactivate
Pressure Fueling System.
Maintenance will ensure Pressure
Fueling System is deactivated by
Manually Closing Fuel Precheck
Valves and pulling and collaring
appropriate (Left or Right) Fueling
Shutoff Valve CB. Refer to AMM,
Chapter 28-22-00. Flight crew may
perform maintenance function if
maintenance is unavailable.
Flight crew may accomplish this task
if properly qualified and authorized.
None required.
An Inoperative Placard will
be placed on Pressure
Refueling Port and between
Left and Right Remote
Fueling Shutoff Switches and
will be noted on ADLS.
0
None required.
None required.
An Inoperative Placard will
be placed on Ground Service
Control Panel and will be
noted on ADLS.
1
0
None required.
None required.
An Inoperative Placard will
be placed on Automatic
Fueling System and will be
noted on ADLS.
-
0
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
14. Mid Wing Ejector
*** (MWE) System
(GV, GV-SP only)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
28. FUEL
Single Point Refueling
Cap
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 28-7
MMEL REV. NO.: 8
C
1
0
May be inoperative or missing provided
the single point refueling receptacle is
checked for leaks before every takeoff.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
2
0
(O) May be inoperative provided the
maximum fuel load for dispatch is limited
to 9,000 lb per tank for a total fuel load of
18,000 lb.
None required.
The flight crew shall ensure that
the maximum fuel load is equil
to or less than 9,000 lb per tnak
for a maximum total of 18,000
lb.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 29-1
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
29. HYDRAULIC POWER
1.
Brake Accumulator
Pressure Gauge
(Nose Wheelwell)
D
1
0
None required.
None required.
An Inoperative Placard will
be placed on face of
Accumulator Pressure
Indicator and will be noted on
ADLS.
2.
Auxiliary Hydraulic
Pump Pressure
Indicator
C
1
0
May be inoperative provided cockpit
Brake Accumulator Pressure Gauge is
operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3.
Power Transfer Unit
(PTU) Hydraulic
Pressure Indication
C
1
0
(O) May be inoperative provided:
a) Left Hydraulic Pressure Indication
is operative,
b) PTU Hydraulic system is operative,
and
c) Prior to left engine start, HMG
operational check is performed.
None required.
Flight crew will ensure
Hydraulic Pressure Indication is
operative and Power Transfer
Unit operation is verified by
performing successful flap
operational test with only right
engine running.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4.
PTU Hydraulic Pump
(Auto Mode)
C
1
0
May be inoperative provided manual
mode is verified to be operative before
every flight.
None required.
None required.
5.
Auxiliary Hydraulic
Pump (Auto Mode)
C
1
0
May be inoperative provided the
Auxiliary pump is selected ON for takeoff
and landing.
None required.
None required.
An Inoperative Placard will
be placed on Power Transfer
NOTE: With right engine
Unit Arm Switch and will be
running, select PTU ON. Verify noted on ADLS.
PTU pressure is present (3000
psi +300/-400).
An Inoperative Placard will
be placed on Auxiliary
Hydraulic Pump Arm Switch
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 29-2
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
29. HYDRAULIC POWER
6.
Left Hydraulic System
Quantity Gauge
(Ground Service
Control Panel Aft Equipment Area)
D
1
0
(O) May be inoperative provided quantity
is checked by reservoir indicator or using
hydraulic quantity indication on hydraulic
synoptic before each departure.
None required.
Flight crew will verify the
hydraulic quantity at the
reservoir or on hydraulic
synoptic prior to each departure.
Refer to AMM Chapter 12-1500.
An Inoperative Placard will
be placed on Ground Service
Control Panel and will be
noted on ADLS.
7.
Right Hydraulic
System
Quantity Gauge
(Ground Service
Control Panel Aft Equipment Area)
D
1
0
(O) May be inoperative provided quantity
is checked by reservoir indicator or using
hydraulic quantity indication on hydraulic
synoptic before each departure.
None required.
Flight crew will verify the
hydraulic quantity at the
reservoir or on hydraulic
synoptic prior to each departure.
Refer to AMM Chapter 12-1500.
An Inoperative Placard will
be placed on Ground Service
Control Panel and will be
noted on ADLS.
8.
Left Hydraulic System
Quantity Indication
(EICAS)
C
1
0
May be inoperative provided quantity is
checked by reservoir indicator or Ground
Service Control Panel Left Hydraulic
Quantity gauges before each departure.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
9.
Right Hydraulic
System
Quantity Indication
(EICAS)
C
1
0
May be inoperative provided quantity is
checked by reservoir indicator or Ground
Service Control Panel Right Hydraulic
Quantity gauges before each departure.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
29. HYDRAULIC POWER
Hydraulic Reservoir
Temperature Sensors
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
10.
PAGE NUMBER: 29-3
MMEL REV. NO.: 8
C
2
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Accuracy of hydraulic quantity
indication will be degraded during long
flights in cold soak conditions. If Right
Hydraulic System (R SYS) sensor has
failed in flight, there is no protection
against overheating R SYS pumps during
Power Transfer Unit (PTU) operation.
In flight, with either or both sensors
failed, there is no warning of hot hydraulic
system temperatures.
11.
Hydraulic Reservoir
Replenishing System
D
1
0
(M) May be inoperative provided
hydraulic reservoirs are replenished as
needed using approved servicing
techniques.
Airplane may continue in service
provided maintenance personnel
replenish hydraulic reservoirs as
needed using approved servicing
techniques. Refer to AMM Chapter
12-15-00.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
12.
Brake Accumulator
Pressure Gauge
(cockpit dial)
C
1
0
May be inoperative provided the Brake
Synoptic Page Accumulator Pressure
indication is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
May be inoperative provided:
a) Brake accumulator gauge in the
nose wheelwell is operative and
checked before each takeoff, and
b) Auxiliary hydraulic pump is on and
running for every takeoff and
landing.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
29. HYDRAULIC POWER
Brake Synoptic Page
Accumulator Pressure
Indication
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 29-4
MMEL REV. NO.: 8
C
1
0
May be inoperative provided the Brake
Accumulator Pressure Gauge (cockpit
dial) is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
May be inoperative provided:
a) Brake accumulator gauge in the
nose wheelwell is operative and
checked before each takeoff, and
b) Auxiliary hydraulic pump is on and
running for every takeoff and
landing.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
2.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
30. ICE and RAIN PROTECTION
Cowl Anti-Ice
Pressure Indication
Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 30-1
MMEL REV. NO.: 8
B
2
0
Except for ER operations, may be
inoperative provided both EICAS Cowl
Anti-Ice Indications are operative.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
2
0
Except for ER operations, may be
inoperative provided airplane is operated
at greater than +10 deg. C SAT.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
2
0
Except for ER operations, may be
inoperative provided:
a) Airplane is operated in VMC, and
b) Airplane is not operated in visible
moisture.
None required.
None required.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Wing Anti-Ice
Systems
C
2
0
Except for ER operations, may be
inoperative provided airplane is not
operated in known or forecast icing
conditions.
None required.
None required.
An Inoperative Placard will
be placed on affected Wing
Anti-Ice "OFF/AUTO/ ON"
Switch and will be noted on
ADLS.
1) Automatic
Functions
C
2
0
May be inoperative provided airplane is
operated in accordance with AFM
Limitations.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Refer to AFM Section 1-30-10,
1-30-20, and 1-30-30.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
30. ICE and RAIN PROTECTION
4.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 30-2
MMEL REV. NO.: 8
Windshield Heat
Systems
C
2
1
Except for ER operations, may be
inoperative provided airplane is not
operated in known or forecast icing
conditions.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1) Windshield Heat
Sensors
D
4
2
One sensor may be inoperative for each
Windshield Heat System
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Side Window Heat
Systems
C
2
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1)
D
4
2
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
4
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Side Window
Heat Sensors
One Side Window Heat Sensor may be
inoperative for each Side Window Heat
System.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 30-3
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
30. ICE and RAIN PROTECTION
5.
Anti-Ice Heater
Switch Lights
B
4
0
(M)(O) May be inoperative provided all
other elements of the anti-ice heater
indicating system are verified to operate
normally.
Maintenance will check all other
elements of Probe Heat Control
Switch and ensure them to be
functional. Refer to AMM Chapter
30-31-03.
Flight crew will ensure all other
elements of Probe Heat
Indicating Switch are
functioning normally, i.e. when
pitot heat is selected ON,
appropriate EICAS fail message
extinguishes.
An Inoperative Placard will
be placed on Probe Heat
Switch and will be noted on
ADLS.
6.
Pitot Heaters
(GV, GV-SP)
B
4
3
(O) Except for ER operations, may be
inoperative provided airplane is not
operated in visible moisture or known or
forecast icing conditions.
None required.
Flight crew will select MADC
sources that are different and
not associated with failed pitot
heater element.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(GIV-X)
B
3
2
(O) Except for ER operations, may be
inoperative provided airplane is not
operated in visible moisture or known or
forecast icing conditions.
None required.
Flight crew will select MADC
sources that are different and
not associated with failed pitot
heater element.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Ice Detection
Systems
C
2
0
(O) May be inoperative provided airplane
is operated in accordance with alternate
AFM procedures.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7.
NOTE: With both Ice Detection Systems
inoperative, automatic anti-ice is not
available.
Refer to AFM Section 1-30-10,
1-30-20, and 1-30-30. Cowl
Anti-Ice shall be selected ON
manually any time visible
moisture is present and the SAT
is +10°C or less.
Wing Anti-Ice should be
selected ON manually if icing
conditions are imminent or
immediately upon detection of
ice formation on the wings,
winglets or windshield edges.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
C
NUMBER REQ’D FOR DISPATCH
PROCEDURE
2
0
(M) Except for ER operations, may be
inoperative provided:
a) Affected Valve(s) are verified
CLOSED, and
b) Airplane is not operated in known
or forecast icing conditions.
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
PROCEDURE
For G-V, GV-SP (G550, G500)
None required.
aircraft: Maintenance will ensure
affected Cowl Anti-Ice Valve(s)
is/are verified closed IAW RR EMM,
task # 30-21-01-040-801.
For GIV-X (G450, G350):
Maintenance will ensure affected
Cowl Anti-Ice Valve(s) is/are
Deactivated IAW AMM, Chapter 3021-01, paragraph 1.A and 1.B, Cowl
Anti-Ice System – Operational Test
(Static) and follow the steps under
B.(1) thru B.(3).
Flight crew may accomplish this task
if properly qualified and authorized.
(continued)
MMEL DATE: 11/07/2014
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
30. ICE and RAIN PROTECTION
Cowl Anti-Ice
Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
PAGE NUMBER: 30-4
MMEL REV. NO.: 8
An Inoperative Placard will
be placed on or next to
affected Cowl Anti-Ice
Switch indicting valve
position and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
30. ICE and RAIN PROTECTION
8.
PAGE NUMBER: 30-5
MMEL REV. NO.: 8
Cowl Anti-Ice
Systems (continued)
C
2
1
(M) May be inoperative provided:
Maintenance will ensure:
None required.
a) Affected Valves is verified OPEN,
a) BOTH HP Bleed Air Systems
b) All components of both HP Bleed
and BOTH Environmental
Air Systems are operative,
Control System (ECS) Packs are
c) Both Environmental Control
operative.
System (ECS) Packs are operative,
b) Select the affected Cowl Antid) Performance Computer is initialized
Ice switch ON and ensure that
with COWL ANTI-ICE selected
the affected valve circuit
ON for either takeoff or landing
breaker is pulled or in the
when COWL ANTI-ICE valve is
OPEN position. Refer to AMM,
pressurized, and
Chapter 21-21-00, 30-21-00 and
e) Airplane is operated in accordance
36-11-00.
with AFM Limitations and
Flight crew may accomplish this task
Performance.
if properly qualified and authorized.
1) Automatic
Functions
C
2
0
May be inoperative provided airplane is
operated in accordance with alternate
AFM procedures.
None required.
None required.
An Inoperative Placard will
be placed on or next to
affected Cowl Anti-Ice
Switch indicting valve
position and will be noted on
ADLS.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
10. Windshield Blower
*** System
1) Windshield Surface
Seal Protection
Systems
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
30. ICE and RAIN PROTECTION
Cowl Pressure
Differential
Indication System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
9.
PAGE NUMBER: 30-6
MMEL REV. NO.: 8
C
1
0
May be inoperative provided Cowl AntiIce Pressure Indications are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
(M) May be inoperative provided the
Surface Seal coating has been checked to
be servicable in accordance with the
Maintenance Manual within the last 12
months or 500 flight hours whichever
occurs first.
Maintenance will verify that
None required.
effectiveness of windshield coating is
in accordance with AMM within the
last 12 months or 500 flight hours.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
(M) May be inoperative provided the
Surface Seal coating is checked to be
serviceable in accordance with the
Maintenance Manual.
Maintenance will verify that
None required.
effectiveness of windshield coating is
in accordance with AMM.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided there is no
precipitation falling on the departure and
arrival airport at the time of taxi, takeoff
and landing.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
2
0
May be inoperative provided airplane is
not operated in precipitation within 5 NM
of the airport of takeoff or intended
landing.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
30. ICE and RAIN PROTECTION
11.
PAGE NUMBER: 30-7
MMEL REV. NO.: 8
Cabin Window Heat
System
D
1
0
(M) May be inoperative provided:
a) Cabin Window Heat switch is
selected OFF, and
b) Cabin Window Heat System circuit
breakers are pulled and collared.
Maintenance will ensure:
a) Cabin Window Heat switch is
selected OFF, and
b) Cabin Window Heat System
circuit breakers are pulled and
collared.
Flight crew may accomplish this task
if properly qualified and authorized.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
a) Cabin Window
Heating Elements
D
-
0
(M) May be inoperative provided the
associated Windown Heat circuit breakers
are pulled and collared.
Maintenance will pull and collar the
affected cabin window heat system
circuit breakers.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
2.
Flight Data
Recorder (FDR)
Systems
5. MAINTENANCE
3.
(continued)
C
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
31. INDICATING / RECORDING
SYSTEMS
1. Clocks (Cockpit)
D
PAGE NUMBER: 31-1
MMEL REV. NO.: 8
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
-
1
-
1
Any in excess of those required by 14
CFR may be inoperative.
None required.
None required.
An Inoperative Placard will
be placed on affected Clock
face and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed on FDR Control
Panel and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
31. INDICATING / RECORDING
SYSTEMS
2. Flight Data
A
Recorder (FDR)
Systems (continued)
PAGE NUMBER: 31-2
MMEL REV. NO.: 8
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
-
0
(Includes FDR function
of Combined Voice and
Flight Data Recorder
(CVFDR))
May be inoperative provided:
None required.
a) Cockpit Voice Recorder (CVR) is
operative,
b) Airplane is not dispatched from a
designated airport as listed in the
operator’s MEL unless:
1. The FDR failure occurs after
pushback but before takeoff, or
2. The FDR repair was attempted
but was not successful.
c) In those cases where repair is
attempted but not successful, the
airplane may be dispatched on a
flight or series of flights until the
next designated airport where repair
must be accomplished prior to
dispatch, and
d) Repairs are made within three (3)
flight days.
None required.
An Inoperative Placard will
be placed on FDR Control
Panel and will be noted on
ADLS.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Repair category does not apply to
Part 91 operators. See 14 CFR 91.609 or
135.152.
FDR Recording
Parameters
required by 14 CFR
(continued)
A
-
-
Up to three (3) recording parameters may
be inoperative provided:
a) Cockpit Voice Recorder (CVR) is
operative, and
b) Repairs are made within 20
calendar days.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
FDR Recording
Parameters not
Required by 14 CFR
A
-
-
May be inoperative provided repairs are
made prior to the completion of the next
heavy maintenance visit.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight Data Recorder
(FDR) Systems
(Operator Other Than a
Holder of an Air
Carrier or Commercial
Operator Certificate)
C
-
1
Any in excess of those required by 14
CFR may be inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
-
0
May be inoperative provided repairs are
made in accordance with applicable 14
CFRs.
None required.
None required.
C
1
0
May be inoperative provided airplane is
operated in accordance with AFM
Appendix on Brake Kinetic Energy and
Carbon Brake Cooling.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Brake Temperature
Monitoring System
(BTMS)
NOTE: This item includes the BTMS
displayed on the brakes synoptic page.
4.
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
31. INDICATING / RECORDING
SYSTEMS
2. Flight Data
Recorder (FDR)
Systems (continued)
3.
PAGE NUMBER: 31-3
MMEL REV. NO.: 8
G Monitor System
D
1
0
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
31. INDICATING / RECORDING
SYSTEMS
5. Electronic Checklist
C
(GV)
PAGE NUMBER: 31-4
MMEL REV. NO.: 8
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
2
1
May be inoperative provided the checklist
module in Fault Warning Computer
(FWC) 1 is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
May be inoperative provided the current
AFM is carried on board the airplane.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Electronic Checklist
(GV-SP / GIV-X)
C
1
0
Data Acquisition
Unit (DAU) Channels
(GV)
B
4
3
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7. Security System
***
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
8. Engine Cowl Open
*** Indicating System
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
6.
May be inoperative provided right engine
cowl is visually confirmed CLOSED
before starting APU on the ground.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
31. INDICATING / RECORDING
SYSTEMS
9.
Airplane Personality
C
Modules (APM)
(GV-SP, GIV-X)
PAGE NUMBER: 31-5
MMEL REV. NO.: 8
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
4
3
May be inoperative provided APU fire
bottle switch cover is installed and
operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
10.
Plastic Guard
Switch Covers
D
-
1
11.
Configuration
Management Systems
(GV-SP, GIV-X)
C
2
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
12. InfraRed Counter
*** Measuring System
(IRCM) or Directional
InfraRed Counter
Measurers System
(DIRCM)
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
14. XM Weather Receiver
***
D
15.
A
Modular Avionics Unit
(MAU) Channels
(GV-SP/GIV-X)
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
31. INDICATING / RECORDING
SYSTEMS
13. Quick Access Recorder D
*** (QAR)
PAGE NUMBER: 31-6
MMEL REV. NO.: 8
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew will review the next
worse failures as described in
the GAC-OIS-09 Dispatch with
MAU Channels Inoperative.
Flight crew will discuss
contingency procedures should
the next worse failure occur and
plan accordingly for the flight.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
6
5
(M)(O) May be inoperative provided:
Maintenance will pull and collar the
(MAU) Channels
a) Failed channel is not MAU 1A or
associated MAU circuit breakers.
MAU 2B,
b) No other failures exist in the
Avionics System,
c) Associated MAU circuit breakers
are pulled and collared,
d) Alternate procedures are established
and used, and
e) Repairs are made within two (2)
flight days.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
32. LANDING GEAR
Anti-Skid System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 32-1
MMEL REV. NO.: 8
C
1
0
(O) May be inoperative provided airplane
is operated in accordance with AFM
Limitations.
None required.
Flight crew will ensure airplane
is operated in accordance with
AFM, Section 1, Limitations,
and Automatic Ground Spoilers.
(Ground Spoiler may be
inoperative for takeoff provided
Anti-Skid is operative and 20
degrees flaps are used for
takeoff.)
An Inoperative Placard will
be placed on Anti-Skid
"ON/OFF" Switch and will be
noted on ADLS.
Flight crew will select ANTISKID "OFF" and follow AntiSkid Off Braking Procedures.
AFM, Section 3, Abnormal
Procedures, Anti-Skid Failure,
Section 1, Limitations, AntiSkid.
NOTE: May be inoperative
provided AFM performance
penalties are applied. Refer to
AFM, Section 5, Performance,
Reference Accelerate-Stop
Distance.
2.
Rudder Pedal
Steering System
C
1
0
May be inoperative provided Nose Wheel
Tiller Steering System is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 32-2
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
32. LANDING GEAR
3.
Landing Gear
Position Indicators
Deleted in Revision 7a.
4.
Variable Gain Nose
Wheel Steering
C
1
0
(O) May be inoperative provided the fixed
gain steering mode is operative.
None required.
Flight crew will use tiller
steering at or below 60 KCAS
only. Above 60 KCAS, use
pedal steering only. If pedal
steering is unavailable, use
rudder inputs and/or differential
braking until below 60 KCAS.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
5.
Nosewheel Steering
Accessory Hardware
(Torque Link
Lanyards)
D
-
0
May be inoperative or missing.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
6.
Emergency Landing
Gear Extension Bottle
Pressure Gauge
(Nose Wheelwell)
B
1
0
May be inoperative provided Emergency
Landing Gear Extension Bottle Pressure
Cockpit CAS Indication (Summary Page)
is operative and checked prior to each
flight.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7.
Emergency Landing
Gear Extension Bottle
Pressure Cockpit CAS
Indication
(Summary Page)
B
1
0
May be inoperative provided Emergency
Landing Gear Extension Bottle Pressure
Gauge (Nose Wheelwell) is operative and
checked prior to each flight.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
32. LANDING GEAR
Landing Gear
Extension / Retraction
System (includes dump
valve, gear handle, and
blow down bottle)
(GIV-X)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
PAGE NUMBER: 32-3
MMEL REV. NO.: 8
A
1
0
(O) May be inoperative provided:
a) Airplane is operated with the
landing gear in the extended
position,
b) Landing gear handle remains in the
down position,
c) Ground lock pins are installed to
ensure that all three (3) Landing
gears are LOCKED down
throughout flight,
d) Both pilots use cockpit headsets,
e) Operations are not conducted in
known or forecasted icing
conditions,
f) Extended over water operations are
prohibited,
g) Flight is conducted in accordance
with AFM Supplement No. GIV2009-01,
h) Category II operations are
prohibited,
i) EFVS operations below 200 feet
above touchdown zone elevation
are prohibited, and
j) Repairs are made within one (1)
flight day.
None required.
Flight crew will install all three
landing gear ground lock pins
and ensure that the pin’s flags
are removed prior to every
takeoff.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
32. LANDING GEAR
Landing Gear
Extension / Retraction
System (includes dump
valve, gear handle, and
blow down bottle)
(GV/GV-SP)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
PAGE NUMBER: 32-4
MMEL REV. NO.: 8
A
2
0
(O) May be inoperative provided:
a) Airplane is operated with the
landing gear in the extended
position,
b) Landing gear handle remains in the
down position,
c) Ground lock pins are installed to
ensure that all three (3) Landing
gears are LOCKED down
throughout flight,
d) Both pilots use cockpit headsets,
e) Operations are not conducted in
known or forecasted icing
conditions,
f) Extended over water operations are
prohibited,
g) Flight is conducted in accordance
with AFM Supplement No. GV2009-02,
h) Category II operations are
prohibited,
i) EFVS operations below 200 feet
above touchdown zone elevation
are prohibited, and
j) Repairs are made within one (1)
flight day.
None required.
Flight crew will install all three
landing gear ground lock pins
and ensure that the pin’s flags
are removed prior to every
takeoff.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
Cockpit/Flight Deck/
Flight Compartment and
Instrument Lighting
Systems (Excluding
EFIS and EICAS)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 33-1
MMEL REV. NO.: 8
C
-
-
Individual lights may be inoperative
None required.
provided:
a) Remaining Lighting System lights
are sufficient to clearly illuminate
all required instruments, controls
and other devices for which they
are provided,
b) Remaining Lighting System lights
are positioned so that direct rays are
shielded from flight crewmembers'
eyes, and
c) Lighting configuration and intensity
is acceptable to the flight crew.
None required.
An Inoperative Placard will
be placed above the affected
Lighting Rheostat and will be
noted on ADLS.
None required.
An Inoperative Placard will
be placed on affected Cabin
Interior "ON/OFF" Switch
and will be noted on ADLS.
NOTE 1: Individual button/switch lights
and/or annunciation/indications are
excluded from this relief.
NOTE 2: Unaided operation (without
NVGs) may be permitted with inoperated
NVG supplemental lights; cracked or
missing filters.
2.
Passenger Cabin
Interior Illumination
Systems
D
-
-
May be inoperative provided:
a) Cabin emergency lighting is
operative,
b) Sufficient lighting is operative for
crew to perform required duties,
and
c) Lighting configuration at dispatch
is acceptable to flight crew.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
Passenger Lighted
Information Signs
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 33-2
MMEL REV. NO.: 8
C
-
-
(M) May be inoperative provided:
Maintenance will ensure:
a) Associated passenger seat or
a) Associated passenger seat or
lavatory is not occupied from which
lavatory is not occupied, and
a passenger lighted information
b) Associated seat or lavatory is
sign is not readily legible, and
blocked and placarded “DO
b) Associated seat or lavatory is
NOT OCCUPY.”
blocked and placarded - DO NOT
OCCUPY.
None required.
An Inoperative Placard will
be placed on associated seat
or lavatory stating “DO NOT
OCCUPY” and will be noted
on ADLS.
NOTE: These conditions are not intended
to prohibit lavatory use or inspections by
crewmembers.
1)
All Cargo
Supernumerary/
Courier Area
Lighted
Information Signs
(continued)
C
-
-
(O) May be inoperative and associated
passenger seat or lavatory may be
occupied provided:
a) PA System operates normally, and
b) PA System is used to notify
passengers and cabin crew when
associated sign(s) are placed ON or
OFF.
None required.
Flight crew will ensure other
means of communication are
established if PA System does
not operate.
An Inoperative Placard will
be placed on inoperative PA
System and will be noted on
ADLS.
C
-
-
(O) May be inoperative provided alternate
procedures are established and used to
notify couriers/supernumeraries when
associated sign(s) are placed ON or OFF.
None required.
Flight crew will ensure alternate
procedures are established
when associated sign(s) are
placed ON or OFF.
An Inoperative Placard will
be placed in a prominent
position to notify courier/
supernumerary when
associated sign(s) are placed
ON or OFF and will be noted
on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
3.
PAGE NUMBER: 33-3
MMEL REV. NO.: 8
Passenger Lighted
Information Signs
(continued)
The following pertains
only to operations
involving aircraft with
19 or less passenger
seats, wherein
certification or
operating rules do not
require a public address
system or flight
attendant.
2)
4.
Passenger Lighted
Information Signs
Position Light
Bulbs
C
-
-
(O) May be inoperative provided alternate None required.
procedures are established and used to
notify cabin occupants.
Flight crew will ensure alternate An Inoperative placard will
procedures are established and
be placed on inoperative
used.
Passenger Lighted
Information Signs and will be
noted on ADLS.
C
6
3
May be inoperative provided one light
bulb is operative at each position.
None required.
None required.
An Inoperative Placard will
be placed on Position
(Navigation) Light
"ON/OFF" Switch and will be
noted on ADLS.
C
6
0
May be inoperative provided airplane is
not operated at night.
None required.
None required.
An Inoperative Placard will
be placed on Position
(Navigation) Light
"ON/OFF" Switch and will be
noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
6.
7.
Strobes
(Anti-Collision
Lights)
Wing Inspection
Lights
(Airplanes with Wing
Critical Surfaces Not
Visible from Flight
Deck)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
Beacon Light
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5.
PAGE NUMBER: 33-4
MMEL REV. NO.: 8
C
1
0
May be inoperative provided airplane is
not operated at night.
None required.
None required.
An Inoperative Placard will
be placed on Beacon Light
"ON/OFF" Switch and will be
noted on ADLS.
C
1
0
May be inoperative provided Strobes are
installed and operative.
None required.
None required.
An Inoperative Placard will
be placed on Beacon Light
"ON/OFF" Switch and will be
noted on ADLS.
C
6
3
Bulbs may be inoperative provided one
bulb is operative at each position (wingtip
and tail).
None required.
None required.
An Inoperative Placard will
be placed on Strobe
"ON/OFF" Switch and will be
noted on ADLS.
C
6
2
May be inoperative provided:
a) At least one bulb is operative at
each wingtip, and
b) Airplane is not operated at night.
None required.
None required.
An Inoperative Placard will
be placed on Strobe
"ON/OFF" Switch and will be
noted on ADLS.
C
2
0
May be inoperative provided ground
deicing procedures do not require their
use.
None required.
None required.
An Inoperative Placard will
be placed on Wing Inspection
Light "ON/ OFF" Switch and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
9.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
Landing Lights
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
PAGE NUMBER: 33-5
MMEL REV. NO.: 8
B
2
1
May be inoperative provided all three
bulbs of the taxi lights are operative.
None required.
None required.
An Inoperative Placard will
be placed on affected Landing
Light (L LDG) or (R LDG)
"ON/OFF" Switch(es) and
will be noted on ADLS.
