GULFSTREAM
G100
MAINTENANCE / OPERATIONAL
PLACARDING PROCEDURES
MANUAL
Revision 5a
November 30, 2009
GAC Doc. No. G100-1
C
2009 Gulfstream Aerospace Corporation
DISCLAIMER FOR MAINTENANCE / OPERATIONAL / PLACARDING
PROCEDURES MANUAL (GAC DOC. NO. G100-1)
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.
©2009 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
ATA 21
AIR CONDITIONING ........................................................................................................................................................................................................................... 21-1
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
17.
18.
19.
20.
21.
22.
23.
ATA 22
Bleed Switching Valves..................................................................................................................................................................................................................... 21-1
Ram Air Check Valve........................................................................................................................................................................................................................ 21-1
Cabin Air Out-Flow Valves ............................................................................................................................................................................................................... 21-2
Air Conditioning System ................................................................................................................................................................................................................... 21-2
Automatic Temperature Control System ........................................................................................................................................................................................... 21-2
Manual Temperature Control System ................................................................................................................................................................................................ 21-2
Ground Cooling System .................................................................................................................................................................................................................... 21-3
Pilot’s Conditioned Air...................................................................................................................................................................................................................... 21-3
Cabin Differential Pressure Indicator ................................................................................................................................................................................................ 21-3
Cabin Rate of Climb Indicator........................................................................................................................................................................................................... 21-3
Cabin Altimeter ................................................................................................................................................................................................................................. 21-4
Cabin Altitude Warning..................................................................................................................................................................................................................... 21-4
Ditching Valve .................................................................................................................................................................................................................................. 21-4
Water Separator Temperature Control System .................................................................................................................................................................................. 21-5
Automatic Cabin Pressure Control System ........................................................................................................................................................................................ 21-5
Manual Pressurization System ........................................................................................................................................................................................................... 21-6
Landing Field Elevation Selector (A knob) ....................................................................................................................................................................................... 21-6
Barometric Adjustment Selector (B knob) ........................................................................................................................................................................................ 21-6
Cabin Rate Selector (R knob) ............................................................................................................................................................................................................ 21-7
CABIN / FUEL / RAT TEMP Indicator ........................................................................................................................................................................................... 21-7
Ground Bypass Valve ........................................................................................................................................................................................................................ 21-7
HP Bleed Air Duct Blow Out Discs .................................................................................................................................................................................................. 21-7
Cabin Overhead Airflow Vents (Wemacs / Gasper) .......................................................................................................................................................................... 21-8
AUTO FLIGHT ...................................................................................................................................................................................................................................... 22-1
1.
2.
3.
Autopilot System ............................................................................................................................................................................................................................... 22-1
Yaw Damper System ......................................................................................................................................................................................................................... 22-1
Autopilot Disconnect ......................................................................................................................................................................................................................... 22-1
i
TABLE OF CONTENTS
(CONTINUED)
ATA 23
COMMUNICATIONS ........................................................................................................................................................................................................................... 23-1
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
ATA 24
ELECTRICAL POWER ........................................................................................................................................................................................................................ 24-1
1.
2.
3.
4.
5.
6.
7.
8.
9.
ATA 25
DC Voltmeters ................................................................................................................................................................................................................................... 24-1
DC Ammeters .................................................................................................................................................................................................................................... 24-1
Inverters............................................................................................................................................................................................................................................. 24-1
AC Voltmeters ................................................................................................................................................................................................................................... 24-1
Battery Temperature Indicator .......................................................................................................................................................................................................... 24-1
Nose Compartment Blower ............................................................................................................................................................................................................... 24-2
External Power System ...................................................................................................................................................................................................................... 24-2
Baggage Compartment Heat .............................................................................................................................................................................................................. 24-2
60 Hertz AC Electrical System .......................................................................................................................................................................................................... 24-2
EQUIPMENT/FURNISHINGS ............................................................................................................................................................................................................. 25-1
1.
2.
3.
4.
5.
6.
7.
8.