C
2
0
May be inoperative provided airplane is
not operated at night.
None required.
None required.
An Inoperative Placard will
be placed on affected Landing
Light (L LDG) or (R LDG)
"ON/OFF" Switch(es) and
will be noted on ADLS.
Taxi Light System
C
1
0
None required.
None required.
An Inoperative Placard will
be placed on Taxi "ON/OFF"
Switch and will be noted on
ADLS.
1) Individual Light
Bulbs
C
3
0
None required.
None required.
An Inoperative Placard will
be placed on Taxi "ON/OFF"
Switch to indicate the
inoperative light bulbs and
will be noted on ADLS.
C
2
0
None required.
None required.
An Inoperative Placard will
be placed on Wing Tip Taxi
"ON/OFF" Switch and will be
noted on ADLS.
10. Wing Tip Taxi
*** Light Systems
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 33-6
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
11. Floor Proximity
*** Emergency Escape
Path Marking System
Lights
C
-
-
12. Pulse Light System
*** (Identification Lights)
D
-
13. Recognition Light
*** System
D
14. Logo Light
*** System
D
One (1) lamp in each of the solid red light
assembly pairs and two (2) lamps of the
five (5) lamp floodlight and exit sign
emergency floor path lighting assemblies
may be inoperative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
0
None required.
None required.
An Inoperative Placard will
be displayed on affected
Pulse Light System Light
Switch and will be noted on
ADLS.
1
0
None required.
None required.
An Inoperative Placard will
be displayed on affected
Recognition Light Switch and
will be noted on ADLS.
1
0
None required.
None required.
An Inoperative Placard will
be displayed on affected Logo
Light Switch and will be
noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 33-7
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
15. Ramp Lights
*** Systems
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed on affected
Ramp Light Switch and will
be noted on ADLS.
16. Flashlight Charging
*** Systems
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
17.
D
-
0
None required.
None required.
An Inoperative Placard will
be placed nest to Aft
Compartment Light Switch
and will be noted on ADLS.
D
1
0
May be inoperative provided no
emergency equipment is carried in the
Cargo Compartment.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided an operative
flashlight is installed in Cargo
Compartment.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Aft Compartment
Lights (Boiler Room)
18. Cargo Compartment
*** Light
19. Pylon Mounted
*** Exterior Baggage
Loading Light Systems
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 33-8
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
20.
Wheel Well Lights
D
3
0
21.
Exterior Emergency
Evacuation Lighting
System
C
1
0
22.
Service Door Lights
D
-
0
23.
Dim and Test
Enunciator Channels
C
-
-
May be inoperative provided airplane is
not operated at night.
May be inoperative provided the switch
capsule is not used in an emergency
procedure where the actuation of the
switch is not displayed elsewhere in the
cockpit.
NOTE: The following switches 1-4 may
not be inoperative:
1. GPWS / Ground Spoiler Override
2. Terrain Display (GV) /
Terrain Inhibit (GV-SP)
3. CPCS Panel Flight / Landing (2)
4. Door Safety
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 33-9
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
24.
Airstair Lights
D
-
0
May be inoperative provided an alternate
means (e.g. flashlight) is used to
illuminate the airstairs.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
25.
Dome Light
D
-
0
May be inoperative provided an alternate
means (e.g. flashlight) is used to
illuminate the vestibule area.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
26.
Baggage Compartment
Light
D
1
0
May be inoperative provided no
emergency equipment is carried in the
baggage compartment.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided an operative
flashlight is installed in the baggage
compartment.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
1
May be inoperative provided the operative None required.
flashlight is in good working order in
accordance with the applicable 14 CFR.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
27.
Cockpit Flashlight
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
33. LIGHTS
29. Tail Position Light
*** LED Element Banks
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
28. Wing Tip Position
*** Light LED Element
Banks
PAGE NUMBER: 33-10
MMEL REV. NO.: 8
C
4
2
One may be inoperative per wing tip
position.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
4
0
May be inoperative provided airplane is
not operated at night.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
2
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
2
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
May be inoperative provided airplane is
not operated at night.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-1
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
1.
Directional Compass
Reference Sensors
B
3
2
(O) May be inoperative provided both
PFD Heading Indicating Systems operate
independently.
None required.
Flight crew will ensure that the
same IRS is NOT used as the
heading source for both pilots.
An Inoperative Placard will
be placed on Mode Select
Unit (MSU) and will be noted
on ADLS.
2.
Attitude Reference
Sensors
B
3
2
(O) May be inoperative provided:
a) Both PFD Attitude Indicating
Systems operate independently, and
b) Standby Attitude Indicator is
operative.
None required.
Flight crew will ensure same
IRS is NOT used as attitude
source for both pilots.
An Inoperative Placard will
be placed on MSU and will
be noted on ADLS.
3.
Standby Flight
Displays
C
-
0
Except for ER operations, may be
inoperative provided not required by 14
CFR.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1) Standby Attitude
Indicator (ElectroMechanical Gyro
Horizon)
B
-
0
May be inoperative provided:
a) Operations are conducted in day
VMC only, and
b) Operations are not conducted into
known or forecast VFR-on-Top
Conditions.
None required.
None required.
An Inoperative Placard will
be placed on face of Standby
Attitude Indicator and will be
noted on ADLS.
a) Glideslope/
Localizer
Indicator
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
***
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
3.
PAGE NUMBER: 34-2
MMEL REV. NO.: 8
Standby Flight
Displays (continued)
***
2) Standby Altimeter/
Airspeed Indicator
(combined unit)
C
1
0
May be inoperative provided airplane is
operated in day VMC only.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
3) 3-in-1 Standby
Attitude, Altitude,
Airspeed Indicator
Heading (Color
Video Display)
(GV Only)
C
-
0
Except for ER operations, the Attitude
position indicator may be inoperative
provided not required by 14 CFR.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
-
0
Attitude position indicator may be
inoperative provided:
a) Operations are conducted in Day
VMC only, and
b) Operations are not conducted into
known or forecast VFR-on-Top
Conditions.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
a) Standby Air Data
Unit(Altitude and
Airspeed Function)
C
1
0
May be inoperative provided the airplane
is operated in day VMC only.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
b) Standby Heading
Display
C
1
0
May be inoperative provided all three (3)
Heading Reference Systems are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
3.
PAGE NUMBER: 34-3
MMEL REV. NO.: 8
Standby Flight
Displays (continued)
***
3) 3-in-1 (Color Video
Display) (GV Only)
(cont’d)
***
c) Glideslope /
Localizer Function
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
d) DME Displays
C
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
e) FMS Navigation
Functions
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 34-4
MMEL REV. NO.: 8
Standby Flight
Displays (continued)
4) 4-in-1 Standby
Attitude, Altitude,
Airspeed Indicator
Heading (Color
Video Display)
(GV-SP, GIV-X)
C
-
0
Except for ER operations, the Attitude
position indicator may be inoperative
provided not required by 14 CFR.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
-
0
Attitude position indicator may be
inoperative provided:
a) Operations are conducted in Day
VMC only, and
b) Operations are not conducted into
known or forecast VFR-on-Top
Conditions.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
a)
Standby Air Data
Unit (Altitude and
Airspeed
Function)
C
1
0
May be inoperative provided the airplane
is operated in day VMC only.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
b)
Standby Heading
Display
C
1
0
May be inoperative provided all three (3)
Heading Reference Systems are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 34-5
MMEL REV. NO.: 8
Standby Flight
Displays (continued)
4) 4-in-1 (Color Video
Display) (GV-SP,
GIV-X) (cont’d)
Heading (Color Video Display) (GV-SP, GIV-X)
***
c)
Glideslope/
Localizer
Function
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
d)
DME Displays
C
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
e)
FMS Navigation
Functions
C
1
0
None required.
None required.
C
-
-
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be placed on Radar Control
Heads and will be noted on
ADLS.
4.
Weather Radar
Systems
Except for ER operations, as required by
14 CFR.
NOTE: See 14 CFR 135.173 or 135.175.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
VOR/ILS
Navigation Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5.
PAGE NUMBER: 34-6
MMEL REV. NO.: 8
C
-
-
As required by 14 CFR and no relief may
be provided to an inoperative system or
component if powered by an emergency
bus.
None required.
None required.
An Inoperative Placard will
be placed on affected RFMU
and will be noted on ADLS.
NOTE: Those required by 14 CFR 91.205,
135.161 or 135.165 are operative.
6.
7.
Marker Beacon
Systems
(GV-SP, GIV-X)
C
3
0
May be inoperative provided approach
procedures do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(GV only)
C
2
0
May be inoperative provided approach
procedures do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Automatic Direction
Finding Systems
C
2
-
As required by 14 CFR.
None required.
None required.
An Inoperative Placard will
be placed on or next to
affected ADF Indicator and
will be noted on ADLS.
NOTE: See 14 CFR 91.205, 135.161 or
135.165.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
ATC Transponder and
Automatic Altitude
Reporting Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
8.
PAGE NUMBER: 34-7
MMEL REV. NO.: 8
B
-
0
May be inoperative provided:
a) Operations do not require its use,
and
b) Before flight, approval is obtained
from ATC facilities having
jurisdiction over the planned route
of flight.
None required.
None required.
An Inoperative Placard will
be placed adjacent to RFMU
(GV) or MCDU (GVSP/GIV-X) and will be noted
on ADLS.
D
-
1
Any in excess of those required by 14
CFR may be inoperative.
None required.
None required.
An Inoperative Placard will
be placed adjacent to RFMU
(GV) or MCDU (GVSP/GIV-X) and will be noted
on ADLS.
NOTE 1: Flight Director, Autopilot, and
Transponder must use the same Air Data
source for flight into RVSM airspace.
NOTE 2: Transponder and altitude
reporting capability must be operative for
flight into RVSM airspace.
*** 1) Elementary and
Enhanced
Downlink
Airplane
Reportable
Parameters not
Required by 14
CFR
A
-
0
May be inoperative provided:
None required.
a) Operations do not require its use,
and
b) Repairs are made before completion
of the next heavy maintenance visit.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
*** 2) ADS-B Squitter
Transmissions
A
-
0
May be inoperative provided:
None required.
a) Operations do not require its use,
and
b) Repairs are made before completion
of next heavy maintenance visit.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Distance
Measuring Equipment
(DME) Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
9.
PAGE NUMBER: 34-8
MMEL REV. NO.: 8
D
-
-
Except where en route operations or
None required.
approach minimums require its use, any in
excess of those required by 14 CFR may
be inoperative.
None required.
An Inoperative Placard will
be placed on the RFMU (GV)
or MCDU (GV-SP/GIV-X)
and will be noted on ADLS.
NOTE: Those required by 14 CFR 91.205
or 135.165 are operative.
10.
Standby RMI
(Electro-Mechanical)
(GV)
C
1
0
May be inoperative provided all three (3)
IRS's are operative.
None required.
None required.
An Inoperative Placard will
be placed on Standby RMI
(GV) and will be noted on
ADLS.
***
1) Standby Navigation C
Display (Color
Video)
1
0
May be inoperative provided all three (3)
IRS’s are operative.
None required.
None required.
An Inoperative Placard will
be placed on the EBDI (GVSP/GIV-X) and will be noted
on ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
*** 2) DME Displays
C
2
0
*** 3) EBDI (Electronic
Bearing / Distance
Indicator)
(GV-SP / GIV-X)
C
1
0
May be inoperative provided all three (3)
IRS’s are operative.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-9
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
11.
Radio Altimeter
Systems
C
2
0
May be inoperative provided:
a) Landing weather minimums or
operating procedures do not require
its use, and
b) Other systems affected (E/GPWS,
TCAS, Flight Director, Autopilot,
Autothrottle, Altimeter Ground
Awareness Display, Synthetic
Vision Primary Flight Display) are
considered.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
12.
Long Range
Navigation Systems
(IRS, GPS and
GNSSU)
C
-
-
May be inoperative except where en route
operations or approach minimums require
the use of GPS or GNSSU.
None required.
None required.
An Inoperative Placard will
be placed on affected
Instrument Controller and
will be noted on ADLS.
None required.
None required.
An Inoperative Placard will
be placed on affected
Instrument Controller and
will be noted on ADLS.
NOTE: For flights conducted in RNP4
airspace, both GPS receivers must be
operative.
C
-
-
As required by 14 CFR.
NOTE: IRS Navigation Function only.
See Attitude Reference Sensors for IRS
Attitude Function.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
13.
PAGE NUMBER: 34-10
MMEL REV. NO.: 8
Terrain Awareness and
Warning System
(TAWS)
Class A TAWS
Equipment Required
1) GPWS
A
1
0
(O) May be inoperative provided:
a) Alternate Procedures are
established and used, and
b) Repairs are made within two (2)
flight days.
None required.
a) Modes 1-4
A
4
0
(O) May be inoperative provided:
a) Alternate Procedures are
established and used, and
b) Repairs are made within two (2)
flight days.
None required.
b) Test Modes
A
1
0
May be inoperative provided:
a) GPWS is considered inoperative,
and
b) Repairs are made within two (2)
flight days.
None required.
(continued)
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
TAWS (continued)
c) Glideslope
Deviation(s)
(Mode 5)
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 34-11
MMEL REV. NO.: 8
d) Advisory Callouts
(continued)
C
-
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(O) May be inoperative provided:
None required.
a) Advisory callout not required by 14
CFR, and
b) Alternate procedures are established
and used.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
***
e) Windshear Mode
(Reactive)
NUMBER REQ’D FOR DISPATCH
PROCEDURE
B
1
0
(O) May be inoperative provided alternate
procedures are established and used.
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
None required.
Flight crew will comply with
AFM/AOM guidance in
windshear situations and
recommend procedures when
encountering windshear.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(O) May be inoperative provided:
None required.
a) Alternate procedures are established
and used, and
b) Windshear Detection and
Avoidance System (Predictive) is
operative.
Flight crew will comply with
AFM/AOM guidance in
windshear situations and
recommend procedures when
encountering windshear.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Operator’s alternate procedures
should include reviewing windshear
avoidance and windshear recovery
procedures.
C
(continued)
MMEL DATE: 11/07/2014
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
TAWS (continued)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 34-12
MMEL REV. NO.: 8
1
0
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
***
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 34-13
MMEL REV. NO.: 8
TAWS (conttinued)
2) Terrain System Forward Looking
Terrain Avoidance
(FLTA) and
Premature
Descent Alert
(PDA) Functions
B
1
0
3) Terrain Display
C
-
B
4) Runway Awareness C
& Advisory System
(RAAS)
(continued)
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
13.
PAGE NUMBER: 34-14
MMEL REV. NO.: 8
TAWS (continued)
Class B TAWS
Equipment
Required
***
1) GPWS
A
1
0
(O) May be inoperative provided:
None required.
a) Alternate procedures are established
and used, and
b) Repairs are made within two (2)
flight days.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
a) Modes 1 & 3
A
2
0
(O) May be inoperative provided:
None required.
a) Alternate procedures are established
and used, and
b) Repairs are made within two (2)
flight days.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
b) Test Mode
A
1
0
May be inoperative provided:
a) GPWS is considered inoperative,
and
b) Repairs are made within two (2)
flight days.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
c) Modes 2, 4 & 5
C
3
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
***
d) Advisory Callouts
***
e) Windshear Mode
(Reactive)
(continued)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
TAWS (continued)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
13.
PAGE NUMBER: 34-15
MMEL REV. NO.: 8
B
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(O) May be inoperative provided:
None required.
a) Advisory callouts are not required
by 14 CFR, and
b) Alternate procedures are established
and used.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
(O) May be inoperative provided alternate
None required.
procedures are established and used.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
13.
PAGE NUMBER: 34-16
MMEL REV. NO.: 8
TAWS (continued)
2) Terrain System Forward Looking
Terrain Avoidance
(FLTA) and
Premature Descent
Alert (PDA)
Functions
B
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
3) Terrain Displays
C
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
4) Runaway
Awareness &
Advisory System
(RAAS)
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
None required.
Flight crew will comply with
AFM/AOM guidance and
recommend procedures.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Class C TAWS
Equipment
*** 1) TAWS/GPWS
(O) May be inoperative provided alternate
procedures are established and used.
NOTE: Any mode that is operative may
be used.
14. Lasertrak NDU
*** (GV)
C
1
0
May be inoperative provided at least one
Flight Management System is operative.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Flight Management
Systems (CDU & Nav
Computer Only)
(GV only)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
15.
PAGE NUMBER: 34-17
MMEL REV. NO.: 8
B
-
0
Except where en route operations or
approach minimums require ite use, may
be inoperative provided:
a) Affected system is not required for
IRS alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not require its use,
and
d) Both RFMUs are operative.
None required.
None required.
An Inoperative Placard will
be placed adjacent to the
CDU and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
One (1) system is required in PRNAV,
BRNAV, RNAV 1 and RNAV 2 airspace.
1) Navigation
Databases
C
-
-
Except where en route operations or
approach minimums require a current
database, may be out of currency
provided:
a) Current Aeronautical Charts are
used to verify Navigation fixes
before dispatch,
b) Procedures are established and used
to verify status and suitability of
Navigation Facilities used to define
route of flight, and
c) Approach Navigation Radios are
manually tuned and identified.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
16. Navigation
*** Management System
PAGE NUMBER: 34-18
MMEL REV. NO.: 8
B
-
0
Except where en route operations or
approach minimums require its use, may
be inoperative provided:
a) Affected system is not required for
IRS alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not depend on its
use, and
d) Both RFMUs are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
One (1) system is required in PRNAV,
BRNAV, RNAV 1 and RNAV 2 airspace.
1)
Navigation
Databases
C
-
-
Except where en route operations or
approach minimums require a current
database, may be out of currency
provided:
a) Current Aeronautical Charts are
used to verify Navigation fixes
before dispatch,
b) Procedures are established and used
to verify status and suitability of
Navigation Facilities used to define
route of flight, and
c) Approach Navigation Radios are
manually tuned and identified.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-19
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
17. Lightning Sensor
*** Systems (LSS)
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
18. Stormscope
***
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
19.
B
-
0
(M) May be inoperative provided:
a) System is deactivated and secured,
and
b) En route or approach procedures do
not require its use.
Maintenance or qualified flight crew
will ensure system is deactivated by
pulling and collaring TCAS Power
CB.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(M) May be inoperative provided:
a) Not required by 14 CFR,
b) System is deactivated and secured,
and
c) En route or approach procedures do
not require its use.
Maintenance or qualified flight crew
will ensure system is deactivated by
pulling and collaring TCAS Power
CB.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Traffic Alert and
Collision Avoidance
System (TCAS I)
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
19.
PAGE NUMBER: 34-20
MMEL REV. NO.: 8
Traffic Alert and
Collision Avoidance
System (continued)
Traffic Alert and
Collision Avoidance
System (TCAS II)
1) Combined Traffic
Alert (TA) and
Resolution
Advisory
(RA) Dual Display
System(s)
(continued)
B
-
0
(M) May be inoperative provided:
a) System is deactivated and secured,
and
b) En route or approach procedures do
not require its use.
Maintenance or qualified flight crew
will ensure system is deactivated by
pulling and collaring TCAS Power
CB.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(M) May be inoperative provided:
a) Not required by 14 CFR,
b) System is deactivated and secured,
and
c) En route or approach procedures do
not require its use.
Maintenance or qualified flight crew
will ensure system is deactivated by
pulling and collaring TCAS Power
CB.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
2
1
May be inoperative on the non-flying pilot None required.
side provided:
a) TA and RA visual display is
operative on the flying pilot side,
and
b) TA and RA audio function is
operative on flying pilot side.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
TCAS II
(continued)
2) Resolution
Advisory (RA)
Display System(s)
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
19.
PAGE NUMBER: 34-21
MMEL REV. NO.: 8
C
2
1
May be inoperative on non-flying pilot
side.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(O) May be inoperative provided:
a) Traffic Alert (TA) visual display
and audio functions are operative,
b) TA only mode is selected by the
crew, and
c) En route or approach procedures do
not require its use.
None required.
Flight crew will verify that the
RA Display System is NOT
required for the en route and/or
approach phase of the proposed
flight.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3) Traffic Alert
Display System(s)
C
-
0
(O) May be inoperative provided:
a) RA visual display and audio
functions are operative, and
b) En route or approach procedures do
not require its use.
None required.
Flight crew will verify that the
TA Display System is NOT
required for the en route and/or
approach phase of the proposed
flight.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4) Audio Functions
B
1
0
May be inoperative provided en route or
approach procedures do not require use of
TCAS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
5) Airspace Selection
Function (Above /
Normal / Below)
C
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
20. Microwave Landing
*** Systems (MLS)
D
21.
C
22.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
Symbol Generators
(GV)
PAGE NUMBER: 34-22
MMEL REV. NO.: 8
-
-
As required by 14 CFR.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(M)(O) May be inoperative provided:
a) EFIS displays at pilot’s and
copilot's stations are operative from
independent Symbol Generators,
and
b) Both EICAS displays are operative.
Maintenance should move
inoperative SG to No. 3 position.
Refer to AMM Chapter 31-62-00.
Flight crew will ensure EFIS
Displays at pilot's and copilot's
stations are operative from
Independent Symbol
Generators, and BOTH EICAS
Displays (DU 3 and 4) are
operative. Crew WILL select
ALT for No. 3 SG to power
EICAS displays.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Those required by 14 CFR 91.205
[or] 135.161 thru 135.165 are operative.
3
2
Flight crew may accomplish this task
if properly qualified and authorized.
Guidance Panel Digital
Indications and Mode
Select Indications
1) Speed Display
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2) Heading Display
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
22.
PAGE NUMBER: 34-23
MMEL REV. NO.: 8
Guidance Panel Digital
Indications and Mode
Select Indications
(continued)
3) VS/FPA Display
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4) Altitude Select
Display
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
5) LNAV
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
6) VNAV
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7) FLCH
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
22.
PAGE NUMBER: 34-24
MMEL REV. NO.: 8
Guidance Panel Digital
Indications and Mode
Select Indications
(continued)
8) Manual Speed
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
9) Bank Select
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
10) BC Select
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
11) Heading Select
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
12) VS/FPA Select
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(continued)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
22.
PAGE NUMBER: 34-25
MMEL REV. NO.: 8
Guidance Panel Digital
Indications and Mode
Select Indications
(continued)
13) Alt Hold Select
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
14) Approach
C
1
0
May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
15) PFD Command
L/R
C
1
0
(O) May be inoperative provided the
associated value is available in the
Primary Flight Display.
None required.
On initial power up of the
airplane, the default is PFD
command left PFD. If button is
pushed several times, PFD
command to the left PFD can be
established by pulling and
resetting Guidance Panel circuit
breakers.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
16) APR Switch
C
1
0
May be inoperative provided the
associated valve is available in the
Primary Flight Display
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Altitude Alerting
System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
23.
PAGE NUMBER: 34-26
MMEL REV. NO.: 8
A
-
0
(O) May be inoperative provided:
a) Autopilot with altitude hold, and
altitude capture operates normally,
b) En route operations, i.e. RVSM, do
not require its use,
c) Airplane does not depart from a
designated airport (as listed in the
operator’s MEL) where repair or
replacement can be made, and
d) Repairs are made within three (3)
flight days.
None required.
Flight crew will ensure
Autopilot with Altitude Hold is
operable.
NOTE: Flight into RVSM
airspace is not allowed with
inoperative Altitude Alerting
System.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1)
Aural Alert
C
-
0
May be inoperative provided:
a) Visual alert operates normally, and
b) Auto-pilot with altitude hold and
altitude capture operates normally.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2)
Visual Alert
C
-
0
May be inoperative provided:
a) Aural alert operates normally, and
b) Auto-pilot with altitude hold and
altitude capture operates normally.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
(continued)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
24. Display Units
*** (GV)
PAGE NUMBER: 34-27
MMEL REV. NO.: 8
C
6
5
(M)(O) May be in operative provided:
a) Inoperative tube is located in the
Copilot's Navigation Display
Position (DU #5),
b) Standby Attitude Indicator is
operative,
c) Standby RMI is operative, and
d) Alternate procedures are developed
for operation without the Copilot's
Navigation displays.
Maintenance will move the
inoperative display unit to the
Copilot's Navigation Display
Position (DU #5). Refer to AMM
Chapter 31-63-03.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will ensure Standby
Attitude Indicator and Standby
RMI are operative. Alternate
Procedures for operation
without Copilot's Navigation
Display (Pre-Takeoff and PreArrival Crew Briefings) should
include crew actions in the
event of failure of another DU.
Factors concerning abort
criteria, takeoff continuance,
deviation to alternate airfield
and mission continuance should
be included in there briefings.
For an approach with both
copilot's PFD and ND
inoperative, it is recommended
that Compass Mode be selected
on pilot's ND.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
24.
PAGE NUMBER: 34-28
MMEL REV. NO.: 8
Display Units
(continued)
*** Display Units (GV)
For DU-885 Equipped
Airplanes
(continued)
C
6
5
(M)(O) May be inoperative provided:
a) Inoperative tube is located in the
Copilot’s Navigation Display
Position (DU #5),
b) Standby Attitude Indicator is
operative,
c) Standby RMI is operative,
d) Alternate procedures are developed
for operation without the Copilot’s
Navigation displays, and
e) Terminal charts for the origin,
destination and alternate airports are
verified to be current and onboard
the aircraft.
Maintenance will move the
inoperative display unit to the
Copilot's Navigation Display
Position (DU #5). Refer to AMM
Chapter 31-63-03.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will ensure the
following:
a) Standby Attitude Indicator
and Standby RMI are
operative,
b) Alternate Procedures for
operation without Copilot's
Navigation Display (PreTakeoff and Pre-Arrival
Crew Briefings) should
include crew actions in the
event of failure of another
DU,
c) Factors concerning abort
criteria, takeoff
continuance, deviation to
alternate airfield and
mission continuance
should be included in their
briefings, and
d) Terminal charts for origin,
destination and alternate
airports are verified to be
current and onboard the
aircraft.
For an approach with both
copilot's PFD and ND
inoperative, it is recommended
that Compass Mode be selected
on pilot's ND.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Display Units
(continued)
Display Units
(GV-SP, GIV-X)
25.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
24.
PAGE NUMBER: 34-29
MMEL REV. NO.: 8
Standby Magnetic
Compass System
(Flux Valve)
(GV)
*** Magnetometer
(GV-SP, GIV-X)
C
4
3
(M)(O) May be inoperative provided:
a) The unit is located in the DU 3
position, and
b) The pilot in the left seat flies the
airplane.
Maintenance will move the
inoperative display unit to the DU3
position. Refer to AMM Chapter 3163-03
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will discuss
alternate procedures for loss of a
second display for all phases of
flight including failures during
takeoff, approach, landing, and
go-around. It is required that the
pilot in the left seat fly the
airplane.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
May be inoperative provided all three (3)
Heading Reference systems are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
May be inoperative provided all three (3)
IRS’s are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
27. Head Up Display
*** System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
26. Non-Stabilized
*** Magnetic Compass
PAGE NUMBER: 34-30
MMEL REV. NO.: 8
B
1
0
May be inoperative provided any
combination of three (3) Gyro or INS
(IRU) Stabilized Compass Systems are
operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
1
0
May be inoperative provided:
a) Any combination of two(2) Gyro or
INS (IRU) Stabilized Compass
Systems are operative, and
b) Airplane is operated with Dual
Independent Navigation Capability
and under Positive Radar Control
by ATC on the en route portion of
the flight.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
1
0
May be inoperative for flights that are
entirely within areas of magnetic
unreliability provided at least two
Stabilized Directional Gyro Systems are
installed, operative, and used in
conjunction with accepted Free Gyro
Navigation Techniques.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided landing
weather minimums or operating
procedures do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
29.
AFIS Printer
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
1)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
28. Airborne Flight
*** Information System
(AFIS)
PAGE NUMBER: 34-31
MMEL REV. NO.: 8
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be placed on AFIS Printer
and will be noted on ADLS.
NOTE: The relief includes the datalink
function (GV, GV-SP, GIV-X) and ADSA/ADS-C function (GV-SP, GIV-X).
D
-
0
Slip-Skid Indicator
B
2
1
May be inoperative provided:
a) Third attitude indicator is installed
and operative, and
b) An operative Slip indication is
obtained by selecting another IRS
source via the Display Controller.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(GV Only)
B
2
1
(O) May be inoperative provided
electronic slip indicator is replaced by a
mechanical slip indicator.
None required.
Flight crew will ensure
mechanical slip indicator is
installed.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
B
2
0
May be inoperative provided airplane is
operated during day VMC conditions.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
31.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Data Management
Unit (DMU)
(GV-SP, GIV-X)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
30. Data Loader
*** (GV)
PAGE NUMBER: 34-32
MMEL REV. NO.: 8
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
3
2
Maintenance will pull and collar
circuit breaker associated with Micro
Air Data Computers.
Flight crew will operationally
check and assure that the items
called out in provisos a) thru d)
are operative.
An Inoperative Placard will
be placed on the instrument
panel near the Display Unit
affected.
Air Data Computers/
Systems
1) Micro Air Data
Computers
(GV)
(M) (O) May be inoperative provided:
a) Manual Pressurization Control
System is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative, and
e) Airplane is operated in accordance
with AFM Limitations.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will comply with all
AFM limitations in Section
1-03-30, 1-03-40, and 1-21-10.
NOTE: Two systems are required for
operation in RVSM airspace.
C
(continued)
3
2
May be inoperative provided airplane is
operated in unpressurized configuration.
None required.
None required.
An Inoperative Placard will
be placed on the instrument
panel near the Display Unit
affected.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
31.
PAGE NUMBER: 34-33
MMEL REV. NO.: 8
Air Data Computers/
Systems (continued)
2) Air Data Systems
(ADS)
(GV-SP, GIV-X)
C
3
2
(M) May be inoperative provided:
a) Manual Pressurization Control
System is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative, and
e) Airplane is operated in accordance
with AFM Limitations.
Maintenance will pull and collar the
ADM circuit breaker associated with
the ADS failure.
None required.
An Inoperative Placard will
be placed on Air Data
Systems to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be will be placed on
Integrated Avionics
Computers (IACs) to be seen
by flight crew and will be
noted on ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
NOTE 1: Two systems are required for
operation in RVSM airspace.
NOTE 2: If ADS 2 is failed, the WOW
indications on the copilot’s flight control
synoptic will be crosshatched. Dispatch is
still allowed if the WOW indications on
the pilot’s flight control synoptic are
shown as valid.
32. Integrated Avionics
*** Computers (IACs)
(GV)
C
-
2
May be inoperative provided two bus
controllers are operative for dispatch.
NOTE: The FMS/PMS/Autothrottle
function of the operative IACs may be
inoperative as stated elsewhere in this
section. The autopilot is addressed in
ATA 22.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
34. Airshow Controller
*** System
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Bus Controllers
(GV)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
33.
PAGE NUMBER: 34-34
MMEL REV. NO.: 8
C
-
2
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1) Cockpit Airshow
Display System
D
-
0
None required.
None required.
***
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2) Cabin Airshow
Display System
D
-
0
None required.
None required.
***
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-35
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
35.
***
Windshear Warning
and Flight Guidance
System (Reactive)
C
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will comply with
the AFM/AOM guidance on
windshear conditions and the
recommended procedures for
windshear encounters.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
36.
***
Windshear Detection
and Avoidance System
(Predictive)
C
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will comply with
the AFM/AOM guidance on
windshear conditions and the
recommended procedures for
windshear encounters.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
37.
***
Cockpit Video
Monitors
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
38.
***
Heads Up Checklist
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-36
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
39.
***
Enhanced Vision
System (EVS)
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
1)
EVS Window
Heat
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
2)
Secondary
(non-HUD)
EVS Display
Repeater
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
40.
Terrain Server
Function/EGPWM
Modules (GV-SP,
GIV-X)
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
41.
***
Electronic Flight
Bag
May be inoperative provided procedures
are not dependent on its use.
C Function/EGPWM
2
0
NOTE: Synthetic Vision PFD synthetic
terrain will not be available with dual
Terrain Server failures, but the full PFD
may be used without restriction.
Moved to ATA 46 in Rev. 7
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Advanced Graphics
Modules (AGM)
(GV-SP, GIV-X)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
42.
PAGE NUMBER: 34-37
MMEL REV. NO.: 8
C
Advanced Graphics
C
Module (AGM)
(GV-SP, GIV-X)
(ASC 904 - Cert
Charlie and ASC 905 –
Cert Charlie II and Any
later revision to the
Operating software)
4
4
3
3
(M)(O) May be inoperative provided:
a) The inoperative AGM is located in
the AGM 3 position, and
b) Crew actions for subsequent
failures are established.
Maintenance will move the
inoperative AGM module to the
AGM 3 position.
(O) May be inoperative provided:
a) The inoperative AGM is
electronically switched to the AGM
3 position resulting in DU3 Red
Xing, and
b) Crew actions for subsequent
failures are established.
None required.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will discuss the
alternate procedures for sharing
displays including if a display
fails during all phases of flight
including takeoff, approach,
landing, and go-around.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew will ensure:
a) The failed AGM is
electronically switched to
the number 3 position,
b) Verify that DU 3 is Red
X’ed prior to dispatch,
c) Dim DU 3 to eliminate the
Red X, and
d) Discuss alternate procedures
for sharing displays in the
event a second AGM or DU
fails during any phase of
flight
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Refer to AFM Sections
2-08-260/261 and Section 3-1611.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-38
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
43.
Cockpit Printer
D
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
44.
Cursor Control
Devices
(GV-SP, GIV-X)
C
2
0
May be inoperative provided:
None required.
a) Both Display Controllers, Weather
Radar Controllers, and 2 MCDU’s
are operative, and
b) Terminal charts for the origin,
destination and alternate airports are
verified to be current and onboard
the aircraft.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
Cursor Control Devices C
(GV Only)
2
0
(M)(O) May be inoperative provided:
Maintenance will pull and collar the
a) Both Display Controllers are
circuit breaker for the inoperative
operative, and
CCD.
b) Terminal charts for the origin,
destination and alternate airports are
verified to be current and onboard
the aircraft.
Flight crew will ensure that
terminal charts for the origin,
destination and alternate airports
are verified to be current and
onboard the aircraft.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Multifunction Control
Display Units (MCDU)
(GV-SP, GIV-X)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
45.
PAGE NUMBER: 34-39
MMEL REV. NO.: 8
C
3
2
(M) May be inoperative provided:
a) The FMS functions and Radio
Tuning functions are operative on
the remaining MCDU’s, and
b) The inoperative MCDU is located
in either the No. 1 or the No. 2
position.
Maintenance will perform procedures None required.
in accordance with AMM Chapter
34-60-03. The inoperative MCDU
will be moved to the No. 1 or No. 2
position.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: MCDU 3 has Backup Radio
Tuning functions.
1)
Flight
Management
System (FMS)
Functions
(GV-SP, GIV-X)
(continued)
B
3
1
Except where en route operations or
approach minimums require its use, may
be inoperative provided:
a) Affected system is not required for
IRS alignment,
b) Long Range Navigation is not
dependent on its use, and
c) Procedures do not require its use.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
RNP RNAV including PRNAV and
BRNAV only require a single FMS.
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
45.
PAGE NUMBER: 34-40
MMEL REV. NO.: 8
Multifunction Control
Display Units (MCDU)
(GV-SP, GIV-X)
(continued)
2)
a) Navigation
Database
C
-
-
Except where en route operations or
None required.
minimums require a current database, may
be out of currency provided:
a) Current Aeronautical Charts are
used to verify Navigation fixes
before dispatch,
b) Procedures are established and used
to verify status and suitability of
Navigation Facilities used to define
the route of flight, and
c) Approach Navigation Radios are
manually tuned.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Radio Tuning
Functions
(GV-SP, GIV-X)
B
3
2
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-41
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
46.
Advanced Graphics
Module (AGM)
Databases
(GV-SP, GIV-X)
C
-
0
May be out of currency provided:
a) Current IFR/VFR Aeronautical
Charts or appropriate airport
information charts are used to
verify the information before
dispatch,
b) Procedures are established and used
to verify the status and suitability of
Navigation Facilities used to define
the route of flight, and
c) Approach Navigation Radios are
manually tuned and identified.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
47.
Charts Function
(GV-SP, GIV-X)
D
2
0
May be inoperative provided current
None required.
aeronautical charts are carried onboard the
airplane and available to the flight crew.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1)
C
4
0
May be out of currency provided the
terminal charts for the origin, destination
and alternate airports are verified to be
current.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
4
0
May be out of currency provided the
terminal charts for the origin, destination
and alternate airports are verified to be
current and on board.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
1
0
May be inoperative provided alternate
procedures are established for the use of
the Enhanced Vision System (EVS)
display function.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
48.
Charts Database
Video Function
(GV-SP, GIV-X)
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
***
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
49.
***
PAGE NUMBER: 34-42
MMEL REV. NO.: 8
Automatic Dependent
Surveillance-Broadcast
(ADS-B) System
D
1)
Cockpit Display
and Traffic
Information
(CDTI)
D
-
0
May be inoperative provided it is not
required by 14 CFR.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: If ADS-B is installed in lieu of or
as a replacement for 14 CFR required
equipment, the repair category in the
operator’s MEL will be the same as that of
the 14 CFR required equipment.
-
0
NOTE: Cockpit Display Traffic
Information (CDTI) display of data from
other airplane systems may be used.
***
2)
CDTI Control
Panel
D
-
0
***
3)
Date Link
Transmitter(s)
D
-
0
May be inoperative provided:
a) Flight ID can be set, and
b) Screen display is acceptable to the
flight crew.
NOTE: In some airplanes the Data Link
Transmission is an integral part of the
transponder and relief is provided in that
section.
***
4)
Data Link
Receivers
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
5)
ADS-B
Applications
D
-
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Right Side Display
Controller (GV Only)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
50.
PAGE NUMBER: 34-43
MMEL REV. NO.: 8
A
1
0
(M) (O) May be inoperative provided:
a) The weather at the destination is
forecast to be VFR (1,000 ft ceiling
and three (3) miles visibility),
b) An alternate airport is specified in
the flight plan which has VFR
weather forecast (1,000 ft ceiling
and three (3) miles visibility),
c) Both VOR and ADF navigation
receivers are operative,
d) Flight is conduncted based on short
range navigation sources only being
available,
e) Navigation sufix in the IFR flight
plan clearly indicates that the
airplane is not capable of any RNP
required navigation capability,
f) Flight is conducted in airspace
where the availability of navigation
by short range navigation receivers
(VOR/ADF) is assured,
g) One DBDI or Standby RMI or
Secondary Navigation Display is
operative,
h) Associated Display Controller
circuit breaker is pulled and
collared.
i) Alternate procedures are established
and used, and
j) Repairs are made within one (1)
flight day.
Maintenance will ensure associated
Display Controller circuit breaker for
the failed Display Controller is
pulled and collared.
The flight crew shall prepare
and display a TOLD (Takeoff
and Landing Data) card pror to
takeoff and prior to approach
and landing.
An Inoperative Placard will
be placed on the Right Side
Display Controller and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
Right Side Display
Controller
(GV-SP/GIV-X Only)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
50.
PAGE NUMBER: 34-44
MMEL REV. NO.: 8
A
1
0
(M)(O) May be inoperative provided:
Maintenance will pull and collar
a) FMS is the navigation source on
associated Display Control circuit
both PFD’s,
breaker.
b) Destination and alternate airports
have either LPV, GPS or FMS
overlay approaches available
without NOTAM restrictions for
airplanes not equipped with
Enhanced Navigation Package,
c) Destination and alternate airports
have either LPV, GPS, FMS
overlay, or ILS approach available
without NOTAM restrictions for
airplanes equipped with Enhanced
Navigation Package,
d) No other display system failures
exist,
e) Associated Display Controller
circuit breaker is pulled and
collared,
f) Alternate procedures are established
and used, and
g) Repairs are made within two (2)
flight days.
Flight crew will verify the
required approaches are
available at the destination and
alternate airports without being
NOTAMed out of service or
unusable. When weather
conditions exist at the
destination or alternate airport
during the approach, the PNF
will be prepared to announce
approach minimums in the event
the operative Display Controller
fails en route.
An Inoperative Placard will
be placed on the Right Side
Display Controller and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 34-45
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
34. NAVIGATION
51.
***
Synthetic Vision
Primary Flight Display
(SV-PFD) Functions
D
2
0
None required.
None required.
52.
***
DDA (Digital to
Discrete Adapter)
(GV only)
D
2
0
53.
***
GNSSU WAAS (Wide
Area Augmentation
System or SBAS –
Space Based
Augmentation System)
Function
D
2
***
1)
LPV Enable
Switches
(GV Only)
C
54.
CAS Scroll Switches
D
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
May be inoperative provided approach
minimums do not require its use.
None required.
None required.
0
WAAS function may be inoperative
provided en route and approach
procedures do not require its use.
None required.
None required.
2
0
May be inoperative provided approach
procedures do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2
0
May be inoperative provided both CCD’s
are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
35. OXYGEN
2.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 35-1
MMEL REV. NO.: 8
Passenger Oxygen
System and Supply
B
-
-
As required by 14 CFR.
Cabin Oxygen ON
Warning System
C
1
0
May be inoperative provided:
a) Cabin Altitude and Differential
Pressure Indicators are operative,
and
b) Cabin Altitude Pressure Warning
System is operative.
None required.
None required.
An Inoperative Placard will
be placed above "ON"
position on Oxygen Control
Panel and will be noted on
ADLS.
C
1
0
(O) May be inoperative provide airplane
is operated in unpressurized
configuration.
None required.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to the full open
position with RAM Air selected
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
An Inoperative Placard will
be placed above "ON"
position on Oxygen Control
Panel and will be noted on
ADLS.
None required.
None required.
NOTE: Minimum oxygen
supply for dispatch will be
computed from data in the
applicable AFM Supplement for
the Oxygen System STC with
reference to the requirements of
14 CFR 91.211.
An Inoperative Placard will
be placed on affected Oxygen
Control Panel or Mask Unit
and will be noted on ADLS.
Additionally, affected seats
shall be blocked and
placarded.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MMEL REV. NO.: 8
PAGE NUMBER: 35-2
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
PROCEDURE
7. PLACARDING
PROCEDURE
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
35. OXYGEN
NUMBER REQ’D FOR DISPATCH
4. MMEL REMARKS OR
EXCEPTIONS
5. MAINTENANCE
PROCEDURE
NOTE: Information regarding the oxygen system capabilities for each airplane can be found in the Airplane Flight Manual Supplement for Oxygen Systems. The following document number,
G450/G350 – GC41453M000, G550/G500 – GC51453M004 or GV – GC52712M001 are associated with the Oxygen Flight Manual Supplements however, each operator must verify that the
document number is applicable to the particular airplane.
EXAMPLE OF G550 OXYGEN SYSTEM: OXYGEN REQUIRED FOR DE-PRESSURIZATION AND CONTINUED CRUISE
REQUIRED BOTTLE PRESSURE AT DISPATCH
TIME
NUMBER OF PASSENGERS
(HR:MIN)
0
1
2
4
6
8
10
15
19
1:00
413
447
482
551
621
690
759
932
1071
1:30
508
560
613
717
822
927
1031
1293
1502
2:00
603
673
743
883
1023
1163
1303
1653
1933
2:30
699
786
874
1049
1225
1400
1575
2014
25000
3:00
794
899
1005
1215
1426
1637
1847
3:30
890
1013
1136
1382
1628
1874
4:00
985
1126
1266
1548
1829
4:30
1080
1239
1397
1714
2030
5:00
1176
1352
1528
1880
1:00
369
397
424
479
534
589
644
782
892
1:30
440
481
522
605
687
770
852
1058
1223
2:00
510
565
620
730
840
950
1060
1334
1554
2:30
581
650
718
855
993
1130
1267
1611
1885
20000
3:00
651
734
816
981
1146
1310
1475
1887
3:30
722
818
914
1106
1298
1491
1683
2163
4:00
792
902
1012
1232
1451
1671
1890
4:30
863
986
1110
1357
1604
1851
5:00
933
1070
1208
1482
1757
2031
1:00
342
355
369
397
425
453
481
550
606
1:30
396
416
436
476
517
557
597
698
778
2:00
450
477
503
556
608
661
713
845
950
2:30
505
537
570
635
700
765
830
992
1122
15000
3:00
559
598
637
714
791
869
946
1140
1295
3:30
614
659
703
793
883
973
1063
1287
1467
4:00
668
719
770
873
975
1077
1179
1435
1639
4:30
722
780
837
952
1066
1181
1296
1582
1811
5:00
777
840
904
1031
1158
1285
1412
1730
1984
CRUISE
ALTITUDE
(FT)
Based on pressure reading at 70ºF.
Includes oxygen for three crewmembers breathing 100% oxygen for emergency descent plus two minutes. Normal dillution for remainder of flight.
Increase oxygen required by 37 PSIG for each crewmember on oxygen at/above FL410 for each 60 minutes.
Maximum system pressure is 1800 PSIG. Values in excess of 1800 are shown for interpolation purposes only.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
4. Portable Oxygen
*** Dispensing Units
(Bottle and Mask)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
D
2
0
May be inoperative provided the
associated cockpit gauge is operative and
monitored.
None required.
None required.
An Inoperative Placard will
be placed on Oxygen Service
Panel Gauges and will be
noted on ADLS.
B
-
-
Any in excess of those required by 14
CFR may be inoperative or missing
provided required distribution is
maintained throughout airplane.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Any bottle not properly serviced is
considered inoperative and should be
removed.
5.
Oxygen Supply
Warning Systems
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
35. OXYGEN
Oxygen Service
Panel Pressure
Gauges
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 35-3
MMEL REV. NO.: 8
C
2
0
May be inoperative provided associated
cockpit gauge is operative and monitored.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 35-4
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
35. OXYGEN
6. Protective Breathing
*** Equipment (PBE)
D
-
-
Any in excess of those required by 14
CFR may be inoperative or removed
provided location placarding is removed
or obscured.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
7. Electronic Equipment
*** Rack Oxygen Pressure
Gauges
D
-
0
May be inoperative provided cockpit
gauges are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
8.
Cockpit Oxygen
Pressure Indications
C
-
0
May be inoperative provided:
a) Oxygen Service Panel Pressure
Gauges are operative and checked
before every takeoff, and
b) Crew Oxygen Off and Passenger
Oxygen Off messages are not
displayed on the CAS prior to every
takeoff.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
9.
Therapeutic Oxygen
C
-
-
As required by 14 CFR.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 35-5
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
35. OXYGEN
10. High Landing Field
*** Elevation Passenger
Oxygen Controller
High Altitude Switch
(GV-SP/GIV-X)
D
1
0
May be inoperative provided the
maximum Landing Field Elevation does
not exceed 14,500 feet.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1) High Altitude Switch
*** Light (GV-SP/GIV-X)
D
1
0
May be inoperative provided the switch
position is verified to be depressed in
whenever the Landing Field Elevation
exceeds 14,500 feet.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
36. PNEUMATIC
1.
PAGE NUMBER: 36-1
MMEL REV. NO.: 8
Bleed Air Systems
(GV, GV-SP)
1) Pressurized
Configuration
C
2
1
(M) Except for ER operations, may be
inoperative provided:
a) Inoperative Bleed Control Valve is
CLOSED and deactivated
electrically when associated Engine
Bleed Air System is selected OFF,
b) Opposite Engine Bleed Air System
is operative,
c) Isolation Valve is verified to be
operative and selected OPEN, and
d) Airplane is operated in accordance
with AFM Limitations.
NOTE: Auto-throttle will be inoperative
with Isolation Valve OPEN.
Maintenance will CLOSE
None required.
inoperative Bleed Control Valve and
electrically deactivate affected
system. If failure occurs with 1)
Right Bleed Air Control Valve:
Select Right Bleed Air Valve OFF
utilizing R Eng Bleed Air Switch and
Pull R Bleed CONT Circuit Breaker
(CB). 2) Left Bleed Air Control
Valve: Select Left Bleed Air Valve
OFF utilizing L Eng Bleed Air
Switch and Pull Left Bleed CONT
Circuit Breaker (CB). In addition,
opposite Engine Bleed Air System
and Isolation Valve will be verified
operative and Isolation Valve
selected OPEN. Refer to AMM
Chapter 36-12-00.
Flight crew may accomplish this task
if properly qualified and authorized.
(continued)
An Inoperative Placard will
be placed above the affected
Bleed Air Control Switch and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
36. PNEUMATIC
1.
PAGE NUMBER: 36-2
MMEL REV. NO.: 8
Bleed Air Systems
(GV, GV-SP)
(continued)
2) Unpressurized
Configration
(continued)
C
2
0
(M)(O) Except for ER operations, may be
inoperative provided:
a) Inoperative Bleed Control Valve is
CLOSED and deactivated
electrically when associated Engine
Bleed Air System is selected OFF,
b) Airplane is not operated in forecast
or known icing conditions, and
c) Airplane is operated in accordance
with AFM Limitations.
Maintenance will ensure both Bleed
Air Valves are CLOSED and
deactivated electrically.
Flight crew may accomplish this task
if properly qualified and authorized.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to the full open
position with RAM Air selected
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
An Inoperative Placard will
be placed above the affected
Bleed Air Control Switch(es)
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
36. PNEUMATIC
1.
PAGE NUMBER: 36-3
MMEL REV. NO.: 8
Bleed Air Systems
(continued)
(GIV-X only)
1) Pressurized
Configuration
C
2
1
(M) Except for ER operations, may be
inoperative provided:
a) Inoperative Bleed Control Valve is
CLOSED and deactivated
electrically when associated Engine
Bleed Air System is selected OFF,
b) Opposite Engine Bleed Air System
is operative,
c) Isolation Valve is verified to be
operative and selected OPEN,
d) Airplane is not operated in forecast
or known icing conditions, and
e) Airplane is operated in accordance
with AFM Limitations.
Maintenance will CLOSE associated
Bleed Control Valve and electrically
deactivate system. In addition,
opposite Engine Bleed Air System
and Isolation Valve will be verified
operative and Isolation Valve
selected OPEN. Refer to AMM
Chapter 36-12-00.
None required.
An Inoperative Placard will
be placed above both Bleed
Air Control Switches and will
be noted on ADLS.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to the full open
position with RAM Air selected
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
An Inoperative Placard will
be placed on affected
Valve(s) and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
NOTE: Auto-throttle will be inoperative
with Isolation Valve OPEN.
2) Unpressurized
Configuration
C
2
0
(M)(O) Except for ER operations, may be
inoperative provided:
a) Affected Valve(s) is verified
CLOSED,
b) Airplane is not operated in known
or forecast icing conditions, and
c) Airplane is operated in accordance
with AFM Limitations.
NOTE: Auto-throttle will be inoperative
with Isolation Valve OPEN.
Maintenance will ensure all affected
Valve(s) are verified CLOSED.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
36. PNEUMATIC
2.
PAGE NUMBER: 36-4
MMEL REV. NO.: 8
Bleed Air Hot Warning
Systems
1) Pressurized
Configuration
C
2
1
(M) Except for ER operations, may be
inoperative provided:
a) Associated Bleed Control Valve is
CLOSED and deactivated
electrically when associated Engine
Bleed Air System is selected OFF,
b) Opposite Engine Bleed Air System
is operative,
c) Isolation Valve is verified to be
operative and selected OPEN,
d) Airplane is not operated in known
or forecast icing conditions, and
e) Airplane is operated in accordance
with AFM Limitations.
NOTE: Auto-throttle will be inoperative
with Isolation Valve OPEN.
(continued)
Maintenance will CLOSE associated
Bleed Control Valve and electrically
deactivate system. In addition,
opposite Engine Bleed Air System
and Isolation Valve will be verified
operative and Isolation Valve
selected OPEN. Refer to AMM
Chapter 36-12-00.
Flight crew may accomplish this task
if properly qualified and authorized.
None required.
An Inoperative Placard will
be placed above both Bleed
Air Control Switches and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
36. PNEUMATIC
2.
PAGE NUMBER: 36-5
MMEL REV. NO.: 8
Bleed Air Hot Warning
System (continued)
2) Unpressurized
Configuration
C
2
0
(M)(O) Except for ER operations, may be
inoperative provided:
a) Associated Bleed Control Valve is
CLOSED and deactivated
electrically when associated Engine
Bleed Air System is selected OFF,
b) Airplane is not operated in forecast
or known icing conditions, and
c) Airplane is operated in accordance
with AFM Limitations.
Maintenance will ensure both Bleed
Air Valves are CLOSED and
deactivated electrically by verifying
the capsules indicate OFF.
Flight crew may accomplish this task
if properly qualified and authorized.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to the full OPEN
position with RAM Air selected
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
An Inoperative Placard will
be placed above both Bleed
Air Control Switches and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
36. PNEUMATIC
Isolation Valve
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 36-6
MMEL REV. NO.: 8
C
1
0
(M) May be inoperative provided:
a) Both Bleed Air Systems are
operative,
b) Both Environmental Control
Systems (ECS) Packs are operative,
c) Isolation Valve is electrically
deactivated,
d) Isolation Valve is verified
CLOSED, and
e) Airplane is operated in accordance
with AFM Limitations.
Maintenance will ensure BOTH
None required.
Bleed Air System and Environmental
Control System (ECS) Packs are
operative. In addition, Isolation
Valve is to be electrically deactivated
and verified "CLOSED". Refer to
AMM Chapters 21-51-00 and 36-1200.
An Inoperative Placard will
be placed on Isolation Valve
Switch and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
NOTE: Valve must be OPENED
manually during left engine start.
4.
Bleed Air System
Switch Capsule Lights
C
4
0
May be inoperative provided Bleed Air
System indications are available on the
Synoptic display.
None required.
None required.
An Inoperative Placard will
be placed on Bleed Air
System Switch Capsule
Lights and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
38. WATER/WASTE
Potable Water
Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 38-1
MMEL REV. NO.: 8
C
-
-
(M) Individual components may be
inoperative provided:
a) Associated components are
deactivated or isolated,
b) Associated system components are
verified not to have leaks, and
c) Passengers are advised of the
inoperative water system.
Maintenance will ensure appropriate
procedures are established to
deactivate applicable system
components and verify that
components do not have leaks.
None required.
An Inoperative Placard will
be placed on Portable Water
System and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
NOTE: Any portion of system which
operates normally may be used.
2.
Lavatory Waste
Systems (Including
Wheelchair Accessible
Lavatories)
C
-
-
(M) May be inoperative provided:
Maintenance will drain the system
a) System is drained, and
and placard the access door to
b) Procedures are established to ensure prohibit servicing.
that system is not serviced.
Flight crew may accomplish this task
if properly qualified and authorized.
None required.
An Inoperative Placard will
be placed on Portable Water
System and will be noted on
ADLS.
C
-
-
(M) Individual components may be
inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system components are
verified not to have leaks.
None required.
An Inoperative Placard will
be placed on Lavatory Waste
System and will be noted on
ADLS.
NOTE: Any portion of system which
operates normally may be used.
(continued)
Maintenance will ensure appropriate
procedures are established to
deactivate applicable system
components and verify that
components do not have leaks. If
maintenance is not available, flight
crew may perform the procedure.
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
38. WATER/WASTE
2.
PAGE NUMBER: 38-2
MMEL REV. NO.: 8
Lavatory Waste
Systems (Including
Wheelchair Accessible
Lavatories) (continued)
C
-
-
(M) Associated lavatory system(s) may be
inoperative provided:
a) Associated components are
deactivated or isolated to prevent
leaks, and
b) Associated lavatory door(s) is
secured CLOSED and placarded
“INOPERATIVE - DO NOT
ENTER.
Maintenance will ensure appropriate
procedures are established to
deactivate applicable system
components. If maintenance is not
available, flight crew may perform
the procedure.
None required.
An Inoperative Placard will
be placed on Lavatory Waste
System and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
NOTE: These provisos are not intended to
prohibit inspections by crewmembers.
3.
Lavatory Dump/Drain
System
C
-
-
May be inoperative provided:
a) Dump valve is secured in the
CLOSED and LOCKED position,
and
b) System is checked for leaks before
every flight.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4.
Vacuum Toilet
Holding Tank
Indicator
D
1
0
May be inoperative provided:
a) Tank is verified to be serviced prior
to the first flight of the day, and
b) Tank is serviced after the last flight
of the day.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
SYSTEM &
SEQUENCE
NUMBERS
45. CENTRAL MAINTENANCE
COMPUTER
1)
Maintenance Data
D
Acquisition Unit
(MDAU) (GV)
2)
Central Maintenance
Computer (CMC)
(GV-SP, GIV-X)
PAGE NUMBER: 45-1
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
1
0
C
1
0
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
May be inoperative provided all faults are
recorded after each flight.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(M) May be inoperative or missing
provided:
a) All faults are recorded after each
flight, and
b) The CMC module is replaced with
an Airflow Blockage Module
(ABM) if the CMC module is
removed from the MAU.