ATA 26
Communications Systems (VHF, UHF) ............................................................................................................................................................................................ 23-1
Cockpit Voice Recorder (CVR) ........................................................................................................................................................................................................ 23-2
Passenger Address (PA) System ........................................................................................................................................................................................................ 23-2
Boom Microphones ........................................................................................................................................................................................................................... 23-3
Recorded Passenger Briefing System ................................................................................................................................................................................................ 23-4
Selective Call System (SELCAL) ...................................................................................................................................................................................................... 23-4
Cockpit Speakers ............................................................................................................................................................................................................................... 23-5
Headsets ............................................................................................................................................................................................................................................ 23-5
High Frequency (HF) Communication System .................................................................................................................................................................................. 23-5
Hand Held Microphones ................................................................................................................................................................................................................... 23-6
Flight Phone Systems ........................................................................................................................................................................................................................ 23-6
Automatic Cabin Briefing System ..................................................................................................................................................................................................... 23-6
Passenger Seat(s) ............................................................................................................................................................................................................................... 25-1
Passenger Convenience Item(s) ......................................................................................................................................................................................................... 25-1
Emergency Medical Equipment......................................................................................................................................................................................................... 25-2
Flotation Devices ............................................................................................................................................................................................................................... 25-2
Emergency Locator Transmitter (ELT) ............................................................................................................................................................................................. 25-2
“Fasten Seat Belt While Seated” Sign or Placard .............................................................................................................................................................................. 25-2
Cargo Restraint System(s) ................................................................................................................................................................................................................. 25-3
Life Rafts ........................................................................................................................................................................................................................................... 25-3
FIRE PROTECTION ............................................................................................................................................................................................................................. 26-1
1.
2.
3.
4.
Portable Fire Extinguishers ............................................................................................................................................................................................................... 26-1
Lavatory Smoke Detection System .................................................................................................................................................................................................... 26-1
Lavatory Fire Extinguisher System.................................................................................................................................................................................................... 26-1
Fire Bottle Thermal Discharge Indicator (Disc) ................................................................................................................................................................................ 26-1
ii
TABLE OF CONTENTS
(CONTINUED)
ATA 27
FLIGHT CONTROLS ........................................................................................................................................................................................................................... 27-1
1.
2.
3.
4.
5.
ATA 28
FUEL ....................................................................................................................................................................................................................................................... 28-1
1.
2.
3.
4.
5.
6.
ATA 29
Windshield Wipers ............................................................................................................................................................................................................................ 30-1
Pitot-Static Heater System ................................................................................................................................................................................................................. 30-1
Windshield Heat ................................................................................................................................................................................................................................ 30-1
Pneumatic De-icing Boot System ...................................................................................................................................................................................................... 30-1
Surface De-icing System Control ...................................................................................................................................................................................................... 30-2
Defog System .................................................................................................................................................................................................................................... 30-2
Engine Inlet Anti-Icing Valve (TAI Valve) ....................................................................................................................................................................................... 30-2
INDICATING/RECORDING SYSTEM .............................................................................................................................................................................................. 31-1
1.
2.
3.
4.
ATA 32
Hydraulic Tank Pressurization .......................................................................................................................................................................................................... 29-1
ICE AND RAIN PROTECTION........................................................................................................................................................................................................... 30-1
1.
2.
3.
4.
5.
6.
7.
ATA 31
Interconnect Valves ........................................................................................................................................................................................................................... 28-1
Transfer Valves ................................................................................................................................................................................................................................. 28-1
Jettison Valves................................................................................................................................................................................................................................... 28-1
Fuel Low Level Light ........................................................................................................................................................................................................................ 28-1
Pressure Fueling System .................................................................................................................................................................................................................... 28-1
Fuel Management Indicator ............................................................................................................................................................................................................... 28-2
HYDRAULIC POWER ......................................................................................................................................................................................................................... 29-1
1.
ATA 30
Slat and Flap Position Indicator ........................................................................................................................................................................................................ 27-1
Horizontal Stabilizer Trim Indicator ................................................................................................................................................................................................. 27-1
Aileron Trim Indicator ...................................................................................................................................................................................................................... 27-1
Rudder Trim Indicator ....................................................................................................................................................................................................................... 27-1
Automatic Slat Extension System ...................................................................................................................................................................................................... 27-1
Clocks ................................................................................................................................................................................................................................................ 31-1
Flight Data Recorder (FDR) System ................................................................................................................................................................................................. 31-1
Cockpit Voice Recorder .................................................................................................................................................................................................................... 31-2
Flight Hour Recorder......................................................................................................................................................................................................................... 31-2
LANDING GEAR ................................................................................................................................................................................................................................... 32-1
1.