Maintenance will ensure CMC
module is removed for maintenance
and is replaced with an Air Blockage
Module (ABM). Refer to AMM
Chapter 31-43-13.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 46-1
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
46. NEW TECHNOLOGY
1.
Electronic Flight Bag
*** Systems (EFBs)
***
1) Class 3 EFBs
C
-
-
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will establish
alternate procedures to ensure
required information normally
provided by the EFB is
available. These alternate
procedures include using other
means to acquire data through
datalink, SATCOM or
FliteFone, or over the VHF
radio through either a FSS or
Flight Watch.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Any function, program or
document which operates normally may
be used.
D
(continued)
-
0
May be inoperative or missing provided
procedures do not require its use.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 46-2
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
46. NEW TECHNOLOGY
1.
Electronic Flight Bag
*** Systems (EFBs)
(continued)
***
***
2) Data Connectivity
(Class 2)
3) Power Connection
(Class 1 & 2)
(continued)
C
-
-
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will establish
alternate procedures to ensure
required information normally
provided by the EFB is
available. These alternate
procedures include using other
means to acquire data through
datalink, SATCOM or
FliteFone, or over the VHF
radio through either a FSS or
Flight Watch.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
May be inoperative provided procedures
do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
-
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Flight crew will establish
alternate procedures to ensure
required information normally
provided by the EFB is
available. These alternate
procedures include using other
means to acquire data through
datalink, SATCOM or
FliteFone, or over the VHF
radio through either a FSS or
Flight Watch.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 46-3
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
46. NEW TECHNOLOGY
1.
Electronic Flight Bag
*** Systems (EFBs)
(continued)
***
4) Mounting Device
(Class 2)
D
-
-
May be inoperative provided procedures
do not require its use.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(M) (O) May be inoperative provided:
a) Associated EFB and hardware is
secured by an alternate means or
removed from airplane, and
b) Alternate procedures are established
and used.
Maintenance will ensure EFB and
hardware is secured by an alternate
means or removed from airplane, and
procedures do not require its use.
Flight crew will use other means
to retrieve information provided
by data connectivity, e.g.,
datalink to obtain current
weather, uplink weather for
graphical weather etc.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
D
-
0
(M) May be inoperative provided:
a) Associated EFB and hardware is
secured by an alternate means or
removed from airplane, and
b) Procedures do not require its use.
Maintenance will ensure EFB and
hardware is secured by an alternate
means or removed from airplane, and
procedures do not require its use.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
49. AIRBORNE AUXILIARY
POWER
1.
Auxiliary Power
Unit (APU)
C
1
0
2.
APU EGT Indicators
(EICAS and Overhead)
C
2
1
C
2
0
C
2
1
C
2
0
APU Tachometers
(EICAS and Overhead)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 49-1
MMEL REV. NO.: 8
(O) Except for ER operations, may be
inoperative provided:
a) Both Engine Driven generators are
operative, and
b) Standby Electrical System is
operative.
Except for ER operations, may be
inoperative provided:
a) APU is not operated,
b) Both Engine Driven generators are
operative, and
c) Standby Electrical System is
operative.
Except for ER operations, may be
inoperative provided :
a) APU is not operated,
b) Both Engine driven generators are
operative, and
c) Standby Electrical System is
operative.
None required.
Flight crew will ensure:
a) BOTH Engine Driven
Generators are operative.
AFM, Section 2, Normal
Procedure, After Starting
Engines.
b) Standby Electrical System
is operative. (Same as a).
An Inoperative Placard will
be placed on APU
"MASTER" Switch and will
be noted on ADLS.
None required.
None required.
An Inoperative Placard will
be placed on inoperative APU
EGT indicator and will be
noted on ADLS.
None required.
None required.
An Inoperative Placard will
be placed on inoperative APU
EGT indicator and will be
noted on ADLS.
None required.
None required.
An Inoperative Placard will
be placed on inoperative APU
Tachometer indicator and will
be noted on ADLS.
None required.
None required.
An Inoperative Placard will
be placed on inoperative APU
Tachometer indicator and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 49-2
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
49. AIRBORNE AUXILIARY
POWER
4.
APU "READY" Light
System
C
1
0
May be inoperative provided APU is
operated in accordance with AFM
Limitations.
None required.
None required.
An Inoperative Placard will
be placed on APU "READY"
Light and will be noted on
ADLS.
5.
APU Remote Oil
Quantity/Servicing
System
C
1
0
May be inoperative provided oil is
checked before every flight.
None required.
None required.
An Inoperative Placard will
be placed on APU Oil
Quantity Indication System
and will be noted on ADLS.
6. APU Oil Pressure
*** Gauges
D
-
0
None required.
None required.
An Inoperative Placard will
be placed on APU Oil
Pressure Gauges and will be
noted on ADLS.
7. APU Oil Temperature
*** Gauges
D
-
0
None required.
None required.
An Inoperative Placard will
be placed on APU Oil
Temperature Gauges and will
be noted on ADLS.
8. APU Fuel Pressure
*** Gauges
D
-
0
None required.
None required.
An Inoperative Placard will
be placed on APU Fuel
Pressure Gauges and will be
noted on ADLS.
9.
C
1
0
None required.
None required.
An Inoperative Placard will
be placed on APU Start
Indicator Light and will be
noted on ADLS.
APU Start Indicator
Light
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
49. AIRBORNE AUXILIARY
POWER
APU Air Load Control
Valve
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
10.
PAGE NUMBER: 49-3
MMEL REV. NO.: 8
C
1
0
(M) May be inoperative provided valve is
verified in CLOSED position.
Maintenance will ensure APU Air
Load Valve is verified in a CLOSED
position by Butterfly Plate Shaft
Indicator.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
11.
APU External Fire
Warning Alarm (Fire
Warning Bell)
C
1
0
May be inoperative provided APU
operation is monitored in cockpit.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
12.
APU Air Inlet Door
System
C
1
0
(M) Except for ER operations, may be
inoperative provided:
a) APU Air Inlet door is secured fully
CLOSED,
b) APU is not operated,
c) Both Engine Driven Generators are
operative, and
d) Standby Electrical System is
operative.
Maintenance will ensure Air Intake
Door is secured fully CLOSED by
visually verifying door is CLOSED
and pulling and collaring the APU
door actuator circuit breaker.
Flight crew may accomplish this task
if properly qualified and authorized.
None required.
An Inoperative Placard will
be placed on APU Control
Panel and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 49-4
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
49. AIRBORNE AUXILIARY
POWER
13.
Bleed Air
Augmentation
Valve (GV, GV-SP)
C
1
0
(O) May be inoperative provided:
a) APU startng is not attempted above
FL 350, and
b) APU is operated in accordance with
AFM Limitations.
None required.
Flight crew will ensure APU
will be operated in accordance
with AFM, Section 1,
Limitations, APU Operation.
Successful airstart only below
35,000 ft.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
14.
Surge Control Valve
(GV, GV-SP)
C
1
0
(O) Except for ER operations, may be
inoperative provided:
a) APU is restricted to ground use
only at pressure altitude of 8000 ft.
or below,
b) Both Engine Generators are
operative, and
c) Standby Electrical System is
operative.
None required.
Flight crew will ensure APU is
restricted to ground use only at
P.A. < 8000 ft.
An Inoperative Placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
15.
Ignition System
Channels (GV, GV-SP)
C
2
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
16.
EGT Thermocouple
System (GV, GV-SP)
C
2
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 49-5
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
49. AIRBORNE AUXILIARY
POWER
17.
Temperature
Resistance Bulb (T2)
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
18.
Inlet Pressure
Transmitter (P2)
(GV, GV-SP)
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
19.
RPM Speed Sensor
Channels
(GV, GV-SP)
C
2
1
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
20.
APU Hour Meter
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
21.
Oil Temperature
(GV, GV-SP)
C
1
0
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
May be inoperative provided airplane is
operated in accordance with AFM
Limitations.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
49. AIRBORNE AUXILIARY
POWER
Deprime Solenoid
(GV, GV-SP)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
22.
PAGE NUMBER: 49-6
MMEL REV. NO.: 8
C
1
0
(M) May be inoperative provided airplane
is operated in accordance with AFM
Limitations.
Maintenance will verify Deprime
None required.
Solenoid is inoperative by reference
to MDAU. Maintenance will
visually check APU oil level and
perform APU start, run and shutdown
per AFM procedures.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
23.
Oil Heater
(GV, GV-SP)
24. APU Start/Engine
*** Cowl Interrupt System
C
1
0
D
1
0
May be inoperative provided airplane is
operated in accordance with AFM
Limitations.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
2. Cargo Door Operating
*** System
NUMBER REQ’D FOR DISPATCH
PROCEDURE
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
C
1
0
May be inoperative provided a
crewmember verifies by visual inspection
before each departure that the associated
door is CLOSED and LOCKED.
None required.
Flight crew will visually inspect
Door(s) to ensure they are
CLOSED and LOCKED prior to
departure. AFM, Section 2,
Normal Procedures, After
Starting Engines.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
1
0
May be inoperative provided a
crewmember verifies by visual inspection
before each departure that the associated
door is CLOSED and LOCKED.
Maintenance will OPEN and CLOSE
doors for each flight from outside
airplane.
Flight crew will ensure by
visual inspection associated
Door is CLOSED and LOCKED
before each departure. In
addition, flight crew will ensure
door is OPENED and CLOSED
by maintenance ground crew.
An Inoperative Placard will
be placed Externally and
Internally near door operating
handles and will be noted on
ADLS.
Flight crew will ensure by
visual inspection associated
Door is CLOSED and LOCKED
before each departure. In
addition, flight crew will ensure
Door is OPENED and CLOSED
by maintenance ground crew.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Flight crew may accomplish this task
if properly qualified and authorized.
3. Cargo Door Warning
*** Light System
MMEL DATE: 11/07/2014
4. MMEL REMARKS OR
EXCEPTIONS
52. DOORS
Door Warning Light
System
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 52-1
MMEL REV. NO.: 8
C
1
0
May be inoperative provided a
crewmember verifies by visual inspection
before each departure that the associated
door is CLOSED and LOCKED.
Maintenance will OPEN and CLOSE
doors for each flight from outside
airplane.
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 52-2
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
52. DOORS
4. Door Seal Pressure
*** Indicator
D
1
0
5.
Main Entry Door
Normal Operating
System
C
1
0
6.
Main Entry Door
Acoustic Curtain/
Door System
D
-
-
(O) May be inoperative provided:
a) Alternate system is operative, and
b) Main door is not CLOSED
manually.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
Flight crew will select the AUX
Hydraulic Pump ON, manually
OPEN the door control valve,
CLOSE and LOCK the main
door, and manually CLOSE the
door control valve. Refer to
AOM Volume 3 Handling and
Servicing Procedures, Section 9
item 09-03-20.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
52. DOORS
Lavatory Door
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
7.
PAGE NUMBER: 52-3
MMEL REV. NO.: 8
D
-
-
May be inoperative provided the affected
door is secured OPEN or CLOSED for
taxi, takeoff and landing.
None required.
None required.
An Inoperative Placard will
be placed on the Lavatory
Door and will be noted on
ADLS.
NOTE: Includes pop-up panels, latches,
locks and handles.
8.
Baggage Door
Warning System
C
1
0
May be inoperative provided a
crewmember verifies by visual inspection
before each departure that the baggage
door is CLOSED and LOCKED.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
9.
Main Entry Door
Warning System
C
1
0
May be inoperative provided a
crewmember verifies by visual inspection
before each departure that the Main Entry
Door is CLOSED and LOCKED.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Internal Baggage Door
Warning System
(GV, GV-SP)
C
1
0
(O) May be inoperative provided:
a) Door is confirmed to be CLOSED
and LOCKED by a crewmember
after each use, and
b) Door is placarded “DO NOT
ENTER” above 40,000 ft.
None required.
The flight crew advises the
passengers when the airplane is
at or above 40,000 ft and that
access to the baggage
compartment is not allowed.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
10.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 52-4
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
52. DOORS
11.
Internal Pocket Doors
D
-
-
May be inoperative provided the affected None required.
door is secured OPEN for taxi, takeoff and
landing.
NOTE: Includes pop-up panels, latches,
locks and handles.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
12.
Cabin Over Wing Exit
Window Warning
System
D
1
0
May be inoperative provided a
crewmember verifies by visual inspection
before each departure that the cabin exit
window internal and external locking (T)
handles in the over wing access panels are
engaged in their LOCKED position.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
71. POWERPLANT
EPA Tank Ejector
Pump
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 71-1
MMEL REV. NO.: 8
D
2
0
(M) May be inoperative provided
maintenance procedures are established to
drain tank:
a) Before the first flight of each day,
b) After three normal shutdowns, and
c) After two false (wet) starts.
Maintenance will perform procedures None required.
in accordance with AMM Chapter
71-71-02. If maintenance is not
available, flight crew may perform
the procedure.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
73. ENGINE FUEL &
CONTROL
2.
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 73-1
MMEL REV. NO.: 8
Fuel Flow
Indication Systems
1) EICAS
C
2
1
May be inoperative provided:
a) Associated EPR, LP and HP
indicating systems are operative,
and
b) Fuel Quantity indicating systems
are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2) RFMU (GV) /
MCDU (GV-SP)/
(GIV-X)
C
2
1
May be inoperative provided:
a) Associated EPR, LP and HP
indicating systems are operative,
and
b) Fuel Quantity indicating systems
are operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Fuel Low Pressure
Warning Systems
(EICAS)
C
2
1
May be inoperative provided:
a) Associated Fuel Boost Pumps are
operative, and
b) Airplane is operated at or below FL
250.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
A
2
0
(M) (O) Airplane may be dispatched with
Blue “Engine Maintenance STD (###)”
and/or “Engine Maintenance LTD”
messages displayed on EICAS provided:
a) Repairs are made in accordance
with times (hours) established by
the BR 710-A1 Time Limits
Manual (GV), chapter 5 or BR 710C4 Time Limits Manual (GV-SP),
chapter 5 (no extensions are
authorized), and
b) FADEC faults are reviewed by
flight crew before each takeoff.
NOTE: GV, GV-SP Blue “Engine
Maintenance STD (###) messages require
maintenance action within 150 hours and
Blue “Engine Maintenance LTD”
messages required maintenance action
within 500 hours.
PROCEDURE
Maintenance will ensure repairs are
made in accordance with times
(hours) established by the BR710
Type Certificate Data Sheet.
The times (hours) established for
Engine Maintenance LTD (Long
Term Dispatch) message is 500
engine hours. The times (hours)
established for Engine Maintenance
### STD (Short Term Dispatch
where ### is the number of hours
remaining) is 150 engine hours when
the fault is first logged. The hours
remaining to affect the repair are
automatically decreased by the
system as engine time is
accumulated. When the time
remaining is zero, the fault
automatically becomes a DND (Do
Not Dispatch) fault.
Flight crew may accomplish this task
if properly qualified and authorized.
(continued)
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
73. ENGINE FUEL &
CONTROL
Engine FADEC
Systems
(GV, GV-SP)
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 73-2
MMEL REV. NO.: 8
Flight crew will review the
FADEC faults prior to each
takeoff.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
73. ENGINE FUEL &
CONTROL
3.
PAGE NUMBER: 73-3
MMEL REV. NO.: 8
Engine FADEC
Systems (continued)
Engine FADEC
System
(GIV-X)
A
2
0
(M) (O) Airplane may be dispatched with
Blue “Engine Maintenance STD (###)”
and/or “Engine Maintenance LTD”
messages displayed on EICAS provided:
a) Repairs are made in accordance
with times (hours) established by
the Tay 611-8C Time Limits
Manual, chapter 5 (no extensions
are authorized), and
b) FADEC faults are reviewed by
flight crew before each takeoff.
Maintenance will ensure repairs are
made in accordance with times
(hours) established by the Tay 6118C Time Limits Manual, chapter 5.
The times (hours) established for
Engine Maintenance LTD (Long
Term Dispatch) message is 500
engine hours. The times (hours)
established for Engine Maintenance
### STD (Short Term Dispatch
where ### is the number of hours
remaining) is 150 engine hours when
NOTE: GIV-X “Blue Engine Maintenance
the fault is first logged. The hours
STD” (###) message require maintenance
remaining to effect the repair are
action within 150 hours and “Blue Engine
automatically decreased by the
Maintenance LTD” messages required
system as engine time is
maintenance action within 500 hours.
accumulated. When the time
remaining is zero, the fault
automatically becomes a DND (Do
Not Dispatch) fault.
Flight crew may accomplish this task
if properly qualified and authorized.
Flight crew will review FADEC
faults prior to each takeoff.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
74. IGNITION
1.
PAGE NUMBER: 74-1
MMEL REV. NO.: 8
Ignition Systems
1)
2)
No. 1 Igniters
No. 2 Igniters
A
2
1
May be inoperative provided:
a) Both No. 2 Igniters are operative,
b) Takeoff runway does not have
standing water, slush, or snow, and
c) Repairs are made within 150 flight
hours.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
2
0
May be inoperative provided:
a) Both No. 2 Igniters are operative,
b) Takeoff runway does not have
standing water, slush, or snow, and
c) Repairs are made within 10 flight
days.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
2
1
May be inoperative provided:
a) Both No. 1 Igniters are operative,
b) Takeoff runway does not have
standing water, slush, or snow, and
c) Repairs are made within 150 flight
hours.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
2
0
May be inoperative provided:
a) Both No. 1 Igniters are operative,
b) Takeoff runway does not have
standing water, slush, or snow, and
c) Repairs are made within 10 flight
days.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
74. IGNITION
Ignition ON
Indicator Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
2.
PAGE NUMBER: 74-2
MMEL REV. NO.: 8
C
2
0
(M) May be inoperative provided both
airstart systems are verified to be
operative before each flight.
To check the igniters: Pull the IGN
None required.
L/R #2 breaker. Select L & R airstart
ignition switches ON. Verify igniters
firing at the engines. Reset breakers.
Pull IGN L/R #1 breaker. Select L &
R airstart ignition switches ON.
Verify igniters firing at the engines.
Reset breaker when complete.
An Inoperative Placard will
be placed near affected
Ignition "ON" Light and will
be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
77. ENGINE INDICATING
HP Tachometer
Indications EICAS
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 77-1
MMEL REV. NO.: 8
C
2
1
May be inoperative on either engine
None required.
provided associated LP, EPR and Fuel
Flow Indicating Systems (EICAS or
Standby) are operative for affected engine.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Standby HP Indication may also
be inoperative on both engines.
2.
Engine Vibration
Monitor Systems
Sensors
1) Primary
Sensors
C
2
0
May be inoperative provided associated
secondary sensor system is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2) Secondary
Sensors
C
2
0
May be inoperative provided associated
primary sensor system is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
77. ENGINE INDICATING
3.
PAGE NUMBER: 77-2
MMEL REV. NO.: 8
Standby Engine
Instruments Indicating
System (RFMU)
(GV)
C
1
4.
Standby Engine
Instruments on
Multifunction Control
Display (MCDU)
(GV-SP, GIV-X)
C
1
5.
Engine Vibration
Monitoring System
B
1
0
May be inoperative provided:
a) Associated EICAS indication is
operative, and
b) All channels of both DAUs are
operative.
None required.
None required.
0
May be inoperative provided associated
EICAS indication is operative.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
0
May be inoperative provided:
a) Both Ice Detection Systems are
operative,
b) Operations are not conducted in
known or forecast icing conditions,
and
c) Crew reviews the Abnormal
Procedures for engine vibration
before each takeoff.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: Individual standby
indications may be inoperative
provided associated EICAS
indication is operative. See
individual indications for other
authorized configurations.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
78. ENGINE EXHAUST
Thrust Reversers
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 78-1
MMEL REV. NO.: 8
C
2
0
(M) May be inoperative provided:
a) Affected Thrust Reverser is
deactivated, stowed and LOCKED
in forward thrust position, and
b) Airplane is operated in accordance
with AFM Limitations and
Procedures.
May be inoperative provided:
a) Affected Thrust Reverser is
deactivated, stowed, and
LOCKED in forward thrust
position. Refer to AMM
Chapter 78-30-00.
b) Airplane is operated IAW
AFM Limitations and
Procedures.
NOTE: AFM Landing Distances are
not impacted for dry runway, refer to
AFM 01-78-10, but is affected in
wet/contaminated runway conditions,
refer to AOM 13-03-00.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 79-1
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
79. ENGINE OIL
1.
Low Oil Pressure
Warning System
C
2
1
2.
Engine Oil
Replenishment
System
D
1
0
3.
Impending Oil Filter
Bypass Indications
A
2
1
May be inoperative provided oil pressure
indication for both engines are operative.
(M) May be inoperative provided:
a) Associated oil filter bypass pop up
indicator is verified in normal
(recessed) position before each
engine start,
b) The oil filter is changed every flight
day or every 15 flight hours,
whichever occurs first,
c) The Magnetic Chip Detectors are
checked and verified to be free of
all debris,
d) Procedures are in place to ensure all
other DND (Do Not Dispatch)
messages are addressed before
dispatch, and
e) Repairs are made within three (3)
flight days.
NOTE: An amber “Engine Maintenance
Required” message will still be displayed
on the Crew Alerting System. Dispatch is
allowed with this message displayed after
complying with the required (M)
procedure.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Maintenance will ensure:
a) Associated oil filter bypass
pop up indicator is verified in
normal (recessed) position
before each engine start
b) Affected engine’s oil filter is
replaced per AMM,
c) Fault is confirmed to be on the
indication system, and
d) Procedures are in place to
ensure all other DND (Do Not
Dispatch) messages are
addressed before dispatch.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
PAGE NUMBER: 79-2
MMEL REV. NO.: 8
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
79. ENGINE OIL
4.
Oil Quantity Indication
Systems (EICAS /
Ground Service
Control Panel)
C
2
0
May be inoperative provided the engine
oil quantity is verified on the engine oil
quantity gauge before each engine start.
None required.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
5.
Oil Filter Pressure
Switch Fault
Indications
C
2
0
(M) May be inoperative provided:
a) Associated oil filter bypass pop up
indicator is verified in normal
(recessed) position before each
engine start,
b) Oil filter fault is not displayed in
MDAU (GV) or CMC (GV-SP,
GIV-X),
c) Fault is confirmed to be on the
indication system, and
d) Procedures are in place to ensure all
other DND (Do Not Dispatch)
messages are addressed before
dispatch.
Maintenance will ensure associated
None required.
oil filter bypass pop up indicator is
verified in normal (recessed) position
before each engine start.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
NOTE: An amber “Engine Maintenance
Required” message will still be displayed
on the Crew Alerting System. Dispatch is
allowed with this message displayed after
complying with the required (M)
procedure.
Flight crew may accomplish this task
if properly qualified and authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
2.
Auto Start System
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
80. STARTING
Engine Starting
Systems
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
1.
PAGE NUMBER: 80-1
MMEL REV. NO.: 8
C
C
2
2
0
0
(M) (O) May be inoperative provided:
a) Airstart Ignition System is
operative,
b) Start Valve has not failed in OPEN
position,
c) Start Valve is manually OPENED
and CLOSED for engine starting,
d) Airstart Ignition, Engine Selector
and Start Switches are switched to
OFF when engine has reached selfsustaining speed, and
e) Engine start is accomplished in
accordance with AFM Engine Start
Valve Fails To Open Procedure.
Maintenance will ensure:
a) Start Valve has not failed in
OPEN position,
b) Start Valve is manually
OPENED and CLOSED for
engine starting,
c) Airstart (Continuous) Ignition,
Engine Selector and Start
Switches are switched to OFF
when engine has reached self
sustaining speed, and
d) The Airstart Ignition System is
operative.
May be inoperative provided:
a) Alternate start system is operative,
and
b) AFM procedures for alternate
engine start are used to start
engines.
None required.
The flight crew may perform this
task if properly qualified and
authorized.
Flight crew will ensure:
a) Start Valve has not failed
in OPEN position.
b) Start Valve is manually
OPENED and CLOSED
for engine starting.
c) Airstart (Continuous)
Ignition, Engine Selector
and Start Switches are
switched to OFF when
engine has reached selfsustaining speed.
d) Engine Start is
accomplished in
accordance with AFM,
Section 3, Abnormal
Procedures, Engine
Starting System.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
An Inoperative Placard will
be displayed in a prominent
position to be seen by the
flight crew and will be noted
on the ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
5. MAINTENANCE
3.
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
NUMBER REQ’D FOR DISPATCH
PROCEDURE
6. OPERATIONAL
7. PLACARDING
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
80. STARTING
Start Valve Position
Indication
MOP REV. NO.: 8
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
3.
PAGE NUMBER: 80-2
MMEL REV. NO.: 8
C
C
2
2
0
0
(M) May be inoperative provided:
a) Start Valve has not failed in OPEN
position as verified by visual means
through an access panel,
b) Ignition ON indication is operative
during engine start, and
c) Start Valve is verified CLOSED
following engine start by visual
means.
Maintenance will ensure:
a) Start Valve has not failed in
OPEN position,
b) Airstart ignition is operative,
c) Start Valve is manually
OPENED and CLOSED for
engine starting.
(M) (O) May be inoperative provided:
a) Airstart Ignition System is
operative,
b) Start Valve has not failed in OPEN
position,
c) Start Valve is manually OPENED
and CLOSED for engine starting,
d) Airstart Ignition, Engine Selector
and Start Switches are switched to
OFF when engine has reached selfsustaining speed, and
e) Engine start is accomplished in
accordance with AFM Engine Start
Valve Fails To Open Procedure.
Maintenance will ensure:
a) Start Valve has not failed in
OPEN position,
b) Start Valve is manually
OPENED and CLOSED for
engine starting,
c) Airstart (Continuous) Ignition,
Engine Selector and Start
Switches are switched to OFF
when engine has reached self
sustaining speed, and
d) The Airstart Ignition System is
operative.
None required.
An Inoperative Placard will
be placed on Start Valve
Position Indicator and will be
noted on ADLS.
Flight crew will comply with
QRH procedures for Manually
Overriding Starter Air Valve
OM-09-03-40 found under
Alternate Normal Procedures
tab.
An Inoperative Placard will
be placed on Start Valve
Position Indicator and will be
noted on ADLS.
The flight crew may perform this
task if properly qualified and
authorized.
The flight crew may perform this
task if properly qualified and
authorized.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350)
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
1.
MOP REV. NO.: 8
MMEL DATE: 11/07/2014
MOP DATE: 11/07/2014
6. OPERATIONAL
7. PLACARDING
2. NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
5. MAINTENANCE
3.
NUMBER REQ’D FOR DISPATCH
PROCEDURE
PROCEDURE
PROCEDURE
4. MMEL REMARKS OR
EXCEPTIONS
80. STARTING
4. Start Valve
*** Position Indicator
Lights
PAGE NUMBER: 80-3
MMEL REV. NO.: 8
C
2
0
(M) May be inoperative provided:
a) Start Valve has not failed in OPEN
position as verified by visual means
through an access panel,
b) Start Valve is manually OPENED
and CLOSED for engine starting in
accordance with AFM Start Valve
Failure procedures, and
c) Airstart Ignition, Engine Selector
and Start switches are switched to
the OFF position when engine has
reached self-sustaining speed.
Maintenance will ensure
a) Start Valve has not failed in
OPEN position,
b) Start Valve is manually
OPENED and CLOSED for
engine starting,
c) Airstart (Continuous) Ignition,
Engine Selector and Start
Switches are switched to OFF
when engine has reached self
sustaining speed, and
d) The Airstart Ignition System is
operative.
The flight crew may perform this
task if properly qualified and
authorized.
None Required.
An Inoperative Placard will
be placed on Start Valve
Position Indicator Lights and
will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
PAGE NO:
2-1
SECTION TWO
CREW ALERTING SYSTEM
(CAS) MESSAGE RELIEF
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
PAGE NO:
2-2
STATEMENT PAGE
1. Section Two of the MMEL will list only Crew Alerting system (CAS) messages meeting the following requirements:
a. Equipment failure indications(s) that can be used to determine the airworthiness status of the airplane.
b. Messages that the crew can act upon with simple troubleshooting procedures without the assistance of a mechanic, and for which the crew
has been trained.
c. Messages using the new self-diagnostic technology (virtual) actions for which the crew has been trained.
2.
CAS message relief items not meeting these requirements will be listed in Section One of the MMEL.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
A/P TRIM PWR FAIL
(O)
Airplane may be dispatched with one (1)
elevator trim servo inoperative provided the
inoperative trim servo circuit breaker(s) is
pulled and collared.
B
(O)
Airplane may be dispatched provided
affected A/T system is confirmed
disengaged.
B
(O)
Airplane may be dispatched provided
affected A/T system is confirmed
disengaged.
Flight crew will confirm affected
A/T system is disengaged.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
ACS Default Mode, L-R
Operational Procedures
B
(Blue – Advisory)
A/T 1-2 TQA Power Fail
2-3
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
A/T 1-2 FAIL
PAGE NO:
Flight crew will ensure
inoperative A/P SERVO #1:
POP, D-4 or A/P SERVO #2:
CPOP, D-4 servo circuit breaker
is pulled and collared.
Flight crew will confirm affected
A/T system is disengaged.
(Blue – Advisory)
(GV-SP/GIV-X)
ACS DEFLT MODE, L-R
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
ACS Fail, L-R
2.
PAGE NO:
2-4
3.
Limitations and/or Procedures
Operational Procedures
B
Except for ER operations, airplane may be
dispatched in the pressurized configuration
with a single pack inoperative provided:
a) Inoperative ECS Pack is selected
OFF,
b) Bleed Air Isolation Valve is CLOSED
and OPERATIVE,
c) Right Main TRU is operative,
d) Airplane is operated in accordance
with AFM Limitations,
e) Airplane is operated at or below
FL410, and
f) Autothrottles must be operative and
engaged at or above FL400.
None required.
B
Except for ER operations, airplane may be
dispatched in the unpressurized
configuration with both packs inoperative
provided the outflow valve is operative.
None required.
(Amber – Caution)
(GV-SP/GIV-X)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
ACS FAIL, L-R
2.
PAGE NO:
2-5
3.
Limitations and/or Procedures
Operational Procedures
B
Except for ER operations, airplane may be
dispatched in the pressurized configuration
with a single pack inoperative provided:
a) Inoperative ECS Pack is selected
OFF,
b) Bleed Air Isolation Valve is CLOSED
and OPERATIVE,
c) Right Main TRU is operative,
d) Airplane is operated in accordance
with AFM Limitations,
e) Airplane is operated at or below
FL410, and
f) Autothrottles must be operative and
engaged at or above FL400.
None required.
B
Except for ER operations, airplane may be
dispatched in the unpressurized
configuration with both packs inoperative
provided the outflow valve is operative.
None required.
(Amber – Caution)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ACS Maintenance, L-R
(Blue – Advisory)
(GV-SP/GIV-X)
Operational Procedures
C
(O)
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative, and
d) Autopilot is operative.
Flight crew will ensure:
a) Manual Pressurization
Control System is operative,
b) Cabin Altitude and
Differential Pressure
Indicators are operative,
c) Cabin Rate of Climb
Indicator is operative, and
d) Autopilot is operative.
C
(O)
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative, and
d) Autopilot is operative.
Flight crew will ensure:
a) Manual Pressurization
Control System is operative,
b) Cabin Altitude and
Differential Pressure
Indicators are operative,
c) Cabin Rate of Climb
Indicator is operative, and
d) Autopilot is operative.
Airplane may be dispatched provided
system is not required by 14 CFR.
None required.
(Blue – Advisory)
(GV)
ADF 1-2 Fail
2-6
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
ACS MAINT REQD, L-R
PAGE NO:
B
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ADM1-3 Probe Heat Fail
(Blue – Advisory)
(GV-SP)
2-7
3.
Limitations and/or Procedures
Operational Procedures
A
(O)
Except for ER operations, airplane may be
dispatched with one (1) probe heater
inoperative provided:
a) Airplane is not operated in visible
moisture or known or forecast icing
conditions,
b) Flight crew select ADS sources that
are different and not associated with
failed pitot heater element, and
c) Repairs are made within two (2) flight
days.
Flight crew will select ADS
sources that are different and not
associated with failed pitot heater
element and transfer transponder
to an operable ADM.
A
(O)
Except for ER operations, airplane may be
dispatched with one (1) probe heater
inoperative provided:
a) Airplane is not operated in visible
moisture or known or forecast icing
conditions,
b) Flight crew select ADS sources that
are different and not associated with
failed pitot heater element, and
c) Repairs are made within two (2) flight
days.
Flight crew will select ADS
sources that are different and not
associated with failed pitot heater
element.
(Blue – Advisory)
(GV-SP)
ADM2 Stby Probe Heat Fail
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ADS 1-2 Probe Heat Fail
(Blue – Advisory)
(GIV-X)
(O)
2-8
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) probe heater
inoperative provided:
a) Airplane is not operated in visible
moisture or known or forecast icing
conditions,
b) Flight crew select ADS sources that
are different and not associated with
failed pitot heater element, and
c) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will select ADS
sources that are different and not
associated with failed pitot heater
element.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ADS 1-2-3 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2-9
3.
Limitations and/or Procedures
B
PAGE NO:
Operational Procedures
Airplane may be dispatched with a single
Flight crew will pull and collar
air data system inoperative provided:
ADM #1: POP B-8, ADM #2:
a) Manual Pressurization Control System CPOP B-8 and ADM #3: POP Bis operative,
9 circuit breakers associated with
b) Cabin Altitude and Differential
the ADS failure.
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations,
f) ADM #1: POP B-8, ADM #2: CPOP B8 and ADM #3: POP B-9 circuit
breakers associated with ADS failure
is pulled and collared, and
g) Flight crew selects operative and
different ADS sources prior to
departure.
NOTE 1: Two systems are required for operation in RVSM airspace.
NOTE 2: Transponder and Flight Director / Autopilot must use same ADC data
for RVSM.
NOTE 3: For ADS 1 Fail, expect the L Engine Backup Air Data advisory and
associated Engine Maintenance message to post.
NOTE 4: For ADS 2 Fail, expect the R Engine Backup Air Data advisory and
associated Engine Maintenance message to post.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ADS 3 Stby Probe Heat Fail
A
(O)
2 - 10
3.
Limitations and/or Procedures
(Blue – Advisory)
(GIV-X)
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) probe heater
inoperative provided:
a) Airplane is not operated in visible
moisture or known or forecast icing
conditions,
b) Flight crew selects ADS sources that
are different and not associated with
failed pitot heater element, and
c) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will select ADS
sources that are different and not
associated with failed pitot heater
element.
NOTE: Standby instruments and ADS 3
may be unreliable.
ADS-B Fail
(Blue – Advisory)
(GV-SP/GIV-X)
A
Airplane may be dispatched provided:
a) Operations do not require its use, and
b) Repairs are made before completion
of next heavy maintenance visit.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Aft Cabin Temp Fan Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 11
3.
Limitations and/or Procedures
C
PAGE NO:
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
Forward Cabin Temp Fan Fail;
Cockpit Temp Fan Fail;
b) Aft Cabin Temperature Manual mode
is operative,
c) Associated temperature indicator is
operative,
d) AFT CABIN SENSOR FAN, LEER E9, is pulled and collared, and
e) Flight crew monitor aft cabin
temperature and aft cabin duct
temperature.
Operational Procedures
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
Forward Cabin Temp
Fan Fail;
Cockpit Temp Fan Fail,
b) Aft Cabin Temperature
Manual mode is operative,
c) Associated temperature
indicator is operative,
d) AFT CABIN SENSOR FAN
circuit breaker: LEER E-9 is
pulled and collared, and
e) Aft cabin temperature and
aft cabin duct temperature
are monitored.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
AFT CABIN TMP FAN FL
C
AGM 1-2-3-4 DMU Charts Fail
(Blue – Advisory)
(GV-SP/GIV-X)
C
(O)
2 - 12
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
PAGE NO:
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
Forward Cabin Temp Fan Fail;
Cockpit Temp Fan Fail;
b) Aft Cabin Temperature Manual mode
is operative,
c) Associated temperature indicator is
operative,
d) AFT CABIN SENSOR FAN, LEER E9, is pulled and collared, and
e) Flight crew monitor aft cabin
temperature and aft cabin duct
temperature.
Operational Procedures
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
Forward Cabin Temp
Fan Fail;
Cockpit Temp Fan Fail,
b) Aft Cabin Temperature
Manual mode is operative,
c) Associated temperature
indicator is operative,
d) AFT CABIN SENSOR FAN
circuit breaker: LEER E-9 is
pulled and collared, and
e) Aft cabin temperature and
aft cabin duct temperature
are monitored.
Airplane may be dispatched provided:
None required.
a) Current aeronautical charts are carried
onboard the airplane and available to
the flight crew, and
b) Airplane is operated in accordance
with AFM Limitations.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
AGM 1-2-3-4 Fail
B
AIU 1-2 FAIL
(Blue – Advisory)
(GV)
A
(O)
2 - 13
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
Airplane may be dispatched with one AGM Flight crew will ensure:
inoperative provided:
a) The inoperative AGM is
a) The inoperative AGM is electronically
electronically switched to the
switched to the AGM 3 position
number 3 position resulting
resulting in DU3 red Xing,
in DU3 red Xing,
b) DU3 is dimmed to eliminate the Red X,
b) DU 3 is dimmed to eliminate
and
the Red X,
c) Crew actions for subsequent failures
c) Crew actions for
are established.
subsequent failures are
established, and
d) Crew will discuss the
alternate procedures for
sharing displays including if
a display fails during any
phase of flight especially
takeoff, approach, landing
and go-around.
Airplane may be dispatched with one AIU
inoperative provided:
a) Operations do not require use of HF
radio, and
b) Repairs are made within two (2) flight
days.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Alternate Pump Fail, L-R
(Amber – Caution)
(GIV-X)
2 - 14
3.
Limitations and/or Procedures
Operational Procedures
B
(O)
Except for ER operations, airplane may be
dispatched with a single pump inoperative
provided:
a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning
Systems are operative,
d) Flight crew comply with AFM, Section
3, Abnormal Procedures, Fuel Boost
Pump Failure, and
e) Airplane is operated in accordance
with AFM Limitations.
Flight crew will ensure:
a) Fuel Crossflow Valve and
Intertank Valve are
operative,
b) BOTH Fuel Low Quantity
Warning Systems are
operative, and
c) Verify compliance with AFM,
Section 3, Abnormal
Procedures, Fuel Boost
Pump Failure.
B
(O)
Except for ER operations, airplane may be
dispatched with a single pump inoperative
provided:
a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning
Systems are operative,
d) Flight crew comply with AFM, Section
3, Abnormal Procedures, Fuel Boost
Pump Failure, and
e) Airplane is operated in accordance
with AFM Limitations.
Flight crew will ensure:
a) Fuel Crossflow Valve and
Intertank Valve are
operative,
b) BOTH Fuel Low Quantity
Warning Systems are
operative, and
c) Verify compliance with AFM,
Section 3, Abnormal
Procedures, Fuel Boost
Pump Failure
(Amber – Caution)
(GV-SP)
Alt FuelPump Fail, L-R
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ALT PUMP FAIL, L-R
(Amber – Caution)
(GV)
(O)
2 - 15
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched with a single pump inoperative
provided:
a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning
Systems are operative,
d) Flight crew comply with AFM,
Section 3, Abnormal Procedures,
Fuel Boost Pump Failure, and
e) Airplane is operated in accordance
with AFM Limitations.
Operational Procedures
Flight crew will ensure:
a) Fuel Crossflow Valve and
Intertank Valve are
operative,
b) BOTH Fuel Low Quantity
Warning Systems are
operative, and
c) Verify compliance with AFM,
Section 3, Abnormal
Procedures, Fuel Boost
Pump Failure
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Antiskid Fail
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 16
3.
Limitations and/or Procedures
B
PAGE NO:
Airplane may be dispatched provided:
a) ANTI-SKID is selected “OFF”,
b) Anti-skid off braking procedures, AFM
Section 3, Abnormal Procedures, AntiSkid Failure are followed,
c) No WOW Power Faults exist,
d) If Auto mode of the AUX Hydraulic
Pump is inoperative, AUX pump is
selected ON for takeoff and landing,
and
e) Airplane is operated in accordance
with AFM Limitations.
NOTE: Anti-Skid inoperative AFM
performance penalties must be applied.
Refer to AFM, Section 5, Performance,
Reference Accelerate-Stop Distance.
Operational Procedures
Flight crew will ensure airplane is
operated in accordance with
AFM, Limitations. Flight crew will
select ANTI-SKID “OFF” and
follow Anti-Skid Off Braking
Procedures. AFM, Section 3,
Abnormal Procedures, Anti-Skid
Failure.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ANTISKID FAIL
(Amber – Caution)
(GV)
(O)
2 - 17
3.
Limitations and/or Procedures
B
PAGE NO:
Airplane may be dispatched provided:
a) ANTI-SKID is selected “OFF”,
b) Anti-skid off braking procedures, AFM
Section 3, Abnormal Procedures, AntiSkid Failure are followed,
c) No WOW Power Faults exist,
d) If Auto mode of the AUX Hydraulic
Pump is inoperative, AUX pump is
selected ON for takeoff and landing,
and
e) Airplane is operated in accordance
with AFM Limitations.
NOTE: Anti-Skid inoperative AFM
performance penalties must be applied.
Refer to AFM, Section 5, Performance,
Reference Accelerate-Stop Distance.
Operational Procedures
Flight crew will ensure airplane is
operated in accordance with
AFM, Limitations. Flight crew will
select ANTI-SKID “OFF” and
follow Anti-Skid Off Braking
Procedures. AFM, Section 3,
Abnormal Procedures, Anti-Skid
Failure.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
AP 1-2 Fail
B
(O)
2 - 18
3.
Limitations and/or Procedures
(Amber – Caution)
(GV-SP/GIV-X)
PAGE NO:
Except for ER operations or where en route
operations or approach minimums require
its use, Airplane may be dispatched with
one (1) Autopilot inoperative provided the
airplane is operated in accordance with
AFM Limitations in the event operative
FGC fails and Yaw Damper is inoperative.
Operational Procedures
Flight crew will operate the
airplane in accordance AFM
limitations in the event the
operative FGC fails and the Yaw
Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM,
RNP and PRNAV operations.
AP 1-2 Power Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
(O)
Except for ER operations or where en route
operations or approach minimums require
its use, Airplane may be dispatched with
one (1) inoperative provided airplane is
operated in accordance with AFM
Limitations in the event operative FGC fails
and Yaw Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM,
RNP and PRNAV operations.
Flight crew will operate airplane
in accordance with AFM
limitations in the event the FGC
fails and the Yaw Damper is
inoperative.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
AP/Trim Fail
B
APM 1-2-3-4 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
(O)
2 - 19
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
Airplane may be dispatched with one (1)
elevator trim servo inoperative provided the
inoperative trim servo circuit breaker(s) is
pulled and collared.
G550: Flight crew will ensure
inoperative PITCH TRIM SERVO
#1: POP, E-2 or PITCH TRIM
SERVO #2: CPOP, E-1 servo
circuit breaker is pulled and
collared.
G450: Flight crew will ensure
inoperative PITCH TRIM SERVO
#1: POP, E-2 or PITCH TRIM
SERVO #2: CPOP, E-1 servo
circuit breaker is pulled and
collared.
Airplane may be dispatched with one (1)
APM inoperative.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
APU Fail
(Amber – Caution)
(GV-SP/GIV-X)
Operational Procedures
B
(O)
Except for ER operations, airplane may be
dispatched provided:
a) Both Engine Driven generators are
operative, and
b) Standby Electrical System is
operative.
Flight crew will ensure:
a) BOTH Engine Driven
Generators are operative.
b) Standby Electrical system is
operative.
B
(O)
Except for ER operations, airplane may be
dispatched provided:
a) Both Engine Driven generators are
operative, and
b) Standby Electrical System is
operative.
Flight crew will ensure:
a) BOTH Engine Driven
Generators are operativ
b) Standby Electrical system is
operative.
B
(O)
Except for ER operations, airplane may be
dispatched provided:
a) APU is considered inoperative,
b) Both engine driven generators are
operative,
c) Standby electrical system is
operative, and
d) APU CONT #1 and APU CONT #2
circuit breakers are pulled and
collared.
Flight crew will pull and collar
APU CONT #1 and APU CONT
#2 circuit breakers. Flight crew
will ensure:
a) Both Engine Generators are
operative.
b) Standby Electrical Power
System is operative.
(Amber – Caution)
(GV)
APU Fire Bottle Discharge
2 - 20
3.
Limitations and/or Procedures
(Amber – Caution)
(GV-SP/GIV-X)
APU FAIL
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
APU Fire Detector Fail
(Amber – Caution)
(GV)
2 - 21
3.
Limitations and/or Procedures
Operational Procedures
B
(O)
Except for ER operations, airplane may be
dispatched provided:
a) APU is not used, and
b) APU CONT #1 and APU CONT #2
circuit breakers are pulled and
collared.
Flight crew will ensure APU
CONT #1 and APU CONT #2
circuit breakers are pulled and
collared.
B
(O)
Except for ER operations, airplane may be
dispatched provided:
a) APU is not used, and
b) APU CONT #1 and APU CONT #2
circuit breakers are pulled and
collared.
Flight crew will ensure APU
CONT #1 and APU CONT #2
circuit breakers are pulled and
collared.
(Amber – Caution)
(GV-SP/GIV-X)
APU FIRE DET FAIL
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
APU GCU Fail
(Blue – Advisory)
(GV)
2 - 22
3.
Limitations and/or Procedures
Operational Procedures
A
(O)
Except for ER operations, airplane may be
dispatched provided:
a) APU GCU PWR circuit breaker on left
EER, G-11 is pulled and collared,
b) Both Engine Driven generators are
operative as verified by reference to
the AC synoptic and the absence of
failure messages on CAS,
c) Standby Electrical System is
operative, and
d) Repairs are made within two (2) flight
days.
Flight crew will ensure:
a) APU GCU PWR circuit
breaker on left EER, G-11 is
pulled and collared,
b) BOTH Engine Driven
Generators are operative by
reference to the AC synoptic
and the absence of failure
message on CAS, and
c) Standby Electrical System is
operative.
A
(O)
Except for ER operations, airplane may be
dispatched provided:
a) APU GCU PWR circuit breaker on left
EER, G-11 is pulled and collared,
b) Both Engine Driven generators are
operative as verified by reference to
the AC synoptic and the absence of
failure messages on CAS,
c) Standby Electrical System is
operative, and
d) Repairs are made within two (2) flight
days.
Flight crew will ensure:
a) APU GCU PWR circuit
breaker on left EER, G-11 is
pulled and collared,
b) BOTH Engine Driven
Generators are operative by
reference to the AC synoptic
and the absence of failure
message on CAS, and
c) Standby Electrical System is
operative.
(Blue – Advisory)
(GV-SP/GIV-X)
APU GCU FAIL
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
APU Generator Fail
A
APU Generator Maint Reqd
(Blue – Advisory)
(GV-SP/GIV-X)
C
(O)
2 - 23
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
Except for ER operations, airplane may be
dispatched provided:
a) APU GCU PWR circuit breaker on left
EER, G-11 is pulled and collared,
b) Both Engine Driven generators are
operative as verified by reference to
the AC synoptic and the absence of
failure messages on CAS, and
c) Standby Electrical System is
operative.
Flight crew will ensure:
a) APU GCU PWR circuit
breaker on left EER, G-11 is
pulled and collared,
b) BOTH Engine Driven
Generators are operative by
reference to the AC synoptic
and the absence of failure
message on CAS, and
c) Standby Electrical System is
operative.
Airplane may be dispatched.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
APU GEN FAIL
APU GEN MAINT REQD
Operational Procedures
Except for ER operations, airplane may be
dispatched provided:
a) APU GCU PWR circuit breaker on left
EER, G-11 is pulled and collared,
b) Both Engine Driven generators are
operative as verified by reference to
the AC synoptic and the absence of
failure messages on CAS, and
c) Standby Electrical System is
operative.
Flight crew will ensure:
a) APU GCU PWR circuit
breaker on left EER, G-11 is
pulled and collared,
b) BOTH Engine Driven
Generators are operative by
reference to the AC synoptic
and the absence of failure
message on CAS, and
c) Standby Electrical System is
operative.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV)
(O)
2 - 24
3.
Limitations and/or Procedures
A
PAGE NO:
(Blue – Advisory)
(GV)
APU Maintenance Required
(Blue – Advisory)
(GV-SP/GIV-X)
APU MAINT REQD
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
APU Shutoff Valve Fail
B
ATC 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
C
(O)
2 - 25
3.
Limitations and/or Procedures
(Amber – Caution)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
Except for ER operations, may be
inoperative provided:
a) Both Engine Driven generators are
operative,
b) Standby Electrical System is
operative, and
c) APU is not used.
Flight crew will ensure:
a) BOTH Engine Driven
Generators are operative.
b) Standby Electrical system is
operative.
Airplane may be dispatched with any in
excess of those required by 14 CFR
inoperative.
None required.
NOTE 1: Flight Director, Autopilot, and
Transponder must use the same Air Data
source for flight into RVSM airspace.
NOTE 2: Transponder and altitude
reporting capability must be operative for
flight into RVSM airspace.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAROSET 1 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 26
3.
Limitations and/or Procedures
C
PAGE NO:
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
1. ADS 2 Fail
2. ADS 3 Fail
3. BAROSET 2 Fail
4. BAROSET 3 Fail
b) Manual Pressurization Control System
is operative,
c) Cabin Altitude and Differential
Pressure Indicators are operative,
d) Cabin Rate of Climb Indicator is
operative,
e) Flight crew select ADS sources that
are independent and not associated
with the BAROSET failure,
f) Autopilot is operative, and
g) Airplane is operated in accordance
with AFM Limitations.
Operational Procedures
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
1. ADS 2 Fail
2. ADS 3 Fail
3. BAROSET 2 FAIL
4. BAROSET 3 FAIL
b) Manual Pressurization
Control System is operative,
c) Cabin Altitude and
Differential Pressure
Indicators are operative,
d) Cabin Rate of Climb
Indicator is operative,
e) Flight crew select ADS
sources that are
independent and not
associated with the
BAROSET failure,
f) Autopilot is operative, and
NOTE 1: Two systems are required for
g) Airplane is operated in
operation in RVSM airspace.
accordance with AFM
NOTE 2: Transponder and Flight
Limitations.
Director/Autopilot must use same ADC data
for RVSM.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAROSET 2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 27
3.
Limitations and/or Procedures
C
PAGE NO:
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
1. ADS 1 Fail
2. ADS 3 Fail
3. BAROSET 1 Fail
4. BAROSET 3 Fail
b) Manual Pressurization Control System
is operative,
c) Cabin Altitude and Differential
Pressure Indicators are operative,
d) Cabin Rate of Climb Indicator is
operative,
e) Flight crew select ADS sources that
are independent and not associated
with the BAROSET failure,
f) Autopilot is operative, and
g) Airplane is operated in accordance
with AFM Limitations.
Operational Procedures
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
1. ADS 1 Fail
2. ADS 3 Fail
3. BAROSET 1 FAIL
4. BAROSET 3 FAIL
b) Manual Pressurization
Control System is operative,
c) Cabin Altitude and
Differential Pressure
Indicators are operative,
d) Cabin Rate of Climb
Indicator is operative,
e) Flight crew select ADS
sources that are
independent and not
associated with the
BAROSET failure,
f)
Autopilot is operative, and
NOTE 1: Two systems are required for
g) Airplane is operated in
operation in RVSM airspace.
accordance with AFM
NOTE 2: Transponder and Flight
Limitations.
Director/Autopilot must use same ADC data
for RVSM.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAROSET 3 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 28
3.
Limitations and/or Procedures
C
PAGE NO:
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
1. ADS 1 Fail
2. ADS 2 Fail
3. BAROSET 1 Fail
4. BAROSET 2 Fail
b) Manual Pressurization Control System
is operative,
c) Cabin Altitude and Differential
Pressure Indicators are operative,
d) Cabin Rate of Climb Indicator is
operative,
e) Flight crew select ADS sources that
are independent and not associated
with the BAROSET failure,
f) Autopilot is operative, and
g) Airplane is operated in accordance
with AFM Limitations.
Operational Procedures
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
1. ADS 1 Fail
2. ADS 2 Fail
3. BAROSET 1 FAIL
4. BAROSET 2 FAIL
b) Manual Pressurization
Control System is operative,
c) Cabin Altitude and
Differential Pressure
Indicators are operative,
d) Cabin Rate of Climb
Indicator is operative,
e) Flight crew select ADS
sources that are
independent and not
associated with the
BAROSET failure,
f) Autopilot is operative, and
NOTE 1: Two systems are required for
g) Airplane is operated in
operation in RVSM airspace.
accordance with AFM
NOTE 2: Transponder and Flight
Limitations.
Director/Autopilot must use same ADC data
for RVSM.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
BAS Default Mode, L-R
2.
PAGE NO:
2 - 29
3.
Limitations and/or Procedures
Operational Procedures
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
BAS DEFLT MODE, L-R
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAS Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
(continued)
(O)
2 - 30
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched in the pressurized configuration
with one Bleed Air System inoperative
provided
(GV-SP):
a) Inoperative Bleed Control Valve is
CLOSED and deactivated electrically
when associated Engine Bleed Air
System is selected OFF as follows:
1. Affected Bleed Air Valve is
selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTIICE: REER, D-13 or L BLEED AIR
CONT: LEER, E-10 and L WING
ANTI-ICE: LEER, D-4 circuit
breakers are pulled and collared.
b) Opposite Engine Bleed Air System is
operative,
c) Isolation Valve is verified to be
operative and selected OPEN, and
d) Airplane is operated in accordance
with AFM Limitations.
NOTE: Auto-throttle will be inoperative with
Isolation Valve OPEN.
Operational Procedures
GV-SP pressurized
configuration:
Flight crew will CLOSE
inoperative Bleed Control Valve
and electrically deactivate
affected system.
If failure occurs with
1) Right Bleed Air Control Valve:
Select Right Bleed Air Valve OFF
utilizing R Eng Bleed Air Switch
and Pull R Bleed CONT Circuit
Breaker (CB).
2) Left Bleed Air Control Valve:
Select Left Bleed Air Valve OFF
utilizing L Eng Bleed Air Switch
and Pull Left Bleed CONT Circuit
Breaker (CB).
In addition, opposite Engine
Bleed Air Sytem will be verified
operative and Isolation Valve will
be selected OPEN.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAS Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
(O)
(GIV-X):
a) Inoperative Bleed Control Valve is
CLOSED and deactivated electrically
when associated Engine Bleed Air
System is selected OFF as follows:
1. Affected Bleed Air Valve is
selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTIICE: REER, D-13 or L BLEED AIR
CONT: LEER, E-10 and L WING
ANTI-ICE: LEER, D-4 circuit
breakers are pulled and collared.
b) Opposite Engine Bleed Air System is
operative,
c) Isolation Valve is verified to be
operative and selected OPEN,
d) Airplane is not operated in forecast or
known icing conditions, and
e) Airplane is operated in accordance
with AFM Limitations.
NOTE: Auto-throttle will be inoperative with
Isolation Valve OPEN.
(continued)
2 - 31
3.
Limitations and/or Procedures
B
PAGE NO:
Operational Procedures
GIV-X pressurized
configuration:
Flight crew will CLOSE
associated Bleed Control Valve
and electrically deactivate
affected system.
In addition, opposite Engine
Bleed Air Sytem and Isolation
Valve will be verified operative
and Isolation Valve selected
OPEN
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAS Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
(continued)
(O)
2 - 32
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched in the unpressurized configuration
with both Bleed Air Systems inoperative
provided
(GV-SP):
a) Inoperative Bleed Control Valve is
CLOSED and deactivated electrically
when associated Engine Bleed Air System
is selected OFF as follows:
1. Affected Bleed Air Valve is selected
OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTI-ICE:
REER, D-13 or L BLEED AIR CONT:
LEER, E-10 and L WING ANTI-ICE:
LEER, D-4 circuit breakers are pulled
and collared.
b) Manual pressurization control is selected,
c) Outflow valve is slewed to the full OPEN
position,
d) RAM Air is selected ON,
e) Cabin differential pressure is monitored to
be nominally zero psid during the flight,
f) Airplane is not operated in known or
forecast icing conditions, and
g) Airplane is operated in accordance with
AFM Limitations.