Antiskid System................................................................................................................................................................................................................................. 32-1
iii
TABLE OF CONTENTS
(CONTINUED)
ATA 33
LIGHTS ................................................................................................................................................................................................................................................... 33-1
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
Cockpit / Flight Deck / Flight Compartment and Instrument Lighting .............................................................................................................................................. 33-1
Cabin Interior Illumination System ................................................................................................................................................................................................... 33-1
Passenger Notice System (Fasten Seat Belts, No Smoking) .............................................................................................................................................................. 33-1
Baggage Compartment Light System ................................................................................................................................................................................................ 33-1
Anti-Collision Light System (Top and / or Bottom Strobes) ............................................................................................................................................................. 33-2
Wing Tip Strobes .............................................................................................................................................................................................................................. 33-2
Taxi Light System ............................................................................................................................................................................................................................. 33-2
Landing Light System........................................................................................................................................................................................................................ 33-2
Wing Inspection Lights ..................................................................................................................................................................................................................... 33-2
Position Lights System ...................................................................................................................................................................................................................... 33-2
Emergency Exit Lighting System ...................................................................................................................................................................................................... 33-3
Floor Proximity Emergency Escape Path Marking System Lights .................................................................................................................................................... 33-3
Strobes ............................................................................................................................................................................................................................................... 33-3
Pulselite Landing Light System ......................................................................................................................................................................................................... 33-3
Logo Lights ....................................................................................................................................................................................................................................... 33-3
iv
TABLE OF CONTENTS
(CONTINUED)
ATA 34
NAVIGATION ........................................................................................................................................................................................................................................ 34-1
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
17.
18.
19.
20.
21.
22.
23.
24.
25.
26.
27.
28.
29.
30.
31.
32.
33.
34.
ATA 35
Mach / Airspeed Indicator ................................................................................................................................................................................................................. 34-1
Mach / Airspeed Overspeed Warning System ................................................................................................................................................................................... 34-1
RAT / CABIN / FUEL TEMP Indicator ........................................................................................................................................................................................... 34-1
Turn and Bank Indicator.................................................................................................................................................................................................................... 34-2
Vertical Navigation System ............................................................................................................................................................................................................... 34-2
Flight Director System....................................................................................................................................................................................................................... 34-2
Distance Measuring Equipment (DME) ............................................................................................................................................................................................ 34-2
Marker Beacon Receiver ................................................................................................................................................................................................................... 34-2
Weather Radar ................................................................................................................................................................................................................................... 34-2
Automatic Direction Finding (ADF) System ..................................................................................................................................................................................... 34-3
Radio Magnetic Indicator (RMI) ....................................................................................................................................................................................................... 34-3
AOA Indicator ................................................................................................................................................................................................................................... 34-3
Navigation Equipment (VOR / ILS, Loran, RNAV, Omega / VLF, INS, GPS, Doppler, FMS) ....................................................................................................... 34-3
Radio Altimeter ................................................................................................................................................................................................................................. 34-3
Multi-Function Display (MFD) Symbol Generator ........................................................................................................................................................................... 34-4
ATC Transponders and Automatic Altitude Reporting Systems ....................................................................................................................................................... 34-4
Altitude Alerting System ................................................................................................................................................................................................................... 34-5
Remote Tuning Unit (RTU) .............................................................................................................................................................................................................. 34-5
Airborne Flight Information System .................................................................................................................................................................................................. 34-5
Maintenance Diagnostic System ........................................................................................................................................................................................................ 34-5
Ground Proximity Warning System (GPWS) .................................................................................................................................................................................... 34-6
Air Data Computers (ADC) ............................................................................................................................................................................................................... 34-8