Operational Procedures
For GV-SP unpressurized
configuration:
Flight crew will ensure inoperative
Bleed Control Valve is CLOSED and
deactivated electrically.
To operate the airplane
unpressurized, select manual
pressurization and slew the outflow
valve to the full open position with
RAM air selected ON. Monitor
cabin differential pressure to be
nominally zero psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAS Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 33
3.
Limitations and/or Procedures
B
PAGE NO:
(GIV-X):
a) Affected Valve(s) are verified
CLOSED,
b) Manual pressurization control is
selected,
c) Outflow valve is slewed to the full
OPEN position,
d) RAM Air is selected ON,
e) Cabin differential pressure is
monitored to be nominally zero psid
during the flight,
f) Airplane is not operated in forecast or
known icing conditions, and
g) Airplane is operated in accordance
with AFM Limitations.
Operational Procedures
For GIV-X unpressurized
configuration:
Flight crew will ensure all
affected Valve(s) are verified
CLOSED.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to the full open
position with RAM air selected
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAS FAIL, L-R
(Amber – Caution)
(GV)
(continued)
(O)
2 - 34
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched in the pressurized configuration
with one Bleed Air System inoperative
provided
(GV):
a) Inoperative Bleed Control Valve is
CLOSED and deactivated electrically
when associated Engine Bleed Air
System is selected OFF as follows:
1. Affected Bleed Air Valve is
selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTIICE: REER, D-13 or L BLEED AIR
CONT: LEER, E-10 and L WING
ANTI-ICE: LEER, D-4 circuit
breakers are pulled and collared.
b) Opposite Engine Bleed Air System is
operative,
c) Isolation Valve is verified to be
operative and selected OPEN, and
d) Airplane is operated in accordance
with AFM Limitations.
NOTE: Auto-throttle will be inoperative with
Isolation Valve OPEN.
Operational Procedures
GV pressurized configuration:
Flight crew will CLOSE
inoperative Bleed Control Valve
and electrically deactivate
affected system.
If failure occurs with
1) Right Bleed Air Control Valve:
Select Right Bleed Air Valve OFF
utilizing R Eng Bleed Air Switch
and Pull R Bleed CONT Circuit
Breaker (CB).
2) Left Bleed Air Control Valve:
Select Left Bleed Air Valve OFF
utilizing L Eng Bleed Air Switch
and Pull Left Bleed CONT Circuit
Breaker (CB).
In addition, opposite Engine
Bleed Air Sytem will be verified
operative and Isolation Valve will
be selected OPEN.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAS FAIL, L-R
(Amber – Caution)
(GV)
(O)
2 - 35
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched in the unpressurized configuration
with both Bleed Air Systems inoperative
provided
(GV):
a) Inoperative Bleed Control Valve is
CLOSED and deactivated electrically
when associated Engine Bleed Air System
is selected OFF as follows:
1. Affected Bleed Air Valve is selected
OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTI-ICE:
REER, D-13 or L BLEED AIR CONT:
LEER, E-10 and L WING ANTI-ICE:
LEER, D-4 circuit breakers are pulled
and collared.
b) Manual pressurization control is selected,
c) Outflow valve is slewed to the full OPEN
position,
d) RAM Air is selected ON,
e) Cabin differential pressure is monitored to
be nominally zero psid during the flight,
f) Airplane is not operated in known or
forecast icing conditions, and
g) Airplane is operated in accordance with
AFM Limitations.
Operational Procedures
For GV unpressurized
configuration:
Flight crew will ensure both Bleed
Air Valves are CLOSED and
deactivated electrically.
To operate the airplane
unpressurized, select manual
pressurization and slew the outflow
valve to the full open position with
RAM air selected ON. Monitor
cabin differential pressure to be
nominally zero psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
BAS Maintenance Reqd, L-R
PAGE NO:
2 - 36
3.
Limitations and/or Procedures
Operational Procedures
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
BAS MAINT REQD, L-R
(Blue – Advisory)
(GV)
BATT CHGR FAIL, L-R
(Amber – Caution)
(GV)
A
(O)
Airplane may be dispatched with one
Flight crew will pull and collar
inoperative battery charger provided:
associated “BATT CHGR” CB.
a) Both Engine Generators are operative,
b) APU Generator is operative,
c) Associated L BATT CHGR: Left PDB,
Left Main AC section or R BATT
CHGR: Right PDB, Right Main AC
section circuit breaker on the Power
Distribution Box is pulled and collared,
d) Standby Electrical System is
operative,
e) Affected Battery is selected OFF, and
f) Repairs are made within two (2) flight
days.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Battery Charger Fail, L-R
2 - 37
3.
Limitations and/or Procedures
Operational Procedures
A
Airplane
may be dispatched with one
None required.
(
inoperative
battery
charger
provided:
O
)a) Both Engine Generators are operative,
b) APU Generator is operative,
c) Associated L BATT CHGR: Left PDB,
Left Main AC section or R BATT
CHGR: Right PDB, Right Main AC
section circuit breaker on the Power
Distribution Box is pulled and collared,
d) Standby Electrical System is
operative,
e) Affected Battery is selected OFF, and
f) Repairs are made within two (2) flight
days.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
(Amber – Caution)
(GV-SP/GIV-X)
Brake Maintenance Reqd
2.
PAGE NO:
(Blue – Advisory)
(GV-SP/GIV-X)
BRAKE MAINT REQD
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CAB PRESS SEMIAUTO
(Blue – Advisory)
(GV-SP/GIV-X)
Operational Procedures
C
Airplane may be dispatched provided
airplane is operated in accordance with
AFM Limitations.
None required.
C
Airplane may be dispatched provided
airplane is operated in accordance with
AFM Limitations.
None required.
Airplane may be dispatched provided:
a) Both Display Controllers, Weather
Radar Controllers, and 2 MCDU’s are
operative, and
b) Current terminal charts for the origin,
destination and alternate airports are
carried, or EFB’s are carried, onboard
the airplane and available to the flight
crew.
Flight crew will ensure:
a) Both Display Controllers,
Weather Radar Controllers
and two MCDUs are
operative, and
b) Current terminal charts for
the origin, destination and
alternate airports are
carried, or EFB’s are
carried, onboard the
airplane and available to the
flight crew.
(Blue – Advisory)
(GV-SP/GIV-X)
CCD 1-2 Fail
2 - 38
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
Cabin Pressure Semi-auto
PAGE NO:
B
(O)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
CDU 1-2-3 FAIL
(Blue – Advisory)
(GV)
2.
2 - 39
3.
Limitations and/or Procedures
A
PAGE NO:
Operational Procedures
Except where en route operations or
None required.
approach minimums require its use,
airplane may be dispatched provided:
a) Affected system is not required for IRS
alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not require its use,
d) Both RFMUs are operative, and
e) Repairs are made within two (2) flight
days.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
One (1) system is required in PRNAV,
BRNAV, RNAV 1 and RNAV 2 airspace.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CHECKLIST MISMATCH
(Blue – Advisory)
(GV)
2 - 40
3.
Limitations and/or Procedures
Operational Procedures
B
(O)
Airplane may be dispatched provided:
a) The checklist module in Fault Warning
Computer (FWC) 1 is operative, and
b) Current paper checklists are utilized.
Flight crew will ensure:
a) The checklist module in
Fault Warning Computer
(FWC) 1 is operative, and
b) Utilize current paper
checklists.
C
(O)
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
Aft Cabin Temp Fan Fail;
Forward Cabin Temp Fan Fail;
b) Cockpit Temperature Manual mode is
operative,
c) Associated temperature indicator is
operative,
d) CKPT SENSOR FAN, REER D-10, is
pulled and collared, and
e) Flight crew monitor cockpit
temperature and cockpit duct
temperature.
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
Aft Cabin Temp Fan Fail;
Forward Cabin Temp Fan
Fail,
b) Cockpit Temperature
Manual mode is operative,
c) Associated temperature
indicator is operative,
d) CKPT SENSOR FAN
cirucuit breaker: REER D-10
is pulled and collared, and
e) Cockpit temperature and
cockpit duct temperature are
monitored.
(Blue – Advisory)
(GV)
CKPT TEMP FAN FAIL
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CMC Fail
B
CMF 1-2 Fail
Airplane may be dispatched provided all
faults are recorded after each flight.
(Blue – Advisory)
(GV-SP/GIV-X)
Operational Procedures
None required.
B
(O)
Airplane may be dispatched provided:
Flight crew will ensure:
a) Alternate procedures are established
a) Alternate procedures are
and used, and
established and used, and
b) Flight crew utilizes voice over
b) Voice over VHF/HF is used
VHF/HF to relay pertinent
to relay pertinent information
information to the air traffic
to the air traffic management
management system.
system.
B
(O)
Airplane may be dispatch provided routine
procedures do not require its use.
Flight crew will ensure routine
procedures do not require its
use.
Airplane may be dispatched with one (1)
system inoperative.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
CMS 1-2 Fail
2 - 41
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
PAGE NO:
B
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Cockpit Temp Fan Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 42
3.
Limitations and/or Procedures
C
PAGE NO:
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
Aft Cabin Temp Fan Fail;
Forward Cabin Temp Fan Fail;
b) Cockpit Temperature Manual mode is
operative,
c) Associated temperature indicator is
operative,
d) CKPT SENSOR FAN, REER D-10, is
pulled and collared, and
e) Flight crew monitor cockpit
temperature and cockpit duct
temperature.
Operational Procedures
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
Aft Cabin Temp Fan Fail;
Forward Cabin Temp Fan
Fail,
b) Cockpit Temperature
Manual mode is operative,
c) Associated temperature
indicator is operative,
d) CKPT SENSOR FAN
cirucuit breaker: REER D-10
is pulled and collared, and
e) Cockpit temperature and
cockpit duct temperature are
monitored.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Cockpit Voice Recorder Fail
2.
A
without FDR installed
not Air Carrier or Commercial
2 - 43
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
Airplane may be dispatched provided:
a) Flight Data Recorder (FDR) is
operative, and
b) Repairs are made within three (3)
flight days.
None required.
Airplane may be dispatched provided
repairs are made within three (3) flight
days.
None required.
Airplane may be dispatched provided
repairs are made in accordance with
applicable 14 CFRs.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Cowl Valve Fail Open, L-R
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 44
3.
Limitations and/or Procedures
B
PAGE NO:
Airplane may be dispatched with one (1)
inoperative provided:
a) Affected Valve is verified OPEN,
b) All components of both HP Bleed Air
Systems are operative,
c) Both Environmental Control Systems
(ECS) Packs are operative,
d) Affected Cowl Anti-Ice switch is ON,
e) Affected L COWL ANTI-ICE: LEER, D3 or R COWL ANTI-ICE: REER, D-14
valve circuit breaker is pulled or in the
OPEN position,
f) Performance Computer is initialized
with COWL ANTI ICE selected ON for
either takeoff or landing when COWL
ANTI-ICE valve is pressurized, and
g) Airplane is operated in accordance
with AFM Limitations and
Performance.
Operational Procedures
Flight crew will ensure:
a) BOTH HP Bleed Air
Systems and BOTH
Environmental Control
System (ECS) Packs are
operative.
b) Select the affected Cowl
Anti-Ice switch ON and
ensure that the affected
valve circuit breaker is
pulled or in the OPEN
position.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
COWL VLV FL OP, L-R
CPAM Fail
Flight crew will ensure:
a) BOTH HP Bleed Air
Systems and BOTH
Environmental Control
System (ECS) Packs are
operative.
b) Select the affected Cowl
Anti-Ice switch ON and
ensure that the affected
valve circuit breaker is
pulled or in the OPEN
position.
B
Airplane may be dispatched provided both
auto systems are operative.
None required.
B
Airplane may be dispatched provided both
auto systems are operative.
None required.
(Amber – Caution)
(GV-SP/GIV-X)
CPAM FAIL
(Amber – Caution)
(GV)
Operational Procedures
Airplane may be dispatched with one (1)
inoperative provided:
a) Affected Valve is verified OPEN,
b) All components of both HP Bleed Air
Systems are operative,
c) Both Environmental Control Systems
(ECS) Packs are operative,
d) Affected Cowl Anti-Ice switch is ON,
e) Affected L COWL ANTI-ICE: LEER, D3 or R COWL ANTI-ICE: REER, D-14
valve circuit breaker is pulled or in the
OPEN position,
f) Performance Computer is initialized
with COWL ANTI ICE selected ON for
either takeoff or landing when COWL
ANTI-ICE valve is pressurized, and
g) Airplane is operated in accordance
with AFM Limitations and
Performance.
(Amber – Caution)
(GV)
(O)
2 - 45
3.
Limitations and/or Procedures
B
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(continued)
(O)
2 - 46
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations and Abnormal
Procedures (for Taxi, Takeoffs and
Landings – Max Cabin Pressure
Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional.
Flight crew will operate airplane
in accordance with AFM, Section
1, Limitations, and Section 3,
Abnormal Procedures. For Taxi,
Takeoffs and Landings – Max
Cabin Pressure Differential 0.3
psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X) (cont’d)
(O)
2 - 47
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional.
Flight crew will operate airplane
in accordance with AFM, Section
1, Limitations, and Section 3,
Abnormal Procedures. For Taxi,
Takeoffs and Landings – Max
Cabin Pressure Differential 0.3
psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS 1-2 FAIL
(Blue – Advisory)
(GV)
(continued)
(O)
2 - 48
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations and Abnormal
Procedures (for Taxi, Takeoffs and
Landings – Max Cabin Pressure
Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional.
Flight crew will operate airplane
in accordance with AFM, Section
1, Limitations, and Section 3,
Abnormal Procedures. For Taxi,
Takeoffs and Landings – Max
Cabin Pressure Differential 0.3
psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS 1-2 FAIL
(Blue – Advisory)
(GV) (cont’d)
(O)
2 - 49
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional.
Flight crew will operate airplane
in accordance with AFM, Section
1, Limitations, and Section 3,
Abnormal Procedures. For Taxi,
Takeoffs and Landings – Max
Cabin Pressure Differential 0.3
psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS Channel 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(continued)
(O)
2 - 50
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations and Abnormal
Procedures (for Taxi, Takeoffs and
Landings – Max Cabin Pressure
Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional.
Flight crew will operate airplane
in accordance with AFM,
Limitations, and Abnormal
Procedures. For Taxi, Takeoffs
and Landings – Max Cabin
Pressure Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS Channel 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X) (cont’d)
(O)
2 - 51
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional.
Flight crew will operate airplane
in accordance with AFM,
Limitations, and Abnormal
Procedures. For Taxi, Takeoffs
and Landings – Max Cabin
Pressure Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS CHNL 1-2 FAIL
(Blue – Advisory)
(GV)
(continued)
(O)
2 - 52
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations and Abnormal
Procedures (for Taxi, Takeoffs and
Landings – Max Cabin Pressure
Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate airplane in accordance
with AFM, Limitations, and
Abnormal Procedures.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS CHNL 1-2 FAIL
(Blue – Advisory)
(GV) (cont’d)
(O)
2 - 53
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items, e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate airplane in accordance
with AFM, Limitations, and
Abnormal Procedures.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS Control Panel Fail
(Amber – Caution)
(GV-SP/GIV-X)
(continued)
(O)
2 - 54
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations (for Taxi,
Takeoffs and Landings – Max Cabin
Pressure Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS Control Panel Fail
(Amber – Caution)
(GV-SP/GIV-X) (cont’d)
(O)
2 - 55
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS CONT PNL FAIL
(Amber – Caution)
(GV)
(continued)
(O)
2 - 56
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations (for Taxi,
Takeoffs and Landings – Max Cabin
Pressure Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS CONT PNL FAIL
(Amber – Caution)
(GV) (cont’d)
(O)
2 - 57
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS Fail - Select Manual
(Amber – Caution)
(GV-SP/GIV-X)
(continued)
(O)
2 - 58
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations (for Taxi,
Takeoffs and Landings – Max Cabin
Pressure Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS Fail - Select Manual
(Amber – Caution)
(GV-SP/GIV-X) (cont’d)
(O)
2 - 59
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS FAIL-SEL MAN
(Amber – Caution)
(GV)
(continued)
(O)
2 - 60
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched provided:
a) Manual Pressurization Control System
is operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
c) Cabin Rate of Climb Indicator is
operative,
d) Autopilot is operative,
e) Airplane is operated in accordance
with AFM Limitations (for Taxi,
Takeoffs and Landings – Max Cabin
Pressure Differential 0.3 psi), and
f) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
CPCS FAIL-SEL MAN
(Amber – Caution)
(GV) (cont’d)
(O)
2 - 61
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched in unpressurized configuration
provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full
open position,
c) Both engine bleeds and air
conditioning packs are selected ON if
available, or RAM Air is selected ON,
d) Cabin pressure is monitored to be
nominally zero psid during the flight,
and
e) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure required
items e.g. Manual Pressurization
Control System, Cabin Altitude
and Cabin Rate of Climb
Indicator and Auto Pilot are
functional. Flight crew will
operate the airplane in
accordance with AFM
Limitations.
For Taxi, Takeoffs and Landings
– Max Cabin Pressure
Differential 0.3 psi.
To operate the airplane
unpressurized, select manual
pressurization and slew outflow
valve to full open position with
both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
CPCS LAND ELEV FL
Operational Procedures
B
Airplane may be dispatched provided
pressurization system is operated in the
Semi mode.
None required.
B
Airplane may be dispatched provided
pressurization system is operated in the
Semi mode.
None required.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
A
Airplane may be dispatched provided:
a) Auto system (Cabin Pressure Control
Panel) is operative,
b) Semi-auto mode is considered
inoperative, and
c) Repairs are made within two (2) flight
days.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
CPCS Maintenance Required
2 - 62
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
CPCS Landing Elevation Fail
2.
PAGE NO:
(Blue – Advisory)
(GV-SP/GIV-X)
CPCS MAINT REQD
(Blue – Advisory)
(GV)
CPCS Select Panel Fault
(Blue – Advisory)
(GV-SP/GIV-X)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
(Blue – Advisory)
(GV)
A
(Blue – Advisory)
(GV)
without FDR installed
not Air Carrier or Commercial
2 - 63
3.
Limitations and/or Procedures
CPCS SEL PNL FAULT A
CVR FAIL
2.
PAGE NO:
Operational Procedures
Airplane may be dispatched provided:
a) Auto system (Cabin Pressure Control
Panel) is operative,
b) Semi-auto mode is considered
inoperative, and
c) Repairs are made within two (2) flight
days.
None required.
Airplane may be dispatched provided:
a) Flight Data Recorder (FDR) is
operative, and
b) Repairs are made within three (3)
flight days.
None required.
Airplane may be dispatched provided
repairs are made within three (3) flight
days.
None required.
Airplane may be dispatched provided
repairs are made in accordance with
applicable 14 CFRs.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Database Config
B
DAU 1A FL
DAU 1B FL
DAU 2A FL
DAU 2B FL
(Blue – Advisory)
(GV)
A
(O)
2 - 64
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
Except where en route operations or
minimums require a current database,
airplane may be dispatched with charts out
of currency provided:
a) Current Aeronautical Charts are used
to verify Navigation fixes before
dispatch,
b) Procedures are established and used
to verify status and suitability of
Navigation Facilities used to define
route of flight, and
c) Approach Navigation Radios are
manually tuned and identified.
None required.
Airplane may be dispatched with one (1)
failed DAU channel provided:
a) Flight crew selects operative channel
via the display controller, and
b) Repairs are made within two (2) flight
days.
Flight crew will select operative
channel via the display controller.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
DISP CTRL 2 FAIL
(Blue – Advisory)
(GV)
(continued)
(O)
2 - 65
3.
Limitations and/or Procedures
A
PAGE NO:
Aircraft may be dispatched provided:
a) The weather at the destination is
forecast to be VFR (1,000 ft ceiling
and three (3) miles visibility),
b) An alternate airport is specified in the
flight plan which has VFR weather
forecast (1,000 ft ceiling and three (3)
miles visibility),
c) Both VOR and ADF navigation
receivers are operative,
d) Flight is conducted based on short
range navigation sources only being
available,
e) Navigation suffix in the IFR flight plan
clearly indicates that the airplane is not
capable of any RNP required
navigation capability,
f) Flight is conducted in airspace where
the availability of navigation by short
range navigation receivers (VOR/ADF)
is assured,
g) One DBDI or Standby RMI or
Secondary Navigation Display is
operative,
h) Alternate procedures are established
and used,
Operational Procedures
Flight crew will ensure
associated Display Controller
circuit breaker for the failed
Display Controller is pulled and
collared. The flight crew shall
prepare and display a TOLD
(Takeoff and Landing Data) card
prior to takeoff and prior to
approach and landing.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
2.
PAGE NO:
2 - 66
3.
Limitations and/or Procedures
i)
j)
k)
l)
m)
Flight crew pull and collar associated
Display Controller circuit breaker,
Flight crew prepare and display a
TOLD (Takeoff and Landing Data)
card prior to takeoff and prior to
approach and landing (GV only),
Flight crew verify required approaches
are available at the destination and
alternate airports without being
NOTAMed out of service or unusable,
Pilot-Not-Flying (PNF) is prepared to
announce approach minimums in the
event the operative Display Controller
fails enroute, and
Repairs are made within one (1) flight
day.
Operational Procedures
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Display Controller 2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(continued)
(O)
2 - 67
3.
Limitations and/or Procedures
A
PAGE NO:
Aircraft may be dispatched provided:
a) The weather at the destination is
forecast to be VFR (1,000 ft ceiling
and three (3) miles visibility),
b) An alternate airport is specified in the
flight plan which has VFR weather
forecast (1,000 ft ceiling and three (3)
miles visibility),
c) Both VOR and ADF navigation
receivers are operative,
d) Flight is conducted based on short
range navigation sources only being
available,
e) Navigation suffix in the IFR flight plan
clearly indicates that the airplane is not
capable of any RNP required
navigation capability,
f) Flight is conducted in airspace where
the availability of navigation by short
range navigation receivers (VOR/ADF)
is assured,
g) One DBDI or Standby RMI or
Secondary Navigation Display is
operative,
h) Alternate procedures are established
and used,
Operational Procedures
Flight crew will pull and collar
associated Display Controller
circuit breaker. Flight crew will
verify the required approaches
are available at the destination
and alternate airports without
being NOTAMed out of service or
unusable. When weather
conditions exist at the destination
or alternate airport during the
approach, the PNF will be
prepared to announce approach
minimums in the event the
operative Display Controller fails
en route.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
2.
PAGE NO:
2 - 68
3.
Limitations and/or Procedures
i)
j)
k)
l)
m)
Flight crew pull and collar associated
Display Controller circuit breaker,
Flight crew prepare and display a
TOLD (Takeoff and Landing Data)
card prior to takeoff and prior to
approach and landing (GV only),
Flight crew verify required approaches
are available at the destination and
alternate airports without being
NOTAMed out of service or unusable,
Pilot-Not-Flying (PNF) is prepared to
announce approach minimums in the
event the operative Display Controller
fails en route, and
Repairs are made within one (1) flight
day.
Operational Procedures
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
DME 1-2 Fail
(Amber – Caution)
(GV-SP/GIV-X)
Operational Procedures
C
Airplane may be dispatched except where
en route operations or approach minimums
require its use. Any in excess of those
required by 14 CFR may be inoperative.
None required.
B
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
Elevator Trim 1-2 Fail
2 - 69
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
EGPWM SYS 1-2 Fail
PAGE NO:
NOTE: Synthetic Vision PFD synthetic
terrain will not be available with dual
Terrain Server failures, but the full PFD
may be used without restriction.
B
(O)
Airplane may be dispatched with electric
elevator trim inoperative provided:
a) Electric Elevator Trim remains OFF,
b) Both Flap/Stabilizer Control Channels
are operative (no messages on CAS),
and
c) Airplane is operated in accordance
with AFM Limitations (Maximum
Operating Limit Speed 0.80 Mach).
Flight crew will ensure electronic
Pitch Trim remains “OFF”, both
Flap/Stabilizer Control Channels
are operative (no messages on
CAS), and airplane is operated in
accordance with AFM Limitations
(Maximum Operating Limit
Speed is 0.80 Mach).
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ELEV TRIM INOP
B
(O)
Engine Maintenance ###, L-R
(Blue – Advisory)
(GV-SP/GIV-X)
A
(O)
2 - 70
3.
Limitations and/or Procedures
(Amber – Caution)
(GV)
PAGE NO:
Airplane may be dispatched with electric
elevator trim inoperative provided:
a) Electric Elevator Trim remains OFF,
b) Both Flap/Stabilizer Control Channels
are operative (no messages on CAS),
and
c) Airplane is operated in accordance
with AFM Limitations (Maximum
Operating Limit Speed 0.80 Mach).
Airplane may be dispatched with Blue
“Engine Maintenance STD (###)” and/or
“Engine Maintenance LTD” messages
displayed on EICAS provided:
a) Repairs are made in accordance with
times (hours) established by the BR
710-A1 Time Limits Manual (GV),
Chapter 5 or BR 710-C4 Time Limits
Manual (GV-SP), Chapter 5 (no
extensions are authorized), and
b) FADEC faults are reviewed by flight
crew before each takeoff.
NOTE: Blue “Engine Maintenance STD (###)
messages require maintenance action within
150 hours and Blue “Engine Maintenance
LTD” messages required maintenance action
within 500 hours.
Operational Procedures
Flight crew will ensure electronic
Pitch Trim remains “OFF”, both
Flap/Stabilizer Control Channels
are operative (no messages on
CAS), and airplane is operated in
accordance with AFM Limitations
(Maximum Operating Limit
Speed is 0.80 Mach).
Flight crew will ensure repairs
are made in accordance with
times (hours) established. Flight
crew will review FADEC faults
prior to each takeoff.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Engine Maintenance LTD, L-R A
(Blue – Advisory)
(GV-SP/GIV-X)
2 - 71
3.
Limitations and/or Procedures
(O)
PAGE NO:
Airplane may be dispatched with Blue
“Engine Maintenance STD (###)” and/or
“Engine Maintenance LTD” messages
displayed on EICAS provided:
a) Repairs are made in accordance with
times (hours) established by the BR
710-A1 Time Limits Manual (GV),
Chapter 5 or BR 710-C4 Time Limits
Manual (GV-SP), Chapter 5 (no
extensions are authorized), and
b) FADEC faults are reviewed by flight
crew before each takeoff.
NOTE: Blue “Engine Maintenance STD
(###) messages require maintenance
action within 150 hours and Blue “Engine
Maintenance LTD” messages required
maintenance action within 500 hours.
Operational Procedures
Flight crew will ensure repairs
are made in accordance with
times (hours) established. Flight
crew will review FADEC faults
prior to each takeoff.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ENG MAINT ###, L-R
(Blue – Advisory)
(GV)
(O)
2 - 72
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with Blue
“Engine Maintenance STD (###)” and/or
“Engine Maintenance LTD” messages
displayed on EICAS provided:
a) Repairs are made in accordance with
times (hours) established by the BR
710-A1 Time Limits Manual (GV),
Chapter 5 or BR 710-C4 Time Limits
Manual (GV-SP), Chapter 5 (no
extensions are authorized), and
b) FADEC faults are reviewed by flight
crew before each takeoff.
NOTE: Blue “Engine Maintenance STD
(###) messages require maintenance
action within 150 hours and Blue “Engine
Maintenance LTD” messages required
maintenance action within 500 hours.
Operational Procedures
Flight crew will ensure repairs
are made in accordance with
times (hours) established. Flight
crew will review FADEC faults
prior to each takeoff.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ENG MAINT LTD, L-R
(Blue – Advisory)
(GV)
(O)
2 - 73
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with Blue
“Engine Maintenance STD (###)” and/or
“Engine Maintenance LTD” messages
displayed on EICAS provided:
a) Repairs are made in accordance with
times (hours) established by the BR
710-A1 Time Limits Manual (GV),
Chapter 5 or BR 710-C4 Time Limits
Manual (GV-SP), Chapter 5 (no
extensions are authorized), and
b) FADEC faults are reviewed by flight
crew before each takeoff.