Non-Stabilized Magnetic Compass ................................................................................................................................................................................................... 34-9
Traffic Collision and Avoidance System I (TCAS I) ...................................................................................................................................................................... 34-10
Traffic Collision and Avoidance System II (TCAS II) .................................................................................................................................................................... 34-10
Moving Map Display....................................................................................................................................................................................................................... 34-12
Windshear Detection and Guidance System .................................................................................................................................................................................... 34-12
Flight Management System (FMS) .................................................................................................................................................................................................. 34-12
Navigation Management System ..................................................................................................................................................................................................... 34-13
Stormscope ...................................................................................................................................................................................................................................... 34-13
Windshear Warning and Flight Guidance System ........................................................................................................................................................................... 34-13
Windshear Detection and Avoidance System .................................................................................................................................................................................. 34-14
Automatic Dependent Surveillance – Broadcast (ADS – B) System............................................................................................................................................... 34-14
Standby Altitude Indicator............................................................................................................................................................................................................... 34-15
OXYGEN ................................................................................................................................................................................................................................................ 35-1
1. Oxygen System and Supply (Passenger) ........................................................................................................................................................................................... 35-1
2. Oxygen Blow Out Disc...................................................................................................................................................................................................................... 35-1
3. Protective Breathing Equipment ........................................................................................................................................................................................................ 35-1
v
TABLE OF CONTENTS
(CONTINUED)
ATA 49
AIRBORNE AUXILIARY POWER ..................................................................................................................................................................................................... 49-1
1. Auxiliary Power Unit (APU) ............................................................................................................................................................................................................. 49-1
2. APU Generator .................................................................................................................................................................................................................................. 49-1
ATA 52
DOORS .................................................................................................................................................................................................................................................... 52-1
1.
ATA 77
ENGINE INDICATING ......................................................................................................................................................................................................................... 77-1
1.
2.
3.
4.
5.
6.
ATA 78
N1 Indicator Digital Display ............................................................................................................................................................................................................. 77-1
N2 Indicator Digital Display ............................................................................................................................................................................................................. 77-1
ITT Indicator Digital Display ............................................................................................................................................................................................................ 77-1
Automatic Power Reserve (APR) (SPX only) ................................................................................................................................................................................... 77-1
Engine Synchronizer (ENG SYNC) .................................................................................................................................................................................................. 77-1
Liquid Crystal Displays ..................................................................................................................................................................................................................... 77-1
ENGINE EXHAUST .............................................................................................................................................................................................................................. 78-1
1.
ATA 79
Door Warning Light System .............................................................................................................................................................................................................. 52-1
Thrust Reversing System ................................................................................................................................................................................................................... 78-1
ENGINE OIL .......................................................................................................................................................................................................................................... 79-1
1.
Low Oil Pressure Warning Light ....................................................................................................................................................................................................... 79-1
vi
General Information
Gulfstream has developed this manual to assist operators in development of their Maintenance, Operational and
Placarding Procedures (MOP) for the Gulfstream G100 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 G100 Master Minimum Equipment List (MMEL), Revision 5a, dated November 30, 2009. 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 FAR 121, 125, 129 and 135 operations as specified in the preamble. FAR 91
operators must obtain a FAR 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 number following the
assigned FAA revision number, e.g., first update will be reflected as Revision 4.a.
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 is accomplished by this revision of the G100 Maintenance, Operational, and Placarding Manual. Users
should review and become familiar with the manual.
1.
2.
3.
Incorporated latest revision of the MMEL.
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.
vii
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21.
1.
2.
21-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
AIR CONDITIONING
Bleed Switching
Valves
Ram Air Check
Valve
C
2
1
(M) One may be inoperative provided the
airplane is not operated above FL 250.
Prior to flight, close the
None required.
inoperative Bleed Switching
Valve (BSV) by ensuring the
circuit breaker for the
inoperative BSV is in and
placing the CABIN AIR selector
to the engine with the operating
BSV. Then visually check that
the inoperative BSV butterfly
valve is closed by observing that
the indicator shows closed.
Place a placard in the cockpit
stating that the aircraft may not
be operated above 25,000 feet
MSL. An inoperative placard
will be placed adjacent to the
ECS panel and will be noted
on the ADLS.
C
2
0
(M) May be inoperative provided:
a) Affected valves are closed,
b) The airplane is operated
unpressurized and
c) Ram air is selected.