NOTE: Blue “Engine Maintenance STD
(###) messages require maintenance
action within 150 hours and Blue “Engine
Maintenance LTD” messages required
maintenance action within 500 hours.
Operational Procedures
Flight crew will ensure repairs
are made in accordance with
times (hours) established. Flight
crew will review FADEC faults
prior to each takeoff.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
EPS Maintenance Reqd, L-R
2.
PAGE NO:
2 - 74
3.
Limitations and/or Procedures
Operational Procedures
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
EPS MAINT REQD, L-R
(Blue – Advisory)
(GV)
EVS Fail
(Amber – Caution)
(GV-SP/GIV-X)
EVS FAIL
(Amber – Caution)
(GV)
EVS Maintenance Required
(Blue – Advisory)
(GV-SP/GIV-X)
EVS MAINT REQD
(Blue – Advisory)
(GV)
EVS Window Heat Fail
(Amber – Caution)
(GV-SP/GIV-X)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
EVS WINDOW HEAT FAIL
2.
PAGE NO:
2 - 75
3.
Limitations and/or Procedures
Operational Procedures
C
Airplane may be dispatched.
None required.
A
Airplane may be dispatched provided:
a) Cockpit Voice Recorder (CVR) is
operative,
b) Airplane is not dispatched from a
designated airport as listed in the
operator’s MEL unless the FDR failure
occurs after pushback but before
takeoff, and
c) Repairs are made within three (3)
flight days.
None required.
(Amber – Caution)
(GV)
FDAU FAIL
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
FDR SYS FAIL
(Blue – Advisory)
(GV-SP/GIV-X)
2 - 76
3.
Limitations and/or Procedures
Operational Procedures
A
Airplane may be dispatched provided:
a) Cockpit Voice Recorder (CVR) is
operative,
b) Airplane is not dispatched from a
designated airport as listed in the
operator’s MEL unless the FDR failure
occurs after pushback but before
takeoff, and
c) Repairs are made within three (3)
flight days.
None required.
A
Airplane may be dispatched provided:
a) Cockpit Voice Recorder (CVR) is
operative,
b) Airplane is not dispatched from a
designated airport as listed in the
operator’s MEL unless the FDR failure
occurs after pushback but before
takeoff, and
c) Repairs are made within three (3)
flight days.
None required.
(Blue – Advisory)
(GV)
FDR System Fail
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FGC 1-2 FAIL
B
(O)
2 - 77
3.
Limitations and/or Procedures
(Amber – Caution)
(GV)
PAGE NO:
Except for ER operations or where en route
operations or approach minimums require
its use, airplane may be dispatched with
one (1) failed provided airplane is operated
in accordance with AFM Limitations in the
event the operative FGC fails and the Yaw
Damper is inoperative.
Operational Procedures
Flight crew will observe AFM
limitations in the event the
operative FGC fails and the Yaw
Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM,
RNP and PRNAV operations.
Fire Detection Loop Fault
B
Except for ER operations, airplane may be None required.
dispatched with one (1) complete loop (A or
B) inoperative provided the Fault
Switch/Light is pressed to isolate the faulty
loop and illuminate the OFF portion of the
switch light.
B
Except for ER operations, airplane may be None required.
dispatched with one (1) complete loop (A or
B) inoperative provided the Fault
Switch/Light is pressed to isolate the faulty
loop and illuminate the OFF portion of the
switch light.
(Amber – Caution)
(GV-SP/GIV-X)
FIRE DET LOOP FALT
(Amber – Caution)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Flap/Stab Maint Reqd A-B
2.
PAGE NO:
2 - 78
3.
Limitations and/or Procedures
Operational Procedures
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
A
Airplane may be dispatched with one (1)
channel inoperative provided:
a) Electric Pitch Trim System is
operative,
b) Alternate control is verified to be
operative before each departure, and
c) Repairs are made within two (2) flight
days.
None required.
C
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV-SP)
Flap/Stab Maint Reqd
(Blue – Advisory)
(GIV-X)
Flap/Stab System Fail A-B
(Blue – Advisory)
(GV-SP)
FLP/STB MX RQD A-B
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FLP/STB SYS FL A-B
A
FMS/GPS Pos Monitor Unavail B
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 79
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
PAGE NO:
Operational Procedures
Airplane may be dispatched with one (1)
channel inoperative provided:
a) Electric Pitch Trim System is
operative,
d) Alternate control is verified to be
operative before each departure, and
e) Repairs are made within two (2) flight
days.
None required.
Airplane may be dispatched provided:
a) FMS position is checked against
available sensors, and
b) If errors encountered, affected GPS is
de-selected as a position sensor and
FMS position is updated.
Check FMS position against
available sensors. De-select
GPS as a position sensor and
update FMS position if errors
encountered.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
FMS 1-2-3 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
2.
2 - 80
3.
Limitations and/or Procedures
A
PAGE NO:
Operational Procedures
Airplane may be dispatched with two (2)
None required.
inoperative except where en route
operations or approach minimums require
its use provided:
a) Affected system is not required for IRS
alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not require its use,
d) Both RFMU’s are operative (GV), and
e) Repairs are made within two (2) flight
days.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
RNP RNAV including PRNAV and BRNAV
only require a single FMS.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
FMS 1-2 FAIL
(Blue – Advisory)
(GV)
2.
2 - 81
3.
Limitations and/or Procedures
A
PAGE NO:
Operational Procedures
Airplane may be dispatched with two (2)
None required.
inoperative except where en route
operations or approach minimums require
its use provided:
a) Affected system is not required for IRS
alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not require its use,
d) Both RFMU’s are operative (GV), and
e) Repairs are made within two (2) flight
days.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
RNP RNAV including PRNAV and BRNAV
only require a single FMS.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FQMS Maintenance Required
Operational Procedures
Airplane may be dispatched provided:
a) None of the following CAS messages
are also posted:
Aft Cabin Temp Fan Fail;
Cockpit Temp Fan Fail;
b) Forward Temperature Manual mode is
operative,
c) Associated temperature indicator is
operative,
d) FWD CABIN SENSOR FAN, LEER D9, is pulled and collared, and
e) Flight crew monitor forward cabin
temperature and forward cabin duct
temperature.
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
Aft Cabin Temp Fan Fail;
Cockpit Temp Fan Fail,
b) Forward Cabin Temperature
Manual mode is operative,
c) Associated temperature
indicator is operative,
d) FWD CABIN SENSOR FAN
cirucuit breaker: LEER D-9
is pulled and collared, and
e) Forward cabin temperature
and Forward cabin duct
temperature are monitored.
C
Airplane may be dispatched.
None required.
C
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 82
3.
Limitations and/or Procedures
Forward Cabin Temp Fan Fail C
PAGE NO:
(Blue – Advisory)
(GV-SP/GIV-X)
FQMS MAINT REQD
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FQSC Channel Fail, L-R
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 83
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) channel inoperative
provided:
a) Both tanks are completely filled using
overwing refueling,
b) Both Fuel Flow Indicating Systems are
operative,
c) After takeoff, power is set by matching
fuel flow indications on both engines,
and
d) Flight crew maintains a log of fuel
burned.
NOTE: Total Fuel indications will be
INVALID with inoperative indicator.
Operational Procedures
Flight crew will ensure BOTH
tanks are completely filled using
overwing method of fueling.
NOTE: Do not pull Quel Qty
circuit breaker as this disables
Fuel Level Low caution message.
Flight crew will ensure:
a) B oth Fuel Flow Indicating
Systems are operative.
b) After takeoff, power is set by
matching Fuel Flow
indications on both engines.
c) A log of fuel burned is
maintained.
NOTE: Total Fuel indication will
be INVALID with inoperative
indicator.
(continued)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FQSC Channel Fail, L-R
(Blue – Advisory)
(GV-SP/GIV-X) (cont’d)
(O)
2 - 84
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) channel inoperative
provided:
a) Affected tank is defueled before each
refueling,
b) Affected tank is fueled with a known
quantity of fuel,
c) Both fuel flow meters are operative,
d) After takeoff, power is set by matching
fuel flow indications on both engines,
and
e) Flight crew maintains a log of fuel
burned.
NOTE: Total Fuel indications will be
INVALID with inoperative indicator.
Operational Procedures
Flight crew will Defuel affected
tank before each refueling and
refuel it with a Known quantity of
fuel.
Flight crew will ensure:
a) Both fuel flow meters are
operative.
b) After takeoff, power is set by
matching Fuel Flow
indications on both engines.
c) A log of fuel burned is
maintained.
NOTE: Total Fuel indication will
be INVALID with inoperative
indicator.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FQSC CH FAIL, L-R
(Blue – Advisory)
(GV)
(O)
2 - 85
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) channel inoperative
provided:
a) Both tanks are completely filled using
overwing refueling,
b) Both Fuel Flow Indicating Systems are
operative,
c) After takeoff, power is set by matching
fuel flow indications on both engines,
and
d) Flight crew maintains a log of fuel
burned.
NOTE: Total Fuel indications will be
INVALID with inoperative indicator.
Operational Procedures
Flight crew will ensure BOTH
tanks are completely filled using
overwing method of fueling.
NOTE: Do not pull Quel Qty
circuit breaker as this disables
Fuel Level Low caution message.
Flight crew will ensure:
a) B oth Fuel Flow Indicating
Systems are operative.
b) After takeoff, power is set by
matching Fuel Flow
indications on both engines.
c) A log of fuel burned is
maintained.
NOTE: Total Fuel indication will
be INVALID with inoperative
indicator.
(continued)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FQSC CH FAIL, L-R
(Blue – Advisory)
(GV) (cont’d)
(O)
2 - 86
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) channel inoperative
provided:
a) Affected tank is defueled before each
refueling,
b) Affected tank is fueled with a known
quantity of fuel,
c) Both fuel flow meters are operative,
d) After takeoff, power is set by matching
fuel flow indications on both engines,
and
e) Flight crew maintains a log of fuel
burned.
NOTE: Total Fuel indications will be
INVALID with inoperative indicator.
Operational Procedures
Flight crew will Defuel affected
tank before each refueling and
refuel it with a Known quantity of
fuel.
Flight crew will ensure:
a) Both fuel flow meters are
operative.
b) After takeoff, power is set by
matching Fuel Flow
indications on both engines.
c) A log of fuel burned is
maintained.
NOTE: Total Fuel indication will
be INVALID with inoperative
indicator.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Front Windshield Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
Operational Procedures
B
Except for ER operations, airplane may be
dispatched with one (1) inoperative
provided airplane is not operated in known
or forecast icing conditions.
None required.
C
Airplane may be dispatched with one
inoperative sensor in each Windshield Heat
System.
None required.
Except for ER operations, airplane may be
dispatched with inoperative crossflow valve
provided:
a) All Fuel Boost Pumps are operative,
b) Fuel Intertank Valve is operative,
c) Fuel Quantity Indicating System is
operative,
d) Fuel Tank Temperature System is
operative, and
e) Airplane is operated in accordance
with AFM Limitations.
Flight crew will ensure:
a) All Fuel boost Pumps are
operative,
b) Fuel Intertank Valve is
operative,
c) Fuel Quantity Indicating
System is operative,
d) Fuel tank temperature
system is operative.
(Blue – Advisory)
(GV-SP/GIV-X)
Fuel Crossflow Valve Open
2 - 87
3.
Limitations and/or Procedures
(Amber – Caution)
(GV-SP/GIV-X)
Front Windshield Fault, L-R
PAGE NO:
B
(O)
NOTE: Avoid uncoordinated maneuvers
when Fuel Intertank Valve is OPEN.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Fuel Return Fail, L-R
(Blue – Advisory)
(GV)
2 - 88
3.
Limitations and/or Procedures
Operational Procedures
B
Airplane may be dispatched provided:
a) Flight crew monitors fuel tank
temperature, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
B
Airplane may be dispatched provided:
a) Flight crew monitors fuel tank
temperature, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
(Blue – Advisory)
(GV-SP)
FUEL RETURN FL, L-R
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
FWD CAB TMP FAN FL
C
F WSHLD FAIL, L-R
(Amber – Caution)
(GV)
B
(O)
2 - 89
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
PAGE NO:
Operational Procedures
Airplane may be dispatched provided:
a) None of the following CAS
messages are also posted:
Aft Cabin Temp Fan Fail;
Cockpit Temp Fan Fail;
b) Forward Temperature Manual mode
is operative,
c) Associated temperature indicator is
operative,
d) FWD CABIN SENSOR FAN, LEER
D-9, is pulled and collared, and
e) Flight crew monitor forward cabin
temperature and forward cabin duct
temperature.
Flight crew will ensure:
a) None of the following CAS
messages are also posted:
Aft Cabin Temp Fan Fail;
Cockpit Temp Fan Fail,
b) Forward Cabin Temperature
Manual mode is operative,
c) Associated temperature
indicator is operative,
d) FWD CABIN SENSOR FAN
cirucuit breaker: LEER D-9
is pulled and collared, and
e) Forward cabin temperature
and Forward cabin duct
temperature are monitored.
Except for ER operations, airplane may be
dispatched with one (1) inoperative
provided airplane is not operated in known
or forecast icing conditions.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
GCU Fail, L-R
(Blue – Advisory)
(GV)
2 - 90
3.
Limitations and/or Procedures
Operational Procedures
A
Except for ER Operations, airplane may be
dispatched with one Engine Generator
Control Unit (GCU) inoperative provided:
a) APU Generator is used for all phases
of flight,
b) Airplane is operated at or below
FL450,
c) Standby Electrical System is
operative, and
d) Repairs are made within two (2) flight
days.
None required.
A
Except for ER operations, airplane may be
dispatched with one Engine Generator
Control Unit (GCU) inoperative provided:
a) APU Generator is used for all phases
of flight,
b) Airplane is operated at or below
FL450,
c) Standby Electrical System is
operative, and
d) Repairs are made within two (2) flight
days.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
GCU FAIL, L-R
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Generator Fail, L-R
(Blue – Advisory)
(GV)
2 - 91
3.
Limitations and/or Procedures
Operational Procedures
A
Except for ER operations, airplane may be
dispatched with one Engine Generator
Control Unit (GCU) inoperative provided:
a) APU Generator is used for all phases
of flight,
b) Airplane is operated at or below
FL450,
c) Standby Electrical System is
operative, and
d) Repairs are made within two (2) flight
days.
None required.
A
Except for ER operations, airplane may be
dispatched with one Engine Generator
Control Unit (GCU) inoperative provided:
a) APU Generator is used for all phases
of flight,
b) Airplane is operated at or below
FL450,
c) Standby Electrical System is
operative, and
d) Repairs are made within two (2) flight
days.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
GEN FAIL, L-R
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
GPS 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
Operational Procedures
B
Airplane may be dispatched except where
en route operations or approach minimums
require the use of GPS or GNSSU.
None required.
B
Airplane may be dispatched except where
en route operations or approach minimums
require the use of GPS or GNSSU.
None required.
Airplane may be dispatched provided:
a) Alternate procedures are established
and used,
b) Pilot-Not-Flying (PNF) monitors flight
progress with reference to radio
altimeter data and situational
awareness,
c) PNF advises Pilot-Flying (PF) of
adverse situations,
d) Airplane is operated in accordance
with AFM Limitations, and
e) Repairs are made within two (2) flight
days.
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
(Blue – Advisory)
(GV)
GPWS 1-2 Fail
2 - 92
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
GPS 1-2 FAIL
PAGE NO:
A
(O)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
GPWS FAIL
HUD COMP Fan Fail
Pilot-Not-Flying (PNF) will
monitor flight progress with
reference to radio altimeter data
and situational awareness and
advise Pilot-Flying (PF) of
adverse situations.
C
Airplane may be dispatched provided
extended ground operations are avoided.
None required.
C
Airplane may be dispatched provided:
a) Extended ground operations are
avoided, and
b) Pilot selected HUD brightness is
reduced.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
HUD OHU Fan Fail
(Blue – Advisory)
(GV-SP/GIV-X)
Operational Procedures
Airplane may be dispatched provided:
a) Alternate procedures are established
and used,
b) Pilot-Not-Flying (PNF) monitors flight
progress with reference to radio
altimeter data and situational
awareness,
c) PNF advises Pilot-Flying (PF) of
adverse situations,
d) Airplane is operated in accordance
with AFM Limitations, and
e) Repairs are made within two (2) flight
days.
(Blue – Advisory)
(GV)
(O)
2 - 93
3.
Limitations and/or Procedures
A
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Hydraulic Temp Sen Fail, L-R
B
(Blue – Advisory)
(GV)
2 - 94
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
HYD TMP SEN FL, L-R
2.
PAGE NO:
Airplane may be dispatched.
Operational Procedures
None required.
NOTE: Accuracy of hydraulic quantity
indication will be degraded during long
flights in cold soak conditions. If Right
Hydraulic System (R SYS) sensor has
failed in flight, there is no protection against
overheating R SYS pumps during Power
Transfer Unit (PTU) operation. In flight, with
either or both sensors failed, there is no
warning of hot hydraulic system
temperatures.
B
Airplane may be dispatched.
NOTE: Accuracy of hydraulic quantity
indication will be degraded during long
flights in cold soak conditions. If Right
Hydraulic System (R SYS) sensor has
failed in flight, there is no protection against
overheating R SYS pumps during Power
Transfer Unit (PTU) operation. In flight, with
either or both sensors failed, there is no
warning of hot hydraulic system
temperatures.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Ice Detect Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 95
3.
Limitations and/or Procedures
B
PAGE NO:
Airplane may be dispatched provided:
a) Airplane is operated in accordance
with alternate AFM procedures,
b) Cowl Anti-Ice shall be selected ON
manually any time visible moisture is
present and SAT is +10 deg C or less,
and
c) Wing Anti-Ice should be selected ON
manually if icing conditions are
imminent or immediately upon
detection of ice formation on the
wings, winglets or windshield edges.
NOTE: With Ice Detection Systems
inoperative, automatic anti-ice is not
available.
Operational Procedures
Flight crew shall operate airplane
in accordance with Alternate
AFM procedures. Cowl Anti-Ice
shall be selected ON manually
any time visible moisture is
present and the SAT is +10 deg
C or less. Wing Anti-Ice should
be selected ON manually if icing
conditions are imminent or
immediately upon detection of ice
formation on the wings, winglets
or windshield edges.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
ICE DETECT FL, L-R
(Amber – Caution)
(GV)
(O)
2 - 96
3.
Limitations and/or Procedures
B
PAGE NO:
Airplane may be dispatched provided:
a) Airplane is operated in accordance
with alternate AFM procedures,
b) Cowl Anti-Ice shall be selected ON
manually any time visible moisture is
present and SAT is +10 deg C or less,
and
c) Wing Anti-Ice should be selected ON
manually if icing conditions are
imminent or immediately upon
detection of ice formation on the
wings, winglets or windshield edges.
NOTE: With Ice Detection Systems
inoperative, automatic anti-ice is not
available.
Operational Procedures
Flight crew shall operate airplane
in accordance with Alternate
AFM procedures. Cowl Anti-Ice
shall be selected ON manually
any time visible moisture is
present and the SAT is +10 deg
C or less. Wing Anti-Ice should
be selected ON manually if icing
conditions are imminent or
immediately upon detection of ice
formation on the wings, winglets
or windshield edges.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
IRS 1-2-3 Fail
(Blue – Advisory)
(GV)
2 - 97
3.
Limitations and/or Procedures
Operational Procedures
A
(O)
Airplane may be dispatched with one (1)
Flight crew will ensure the same
IRS inoperative provided:
IRS is NOT used as attitude
a) Both PFD attitude indicating systems
source for both pilots.
operate independently,
b) Flight crew ensure same IRS is NOT
used as attitude source for both pilots,
c) Standby Attitude Indicator is operative,
and
d) Repairs are made within two (2) flight
days.
A
(O)
Airplane may be dispatched with one (1)
Flight crew will ensure the same
IRS inoperative provided:
IRS is NOT used as attitude
a) Both PFD attitude indicating systems
source for both pilots.
operate independently,
b) Flight crew ensure same IRS is NOT
used as attitude source for both pilots,
c) Standby Attitude Indicator is operative,
and
d) Repairs are made within two (2) flight
days.
(Blue – Advisory)
(GV-SP/GIV-X)
IRS 1-2-3 FAIL
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
IRS 1-2-3 ON DC
(Blue – Advisory)
(GV-SP/GIV-X)
2 - 98
3.
Limitations and/or Procedures
Operational Procedures
A
Airplane may be dispatched provided only
one (1) IRU / IRS is on Secondary Power
provided repairs are made within one (1)
flight day.
None required.
A
Airplane may be dispatched provided only
one (1) IRU / IRS is on Secondary Power
provided repairs are made within one (1)
flight day.
None required.
(Blue – Advisory)
(GV)
IRU On Sec Pwr
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
IRU Sec Pwr 1-2-3 Fail
(Blue – Advisory)
(GV)
2 - 99
3.
Limitations and/or Procedures
Operational Procedures
A
Airplane may be dispatched with both back- None required.
up batteries inoperative provided:
a) The affected battery is located in the
#2 or #3 IRU back up battery position,
and
b) Repairs are made within one (1) flight
day.
A
Airplane may be dispatched with both back- None required.
up batteries inoperative provided:
a) Airplane is operated in day VMC
conditions, and
b) Repairs are made within one (1) flight
day.
A
Airplane may be dispatched with both back- None required.
up batteries inoperative provided:
a) All other components of the Electrical
Power system are operative, and
b) Repairs are made within one (1) flight
day.
B
Airplane may be dispatched provided at
least one Flight Management System is
operative.
(Blue – Advisory)
(GV-SP/GIV-X)
LASERTRAK FAIL
2.
PAGE NO:
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
L PSU Fan Fail
B
LX Fail
(O)
2 - 100
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
Airplane may be dispatched provided:
Flight crew will:
a) Ambient Temperature is 95 degrees F
a) Minimize ground operation
(35 degrees C) or cooler,
time, espescially during hot
b) TRU electrical loads are 50% or less,
weather,
c) Right main TRU is operative,
b) During Ground operation,
d) Both Environmental Control System
monitor TRU load – limit
(ECS) Packs are operative,
load to 50%,
e) Flight crew minimize ground operation
c) For ground operation longer
time, and
than 15 minutes ensure
f) For ground operations longer than 15
main and baggage doors
minutes, flight crew ensure main and
are closed. APU air is
baggage doors are closed, APU air is
selected “ON” and outflow
selected “ON” and outflow valve is fully
valve is fully OPEN.
OPEN.
C
Airplane may be dispatched.
None required.
B
Airplane may be dispatched with one (1)
Mach Trim System inoperative.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
Mach Trim 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
MADC 1-2-3 FAIL
(Blue – Advisory)
(GV)
(O)
2 - 101
3.
Limitations and/or Procedures
B
PAGE NO:
Airplane may be dispatched with a one (1)
micro air data computer inoperative
provided:
a) Manual Pressurization Control System is
operative,
b) Cabin Altitude and Differential Pressure
Indicators are operative,
c) Cabin Rate of Climb Indicator is operative,
d) Autopilot is operative,
e) Airplane is operated in accordance with
AFM limitations,
f) MADC 1: POP A-9, MADC 2: CPOP A-9,
and MADC 3: POP A-10 circuit breakers
associated with the failed Micro Air Data
Computer (MADC) are pulled and
collared, and
g) Flight crew selects operative and different
MADC sources prior to departure.
NOTE 1: Two systems are required for
operation in RVSM airspace.
NOTE 2: For MADC 1 FAIL, expect the L
Engine Backup Air Data advisory and
associated Engine Maintenance message to
post.
NOTE 3: For MADC 2 FAIL, expect the R
Engine Backup Air Data advisory and
associated Engine Maintenance message to
post.
Operational Procedures
Flight crew will pull and collar
MADC 1: POP A-9, MADC 2:
CPOP A-9, and MADC 3: POP
A-10 circuit breaker associated
with Micro Air Data Computers.
Flight crew will operationally
check and assure that the items
called out in provisos a) thru d)
are operative.
Flight crew will comply with all
AFM limitations in section 1-0330, 1-03-40, and 1-21-10.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
MADC 1-2-3 FAIL
(Blue – Advisory)
(GV)
2 - 102
3.
Limitations and/or Procedures
Operational Procedures
B
(O)
Airplane may be dispatched with one (1)
micro air data computer inoperative
provided airplane is operated in
unpressurized configuration.
To operate the airplane
unpressurized, select manual
pressurization and slew the
outflow valve to full open position
with both engine bleeds and air
conditioning packs selected ON if
available. If not, select RAM Air
ON. Monitor Cabin differential
pressure to be nominally zero
psid during the flight.
A
(O)
Except for ER operations, airplane may be
dispatched with one (1) probe heater
inoperative provided:
a) Airplane is not operated in visible
moisture or known or forecast icing
conditions,
b) L LWR PITOT HTR: CPOP A-5 and R
LWR PITOT HTR: CPOP A-5 circuit
breakers are pulled and collared,
c) Flight crew select MADC sources that
are different and not associated with
failed pitot heater element, and
d) Repairs are made within two (2) flight
days.
Flight crew will pull and collar L
LWR PITOT HTR: CPOP A-5
and R LWR PITOT HTR: CPOP
A-5 circuit breakers and select
MADC sources that are different
and not associated with failed
pitot heater element.
(Blue – Advisory)
(GV) (cont’d)
MADC 1-3 PROBE FL
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
MADC 2-SBY PROBE FL
(Blue – Advisory)
(GV)
(O)
2 - 103
3.
Limitations and/or Procedures
A
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) probe heater
inoperative provided:
a) Airplane is not operated in visible
moisture or known or forecast icing
conditions,
b) L UPR PITOT HTR: CPOP A-6 and R
UPR PITOT HTR: CPOP A-6 circuit
breakers are pulled and collared,
c) Flight crew select MADC sources that
are different and not associated with
failed pitot heater element, and
d) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar L
UPR PITOT HTR: CPOP A-6 and
R UPR PITOT HTR: CPOP A-6
circuit breakers and select MADC
sources that are different and not
associated with failed pitot heater
element.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Main Fuel Pump Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 104
3.
Limitations and/or Procedures
B
PAGE NO:
Except for ER operations, airplane may be
dispatched with one (1) pump inoperative
provided:
a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning
Systems are operative,
d) Flight crew comply with AFM, Section
3, Abnormal Procedures, Fuel Boost
Pump Failure, and
e) Airplane is operated in accordance
with AFM Limitations.
Operational Procedures
Flight crew will ensure:
a) Fuel Crossflow Valve and
Intertank Valve are
operative,
b) BOTH Fuel Low Quantity
Warning Systems are
operative,
c) Verify compliance with AFM,
Section 3, Abnormal
Procedures, Fuel Boost
Pump Failure.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
MAIN PUMP FAIL, L-R
B
MAINT REQUIRED
(Blue – Advisory)
(GV)
C
(O)
2 - 105
3.
Limitations and/or Procedures
(Amber – Caution)
(GV)
PAGE NO:
Operational Procedures
Except for ER operations, airplane may be
dispatched with one (1) pump inoperative
provided:
a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning
Systems are operative,
d) Flight crew comply with AFM, Section
3, Abnormal Procedures, Fuel Boost
Pump Failure, and
e) Airplane is operated in accordance
with AFM Limitations.
Flight crew will ensure:
a) Fuel Crossflow Valve and
Intertank Valve are
operative,
b) BOTH Fuel Low Quantity
Warning Systems are
operative,
c) Verify compliance with AFM,
Section 3, Abnormal
Procedures, Fuel Boost
Pump Failure.
Airplane may be dispatched.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Main TRU Fault, L-R
A
MAU 1-2-3 Fan Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
(O)
2 - 106
3.
Limitations and/or Procedures
(Amber – Caution)
(GV-SP/GIV-X)
PAGE NO:
Airplane may be dispatched with one (1)
main TRU inoperative provided:
a) Both Generators are operative,
b) Both essential TRU’s are operative,
c) Auxiliary TRU is operative,
d) APU Generator is operative,
e) Both Battery chargers are operative,
f) Both Main Airplane Batteries are
operative,
g) Inoperative L MAIN TRU: LPDB, Left
Main AC section or R MAIN TRU:
RPDB, Right Main AC section TRU
circuit breaker on the Power
Distribution Box is pulled and collared,
and
h) Repairs are made within two (2) flight
days.