Prior to flight, close the
None required.
inoperative Bleed Switching
Valves (BSV) by ensuring the
circuit breakers for the
inoperative BSV are in, and
placing the CABIN AIR selector
to the RAM AIR position. Then
visually check that the
inoperative BSV butterfly
valves are closed by observing
that the indicators show closed.
Place a placard in the cockpit
that states the aircraft may not
be operated pressurized and
that the “Oxygen requirements
as outlined in FAR 91.211
MUST BE OBSERVED”. An
inoperative placard will be
placed adjacent to the ECS
panel and will be noted on the
ADLS.
C
1
0
May be inoperative in the open position
provided aircraft is operated unpressurized.
None required.
Place a placard in the cockpit
that states the aircraft may not
be operated pressurized. An
inoperative placard will be
placed adjacent to the ECS
panel and will be noted on the
ADLS.
21-1
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21.
21-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
AIR CONDITIONING
3.
Cabin Air Out-Flow
Valves
C
2
0
(M) May be inoperative provided:
a) Affected valves are secured in
the open position, and
b) The airplane is operated
unpressurized below 10,000 feet
MSL.
The outflow valve may be
None required.
secured open by removing the
floor panel above the outflow
valves. Manually open the
outflow valve and secure it open
with .032 safety wire or larger.
Replace floor panel.
4.
Air Conditioning
System
C
1
0
May be inoperative provided:
a) Aircraft is operated
unpressurized, and
b) Aircraft is operated at or below
10,000 feet MSL.
None required.
None required.
Place a placard in the
cockpit that states the
aircraft may not be operated
pressurized. An inoperative
placard will be placed
adjacent to the ECS panel
and will be noted on the
ADLS.
5.
Automatic Temperature
Control System
C
1
0
May be inoperative provided the manual
temperature control system operates
normally.
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
6.
Manual Temperature
Control System
C
1
0
May be inoperative provided the automatic
temperature control system operates
normally.
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
21-2
Place a placard in the cockpit
that states the aircraft may not
be operated pressurized and
that the “Oxygen
requirements as outlined in
FAR 91.211 MUST BE
OBSERVED”. An
inoperative placard will be
placed adjacent to the ECS
panel and will be noted on
the ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21-3
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
21.
AIR CONDITIONING
7.
Ground Cooling System
C
1
0
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
8.
Pilot’s Conditioned Air
C
1
0
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
9.
Cabin Differential
Pressure Indicator
C
1
0
May be inoperative provided:
a) Cabin altitude indicator is
operative,
b) Cabin altitude warning system is
operative,
c) Cabin rate of climb indicator is
operative and
d) A chart is provided to the crew
for converting cabin altitude to
differential pressure.
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
C
1
0
May be inoperative provided aircraft is
operated unpressurized at or below 10,000
feet MSL.
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
C
1
0
May be inoperative provided all other
components of the pressure control system
are operative.
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
10. Cabin Rate of Climb
Indicator
21-3
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21.
21-4
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
AIR CONDITIONING
11. Cabin Altimeter
C
1
0
May be inoperative provided:
None required.
a) Cabin differential pressure
indicator is operative,
b) Cabin altitude warning system is
operative and
c) A chart is provided to the crew to
convert cabin differential
pressure to cabin altitude.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
C
1
0
May be inoperative provided:
a) Aircraft is operated
unpressurized and
b) Aircraft is operated at or below
10,000 feet MSL.
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
12. Cabin Altitude Warning
System
C
1
0
May be inoperative provided the aircraft is
operated unpressurized at or below 10,000
feet MSL.
None required.
Ensure RAM AIR is selected
on Cabin Air Selector.
Place a placard in the
cockpit that states the
aircraft may not be operated
pressurized. An inoperative
placard will be placed
adjacent to the ECS panel
and will be noted on the
ADLS.
13. Ditching Valve
C
1
0
May be inoperative provided extended
overwater flights are not conducted.
None required.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
21-4
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21.
21-5
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ’D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
AIR CONDITIONING
14. Water Separator
Temperature Control
System
C
1
0
May be inoperative provided the airplane is None required.
operated unpressurized.
Ensure RAM AIR is selected
on Cabin Air Selector.