Airplane may be dispatched:
a) With one (1) failed fan provided
performance of items affected by the
indicated MAU are monitored during
the flight, and
b) Flight crew references the appropriate
matrix in AFM Section 03-16-80.
Operational Procedures
Flight crew will pull and collar
inoperative TRU circuit breaker
on Power Distribution Box.
Flight crew will ensure AUX TRU
is operative and both essential
TRUs are operative.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
MAU 1B-2A-3A-3B Fail
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 107
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with one (1)
channel inoperative provided:
a) Failed channel is not MAU 1A or MAU
2B,
b) No other failures exist in the Avionics
System,
c) Associated MAU circuit breakers:
MAU 1A PRI: POP, A-10
MAU 1A SEC: CPOP, A-10
MAU 1B PRI: CPOP, A-9
MAU 1B SEC: POP, A-9
MAU 2A PRI: CPOP, A-8
MAU 2A SEC: POP, A-8
MAU 2B PRI: CPOP, A-7
MAU 2B SEC: POP, A-7
MAU 3A PRI: POP, A-6
MAU 3A SEC: CPOP, A-6
MAU 3B PRI: POP, A-5
MAU 3B SEC: CPOP, A-5
are pulled and collared,
d) Alternate procedures are established
and used,
e) Flight crew discusses contingency
procedures for next worse failures as
described in GAC-OIS-09 Dispatch
with MAU Channels Inoperative, and
f) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar the
associated MAU circuit breakers.
Flight crew will review the next
worse failures as described in the
GAC-OIS-09 Dispatch with MAU
Channels Inoperative.
Flight crew will discuss
contingency procedures should
the next worse failure occur and
plan accordingly for the flight.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
MDAU FAIL
(Amber – Caution)
(GV)
Operational Procedures
B
Airplane may be dispatched provided all
faults are recorded after each flight.
None required.
B
Airplane may be dispatched provided all
faults are recorded after each flight.
None required.
Airplane may be dispatched with one (1)
main TRU inoperative provided:
a) Both Generators are operative,
b) Both essential TRU’s are operative,
c) Auxiliary TRU is operative,
d) APU Generator is operative,
e) Both Battery chargers are operative,
f) Both Main Airplane Batteries are
operative,
g) Inoperative L MAIN TRU: LPDB, Left
Main AC section or R MAIN TRU:
RPDB, Right Main AC section TRU
circuit breaker on the Power
Distribution Box is pulled and collared,
and
h) Repairs are made within two (2) flight
days.
Flight crew will pull and collar
inoperative TRU circuit breaker
on Power Distribution Box.
(Blue – Advisory)
(GV)
MN TRU FAULT, L-R
2 - 108
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
MDAU MEM 90% FULL
PAGE NO:
A
(O)
Flight crew will ensure AUX TRU
is operative and both essential
TRUs are operative.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
MRC 1 Fail
2.
A
2 - 109
3.
Limitations and/or Procedures
(Amber – Caution)
(GV-SP/GIV-X)
PAGE NO:
Airplane may be dispatched with one (1)
MRC failed, provided:
a) Associated Comm and Nav radios and
opposite ATC are operative, and
b) Repairs are made within one (1) flight
day.
Operational Procedures
None required.
NOTE: EICAS blue messages “APM FAIL”
and “ASCB FAIL” displayed. “ASCB FAIL”
is only displayed in flight.
MRC 2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
A
Airplane may be dispatched provided:
a) Associated Comm and Nav radios and
opposite ATC are operative, and
b) Repairs are made within one (1) flight
day.
NOTE: With MRC 2 Fail, expect EICAS
blue messages “APM FAIL” and “ASCB
FAIL” displayed. “ASCB FAIL” will display
inflight only.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
NAV 2 Fail
(Blue – Advisory)
(GV)
Operational Procedures
B
Airplane may be dispatched as required by
14 CFR.
None required.
B
Airplane may be dispatched provided
operations do not require its use.
None required.
A
Except where en route operations or
None required.
approach minimums require its use,
airplane may be dispatched provided:
a) Affected system is not required for IRS
alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not require its use,
d) Both RFMUs are operative, and
e) Repairs are made within two (2) flight
days.
(Blue – Advisory)
(GV-SP/GIV-X)
NMS 1-2 FAIL
2 - 110
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
NAVCOM Fail
2.
PAGE NO:
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
One (1) system is required in PRNAV,
BRNAV, RNAV 1 and RNAV 2 airspace.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
NMS FAIL
2.
A
2 - 111
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
PAGE NO:
Operational Procedures
Except where en route operations or
None required.
approach minimums require its use,
airplane may be dispatched provided:
a) Affected system is not required for IRS
alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not require its use,
d) Both RFMUs are operative, and
e) Repairs are made within two (2) flight
days.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
One (1) system is required in PRNAV,
BRNAV, RNAV 1 and RNAV 2 airspace.
NWS Fixed Gain
B
Airplane may be dispatched provided Nose
Wheel Tiller Steering System is operative.
None required.
B
Airplane may be dispatched provided Nose
Wheel Tiller Steering System is operative.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
NWS FIXED GAIN
(Blue – Advisory)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Outflow Valve Fault
Airplane may be dispatched provided:
a) DC motor is operative, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
B
Airplane may be dispatched provided:
a) DC motor is operative, and
b) Airplane is operated in accordance
with AFM Limitations.
None required.
Airplane may be dispatched with one (1)
inoperative Autopilot Pitch Trim Servo
provided PITCH TRIM SERVO #1: POP, E2 or PITCH TRIM SERVO #2, CPOP, E-1
circuit breaker is pulled and collared.
Flight crew will ensure
inoperative servo circuit breaker
is pulled and collared.
B
(Blue – Advisory)
(GV-SP/GIV-X)
RAAS 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
Operational Procedures
B
(Blue – Advisory)
(GV)
Pitch Trim 1-2 Power Fail
2 - 112
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
OUTFLOW VLV FAULT
PAGE NO:
B
(O)
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
RAD ALT 1-2 FAIL
(Blue – Advisory)
(GV-SP/GIV-X)
2 - 113
3.
Limitations and/or Procedures
Operational Procedures
B
Airplane may be dispatched provided:
None required.
a) Landing weather minimums or
operating procedures do not require its
use, and
b) Other systems affected (E/GPWS,
TCAS, Flight Director, Autopilot,
Autothrottle, Altimeter Ground
Awareness Display, Synthetic Vision
Primary Flight Display, HUD Flare
Cue) are considered.
B
Airplane may be dispatched provided:
None required.
a) Landing weather minimums or
operating procedures do not require its
use, and
b) Other systems affected (E/GPWS,
TCAS, Flight Director, Autopilot,
Autothrottle, Altimeter Ground
Awareness Display, Synthetic Vision
Primary Flight Display, HUD Flare
Cue) are considered.
(Blue – Advisory)
(GV)
Radio Altimeter 1-2 Fail
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Rudder Steering Fail
(Blue – Advisory)
(GIV-X/GV-SP)
Operational Procedures
B
Airplane may be dispatched provided:
a) Nose Wheel Tiller Steering System is
operative, and
b) Left seat pilot performs the takeoff and
landing task.
None required.
B
Airplane may be dispatched provided:
a) Nose Wheel Tiller Steering System is
operative, and
b) Left seat pilot performs the takeoff and
landing task.
None required.
C
Airplane may be dispatched provided
procedures do not require their use.
None required.
(Amber – Caution)
(GV)
SATCOM Call
2 - 114
3.
Limitations and/or Procedures
(Amber – Caution)
(GV-SP/GIV-X)
RUDDER STRG FAIL
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Service Door
(Amber – Caution)
(GV-SP/GIV-X)
Operational Procedures
B
(O)
Airplane may be dispatched provided a
crewmember verifies by visual inspection
before each departure that the associated
door is CLOSED and LOCKED.
Flight crew will visually inspect
door(s) to ensure it is CLOSED
and LOCKED prior to departure.
B
(O)
Airplane may be dispatched provided a
crewmember verifies by visual inspection
before each departure that the associated
door is CLOSED and LOCKED.
Flight crew will visually inspect
door(s) to ensure it is CLOSED
and LOCKED prior to departure.
Airplane may be dispatched.
None required.
(Blue – Advisory)
(GV)
Side Windshield Fail, L-R
2 - 115
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV-SP/GIV-X)
SERVICE DOOR
PAGE NO:
B
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
STCK PUSH 1-2 FAULT
(Amber – Caution)
(GV)
(O)
2 - 116
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with one (1)
system inoperative provided:
a) Angle of Attack indication is available on
both PFD’s,
b) Alternate procedures are established and
used,
c) The inoperative stall barrier system is
electrically disabled by pulling and
collaring the Stall Barrier Valve and Stick
Shaker associated with the failed system,
d) Crew procedures in the event the
remaining stall barrier fails are discussed,
e) If the remaining stall barrier fails the
minimum speed shall be no less than Vref
(1.3 Vs) for all phases of flight (this
minimum speed shall be cross referenced
to a normalized AOA value of 0.59 as
displayed on the PFD),
f) Weather at departure and destination is
considered,
g) Consideration is given to delaying takeoff
or approach and landing, if windshear is
forecast until such conditions cease, or
consideration is given to proceeding to
alternate, and
h) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar the
circuit breakers for the Stall Barrier
Valve and Stick Shaker associated
with the failed system. Prior to
dispatch, the flight crew will discuss
the dispatch situation with the stall
barrier inoperative and crew
procedures in the event the
remaining operative stall barrier
fails. If the remaining stall barrier
fails, the minimum speed shall be no
less than Vref (1.3 Vs) for all phases
of flight. This minimum speed shall
be cross-referenced to Normalized
Angle of Attack of 0.59 as displayed
on the PFD. Weather conditions at
the departure and destination
airports shall be considered. If there
are known or forecast windshear
conditions at the departure or
destination airport, the crew shall
consider delaying the takeoff or
approach and landing until such
conditions cease to exist, or
consider deviation to an alternate
airport in the approach and landing
case.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
STCK PUSH 1-2 FL
(Amber – Caution)
(GV)
(O)
2 - 117
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with one (1)
system inoperative provided:
a) Angle of Attack indication is available on
both PFD’s,
b) Alternate procedures are established and
used,
c) The inoperative stall barrier system is
electrically disabled by pulling and
collaring the Stall Barrier Valve and Stick
Shaker associated with the failed system,
d) Crew procedures in the event the
remaining stall barrier fails are discussed,
e) If the remaining stall barrier fails the
minimum speed shall be no less than Vref
(1.3 Vs) for all phases of flight (this
minimum speed shall be cross referenced
to a normalized AOA value of 0.59 as
displayed on the PFD),
f) Weather at departure and destination is
considered,
g) Consideration is given to delaying takeoff
or approach and landing, if windshear is
forecast until such conditions cease, or
consideration is given to proceeding to
alternate, and
h) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar the
circuit breakers for the Stall Barrier
Valve and Stick Shaker associated
with the failed system. Prior to
dispatch, the flight crew will discuss
the dispatch situation with the stall
barrier inoperative and crew
procedures in the event the
remaining operative stall barrier
fails. If the remaining stall barrier
fails, the minimum speed shall be no
less than Vref (1.3 Vs) for all phases
of flight. This minimum speed shall
be cross-referenced to Normalized
Angle of Attack of 0.59 as displayed
on the PFD. Weather conditions at
the departure and destination
airports shall be considered. If there
are known or forecast windshear
conditions at the departure or
destination airport, the crew shall
consider delaying the takeoff or
approach and landing until such
conditions cease to exist, or
consider deviation to an alternate
airport in the approach and landing
case.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Stick Push 1-2 Fail
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 118
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with one (1)
system inoperative provided:
a) Angle of Attack indication is available on
both PFD’s,
b) Alternate procedures are established and
used,
c) The inoperative stall barrier system is
electrically disabled by pulling and
collaring the Stall Barrier Valve and Stick
Shaker associated with the failed system,
d) Crew procedures in the event the
remaining stall barrier fails are discussed,
e) If the remaining stall barrier fails the
minimum speed shall be no less than Vref
(1.3 Vs) for all phases of flight (this
minimum speed shall be cross referenced
to a normalized AOA value of 0.59 as
displayed on the PFD),
f) Weather at departure and destination is
considered,
g) Consideration is given to delaying takeoff
or approach and landing, if windshear is
forecast until such conditions cease, or
consideration is given to proceeding to
alternate, and
h) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar the
circuit breakers for the Stall Barrier
Valve and Stick Shaker associated
with the failed system. Flight crew
will discuss crew procedures in the
event the remaining operative stall
barrier fails. If the remaining stall
barrier fails, the minimum speed
shall be no less than Vref (1.3 Vs)
for all phases of flight. This
minimum speed shall be crossreferenced to Normalized Angle of
Attack of 0.59 as displayed on the
PFD. Weather conditions at the
departure and destination airports
shall be considered. If there are
known or forecast windshear
conditions at the departure or
destination airport, the crew shall
consider delaying the takeoff or
approach and landing until such
conditions cease to exist, or
consider deviation to an alternate
airport in the approach and landing
case.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Stick Push 1-2 Fault
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 119
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with one (1)
system inoperative provided:
a) Angle of Attack indication is available on
both PFD’s,
b) Alternate procedures are established and
used,
c) The inoperative stall barrier system is
electrically disabled by pulling and
collaring the Stall Barrier Valve and Stick
Shaker associated with the failed system,
d) Crew procedures in the event the
remaining stall barrier fails are discussed,
e) If the remaining stall barrier fails the
minimum speed shall be no less than Vref
(1.3 Vs) for all phases of flight (this
minimum speed shall be cross referenced
to a normalized AOA value of 0.59 as
displayed on the PFD),
f) Weather at departure and destination is
considered,
g) Consideration is given to delaying takeoff
or approach and landing, if windshear is
forecast until such conditions cease, or
consideration is given to proceeding to
alternate, and
h) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar the
circuit breakers for the Stall Barrier
Valve and Stick Shaker associated
with the failed system. Prior to
dispatch, the flight crew will discuss
the dispatch situation with the stall
barrier inoperative and crew
procedures in the event the
remaining operative stall barrier
fails. If the remaining stall barrier
fails, the minimum speed shall be no
less than Vref (1.3 Vs) for all phases
of flight. This minimum speed shall
be cross-referenced to Normalized
Angle of Attack of 0.59 as displayed
on the PFD. Weather conditions at
the departure and destination
airports shall be considered. If there
are known or forecast windshear
conditions at the departure or
destination airport, the crew shall
consider delaying the takeoff or
approach and landing until such
conditions cease to exist, or
consider deviation to an alternate
airport in the approach and landing
case.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
STICK PUSH UNAVAIL
(Amber – Caution)
(GV)
(O)
2 - 120
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with one (1)
system inoperative provided:
a) Angle of Attack indication is available on
both PFD’s,
b) Alternate procedures are established and
used,
c) The inoperative stall barrier system is
electrically disabled by pulling and
collaring the Stall Barrier Valve and Stick
Shaker associated with the failed system,
d) Crew procedures in the event the
remaining stall barrier fails are discussed,
e) If the remaining stall barrier fails the
minimum speed shall be no less than Vref
(1.3 Vs) for all phases of flight (this
minimum speed shall be cross referenced
to a normalized AOA value of 0.59 as
displayed on the PFD),
f) Weather at departure and destination is
considered,
g) Consideration is given to delaying takeoff
or approach and landing, if windshear is
forecast until such conditions cease, or
consideration is given to proceeding to
alternate, and
h) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar the
SHAKER #1: POP E-6, SHAKER #2:
CPOP E-6, STALL BARR VALVE #1:
POP E-5, STALL BARR VALVE #2:
CPOP E-5, FLAP/STAB LEFT DC: POP
C-6 or FLAP / STAB RIGHT DC: CPOP
C-6 circuit breakers for the Stall Barrier
Valve and Stick Shaker associated with
the failed system. Prior to dispatch, the
flight crew will discuss the dispatch
situation with the stall barrier
inoperative and crew procedures in the
event the remaining operative stall
barrier fails. If the remaining stall
barrier fails, the minimum speed shall
be no less than Vref (1.3 Vs) for all
phases of flight. This minimum speed
shall be cross-referenced to Normalized
Angle of Attack of 0.59 as displayed on
the PFD. Weather conditions at the
departure and destination airports shall
be considered. If there are known or
forecast windshear conditions at the
departure or destination airport, the
crew shall consider delaying the takeoff
or approach and landing until such
conditions cease to exist, or consider
deviation to an alternate airport in the
approach and landing case.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Stick Push Unavailable
(Amber – Caution)
(GV-SP/GIV-X)
(O)
2 - 121
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with one (1)
system inoperative provided:
a) Angle of Attack indication is available on
both PFD’s,
b) Alternate procedures are established and
used,
c) The inoperative stall barrier system is
electrically disabled by pulling and
collaring the Stall Barrier Valve and Stick
Shaker associated with the failed system,
d) Crew procedures in the event the
remaining stall barrier fails are discussed,
e) If the remaining stall barrier fails the
minimum speed shall be no less than Vref
(1.3 Vs) for all phases of flight (this
minimum speed shall be cross referenced
to a normalized AOA value of 0.59 as
displayed on the PFD),
f) Weather at departure and destination is
considered,
g) Consideration is given to delaying takeoff
or approach and landing, if windshear is
forecast until such conditions cease, or
consideration is given to proceeding to
alternate, and
h) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will pull and collar the
SHAKER #1: POP E-6, SHAKER #2:
CPOP E-6, STALL BARR VALVE #1:
POP E-5, STALL BARR VALVE #2:
CPOP E-5, FLAP/STAB LEFT DC: POP
C-6 or FLAP / STAB RIGHT DC: CPOP
C-6 circuit breakers for the Stall Barrier
Valve and Stick Shaker associated with
the failed system. Prior to dispatch, the
flight crew will discuss the dispatch
situation with the stall barrier
inoperative and crew procedures in the
event the remaining operative stall
barrier fails. If the remaining stall
barrier fails, the minimum speed shall
be no less than Vref (1.3 Vs) for all
phases of flight. This minimum speed
shall be cross-referenced to Normalized
Angle of Attack of 0.59 as displayed on
the PFD. Weather conditions at the
departure and destination airports shall
be considered. If there are known or
forecast windshear conditions at the
departure or destination airport, the
crew shall consider delaying the takeoff
or approach and landing until such
conditions cease to exist, or consider
deviation to an alternate airport in the
approach and landing case.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
Stick Shake 1-2 Fail
(Blue – Advisory)
(GV)
2 - 122
3.
Limitations and/or Procedures
Operational Procedures
A
Airplane may be dispatched with a single
None required.
control column shaker inoperative provided:
a) Angle of Attack indication is available
on both PFD’s,
b) Both stall barrier systems are
operative, and
c) Repairs are made within two (2) flight
days.
A
Airplane may be dispatched with a single
None required.
control column shaker inoperative provided:
a) Angle of Attack indication is available
on both PFD’s,
b) Both stall barrier systems are
operative, and
c) Repairs are made within two (2) flight
days.
(Blue – Advisory)
(GV-SP/GIV-X)
STICK SHAKE 1-2 FL
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Stuck MIC ACP 3
(Blue – Advisory)
(GV-SP/GIV-X)
(continued)
(O)
2 - 123
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched with ACP 3
indicating stuck MIC provided:
a) Pilot and Copilot ACP’s are operative,
b) OBSERVER ACP: REER, D-7, is
pulled and collared,
c) Affected ACP is not required as
determined by the Pilot-in-Command,
d) Flight Deck to cabin communication is
operative,
e) A passenger seat in the passenger
cabin is made available to an FAA
inspector for the performance of
official duties,
f) Alternate procedures are established
and used,
g) Required minimum safety equipment
(safety belt and oxygen) is available,
h) Seat is acceptable to the FAA
inspector for performance of official
duties, and
i) Repairs are made within two (2) flight
days.
Operational Procedures
Flight crew will ensure:
a) Pilot and Copilot ACP’s are
operative,
b) OBSERVER ACP: REER D7, is pulled and collared,
c) Affected ACP is not required
as determined by the Pilotin-Command,
d) Flight Deck to cabin
communication is operative,
and
e) Alternate procedures are
established and used.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Stuck MIC ACP 3
2 - 124
3.
Limitations and/or Procedures
A
PAGE NO:
Operational Procedures
NOTE 1: These provisos are intended to
provide for occupancy of the above seats
by an FAA inspector when the minimum
safety equipment (oxygen and safety belt)
is functional and the inspector determines
the condition to be acceptable.
(Blue – Advisory)
(GV-SP/GIV-X) (cont’d)
NOTE 2: The pilot-in-command will
determine if the minimum safety equipment
is functional for other persons authorized to
occupy any observer seat(s).
S WSHLD FAIL, L-R
B
Airplane may be dispatched.
None required.
Airplane may be dispatched provided:
a) System is deactivated and secured by
pulling and collaring TCAS: POP, F-2
circuit breaker,
b) En route or approach procedures do
not require its use, and
c) Repairs are made within two (2) flight
days.
Flight crew will ensure:
a) System is deactivated and
secured by pulling and
collaring TCAS Power CB,
and
b) En route or approach
procedures do not require its
use.
(Amber – Caution)
(GV)
TCAS Fail
(Blue – Advisory)
(GV-SP/GIV-X)
A
(O)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
TCAS FAIL
A
Terrain 1-2 Fail
B
(Blue – Advisory)
(GV-SP/GIV-X)
Terrain Bus Fail
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
2 - 125
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
PAGE NO:
Operational Procedures
Airplane may be dispatched provided:
a) System is deactivated and secured by
pulling and collaring TCAS: POP, F-2
circuit breaker,
b) En route or approach procedures do
not require its use, and
c) Repairs are made within two (2) flight
days.
Flight crew will ensure:
a) System is deactivated and
secured by pulling and
collarin TCAS Power CB,
and
b) En route or approach
procedures do not require its
use.
Airplane may be dispatched.
None required.
NOTE: Synthetic Vision PFD synthetic
terrain will not be available with dual
Terrain Server failures, but the full PFD
may be used without restriction.
B
Airplane may be dispatched.
NOTE: Synthetic Vision PFD synthetic
terrain will not be available with dual
Terrain Server failures, but the full PFD
may be used without restriction.
None required.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
CAS Message
THROT QUAD 1-2 FL
B
B
(Blue – Advisory)
(GV)
None required.
Airplane may be dispatched.
None required.
NOTE: With both Channel 1 and Channel 2
failed, the autothrottle system will be
inoperative.
C
Airplane may be dispatched with any in
excess of those required by 14 CFR.
None required.
C
Airplane may be dispatched with any in
excess of those required by 14 CFR.
None required.
(Blue – Advisory)
(GV-SP/GIV-X)
VHF COMM 1-2 FAIL
Airplane may be dispatched.
Operational Procedures
NOTE: With both Channel 1 and Channel 2
failed, the autothrottle system will be
inoperative.
(Blue – Advisory)
(GV-SP/GIV-X)
VHF COM 1-2 Fail
2 - 126
3.
Limitations and/or Procedures
(Blue – Advisory)
(GV)
Throttle Quadrant 1-2 Fail
2.
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
WG A/I SYS FL, L-R
B
2 - 127
3.
Limitations and/or Procedures
Except for ER operations, airplane may be
dispatched with wing anti-ice system
inoperative provided airplane is not
operated in known or forecast icing
conditions.
(Amber – Caution)
(GV)
PAGE NO:
Operational Procedures
None required.
NOTE: Do not select affected side Wing
Anti-Ice to ON.
Windshear 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
A
(O)
Airplane may be dispatched provided:
a) At least one (1) radio altimeter is
operative,
b) Alternate procedures are established
and used,
c) Flight crew comply with AFM/AOM
guidance in windshear situations and
recommend procedures when
encountering windshear, and
d) Repairs are made within two (2) flight
days.
NOTE: Operator’s alternate procedures
should include reviewing windshear
avoidance and windshear recovery
procedures.
Flight crew will comply with
AFM/AOM guidance in
windshear situations and
recommend procedures when
encountering windshear and
verify both radio altimeters are
valid.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
WINDSHEAR FAIL
(Blue – Advisory)
(GV)
(O)
2 - 128
3.
Limitations and/or Procedures
A
PAGE NO:
Airplane may be dispatched provided:
a) At least one (1) radio altimeter is
operative,
b) Alternate procedures are established
and used,
c) Flight crew comply with AFM/AOM
guidance in windshear situations and
recommend procedures when
encountering windshear, and
d) Repairs are made within two (2) flight
days.
NOTE: Operator’s alternate procedures
should include reviewing windshear
avoidance and windshear recovery
procedures.
Operational Procedures
Flight crew will comply with
AFM/AOM guidance in
windshear situations and
recommend procedures when
encountering windshear and
verify both radio altimeters are
valid.
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
Wing Anti-Ice Sys Fail, L-R
B
2 - 129
3.
Limitations and/or Procedures
Except for ER operations, airplane may be
dispatched with wing anti-ice system
inoperative provided airplane is not
operated in known or forecast icing
conditions.
(Amber – Caution)
(GV-SP/GIV-X)
PAGE NO:
Operational Procedures
None required.
NOTE: Do not select affected side Wing
Anti-Ice to ON.
Yaw Damper 1-2 Fail
B
(O)
Except for ER operations, airplane may be
dispatched with one (1) channel inoperative
provided airplane is operated in
accordance with AFM Limitations in the
event the operative Yaw Damper fails.
Flight crew will ensure airplane is
operated in accordance with
AFM Limitations in the event the
operative Yaw Damper fails.
B
(O)
Except for ER operations, airplane may be
dispatched with one (1) channel inoperative
provided airplane is operated in
accordance with AFM Limitations in the
event the operative Yaw Damper fails.
Flight crew will ensure airplane is
operated in accordance with
AFM Limitations in the event the
operative Yaw Damper fails.
(Amber – Caution)
(GV-SP/GIV-X)
YD 1-2 FAIL
(Amber – Caution)
(GV)
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
YD 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
2 - 130
3.
Limitations and/or Procedures
Operational Procedures
B
(O)
Airplane may be dispatched with one
inoperative yaw damper system provided
the inoperative YAW DAMPER SERVO #1:
POP, D-6 or YAW DAMPER SERVO #2:
CPOP, D-6 circuit breaker is pulled and
collared.
Flight crew will ensure
inoperative servo circuit breaker
is pulled and collared.
C
(O)
Airplane may be dispatched provided:
a) L FREQ CONV: Left PDB or R FREQ
CONV: Right PDB circuit breaker is
pulled and collared,
b) Flight crew brief passengers on items
that are inoperative with the failure of
the power source for cabin
entertainment, and
c) Backup battery is available if EFB is
used.
Flight crew will pull and collar
affected circuit breaker. Flight
crew will brief the passengers on
the items that are inoperative
with the failure of the power
source for cabin entertainment.
(Blue – Advisory)
(GV-SP/GIV-X)
50 HZ Power Fail, L-R
PAGE NO:
GULFSTREAM AEROSPACE CORPORATION
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
1.
2.
CAS Message
60 HZ Power Fail, L-R
(Blue – Advisory)
(GV)
2 - 131
3.
Limitations and/or Procedures
Operational Procedures
C
(O)
Airplane may be dispatched provided:
a) Affected L FREQ CONV: Left PDB or
R FREQ CONV: Right PDB circuit
breaker is pulled and collared,
b) Flight crew brief passengers on items
that are inoperative with the failure of
the power source for cabin
entertainment, and
c) Backup battery is available if EFB is
used.
Flight crew will pull and collar
affected circuit breaker. Flight
crew will brief the passengers on
the items that are inoperative
with the failure of the power
source for cabin entertainment.
C
(O)
Airplane may be dispatched provided:
a) Affected L FREQ CONV: Left PDB or
R FREQ CONV: Right PDB circuit
breaker is pulled and collared,
b) Flight crew brief passengers on items
that are inoperative with the failure of
the power source for cabin
entertainment, and
c) Backup battery is available if EFB is
used.
Flight crew will pull and collar
affected circuit breaker. Flight
crew will brief the passengers on
the items that are inoperative
with the failure of the power
source for cabin entertainment.
(Blue – Advisory)
(GV-SP/GIV-X)
60HZ PWR FAIL, L-R
PAGE NO:

GULFSTREAM AEROSPACE CORPORATION
P.O. Box 2206, Savannah, Georgia 31402-2206
Telephone (912) 965-3000 Telex 3772775