Place a placard in the
cockpit that states the
aircraft may not be operated
pressurized. An inoperative
placard will be placed
adjacent to the ECS panel
and will be noted on the
ADLS.
15. Automatic Cabin
Pressure Control
System
C
1
0
(M) May be inoperative provided:
a) Cabin air out-flow valves are
secured in the open position and
b) The airplane is operated
unpressurized at or below 10,000
feet.
The outflow valve may be
Ensure RAM AIR is selected
secured open by removing the
on Cabin Air Selector.
floor panel above the outflow
valves. Manually open the
outflow valve and secure it open
with .032 safety wire or larger.
Replace the floor panel.
Place a placard in the
cockpit that states the
aircraft may not be operated
pressurized and that the
“Oxygen requirements as
outlined in FAR 91.211
MUST BE OBSERVED”.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
C
1
0
May be inoperative providing the manual
pressurization system is operative.
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
21-5
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21.
21-6
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
AIR CONDITIONING
16. Manual Pressurization
System
C
1
0
May be inoperative provided automatic
cabin pressure control system is operative.
C
1
0
17. Landing Field Elevation
Selector (A knob)
C
1
18. Barometric Adjustment
Selector (B knob)
C
1
None required.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
May be inoperative provided the airplane is None required.
operated unpressurized at or below 10,000
feet MSL.
Ensure RAM AIR is selected
on Cabin Air Selector.
Place a placard in the
cockpit that states the
aircraft may not be operated
pressurized. An inoperative
placard will be placed
adjacent to the ECS panel
and will be noted on the
ADLS.
0
May be inoperative provided:
a) All other components of
pressurization control system are
operative and
b) Cabin is unpressurized prior to
landing.
None required.
None required.
Place a placard in the
cockpit that states the
aircraft may not be landed
pressurized. An inoperative
placard will be placed
adjacent to the CABIN
PRESSURE selector and
will be noted on the ADLS.
0
May be inoperative provided:
a) All other components of
pressurization control system are
operative and
b) Cabin is unpressurized prior to
landing.
None required.
None required.
Place a placard in the
cockpit that states the
aircraft may not be landed
pressurized. An inoperative
placard will be placed
adjacent to the CABIN
PRESSURE and will be
noted on the ADLS.
21-6
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21.
21-7
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
AIR CONDITIONING
19. Cabin Rate Selector
(R knob)
C
0
May be inoperative provided:
a) All other components of
pressurization control system are
operative and
b) Cabin is unpressurized prior to
landing.
None required.
None required.
Place a placard in the
cockpit that states the
aircraft may not be landed
pressurized. An inoperative
placard will be placed
adjacent to the CABIN
PRESSURE selector and
will be noted on the 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.
None required.
To ensure the GROUND BYPASS valve is closed, select
RAM AIR on the air selector
switch and operate the right
engine to approximately 50%
N1. There should be no
airflow in the cabin.
An inoperative placard will
be placed adjacent to the
ECS panel and will be noted
on the ADLS.
20. CABIN / FUEL / RAT
TEMP Indicator
Cabin Temp Mode
21. Ground Bypass
Valve
C
1
0
C
1
0
(O) May be inoperative in the closed
position.
21-7
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
21.
21-8
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
AIR CONDITIONING
22. HP Bleed Air Duct
Blow Out Discs
C
2
0
23. Cabin Overhead
Airflow Vents
(Wemacs / Gasper)
D
-
-
(M)
The HP bleed air duct blow out
disk may be checked to ensure
there is no leak by operating the
respective engine and ensuring
no airflow is exiting from the
port. This check must be
accomplished prior to each
flight until the blow out disk is
replaced.
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.
21-8
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
22.
AUTO FLIGHT
1.
Autopilot System
22-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
1)
One Autopilot System B
Installed
1
0
(M) (O) May be inoperative provided:
a) En route operations, including
RVSM, RNP-5 and RNP-10, and
approach procedures do not
require its use and
b) AFM limitations are observed.
Ensure the autopilot circuit
breaker is in and the autopilot
annunciation on PFD is flashing
red.
Pilots must not engage
autopilot and must observe
AFM limitations.
Place a placard in the cockpit
stating that the autopilot is to
remain disengaged. An
inoperative placard will be
placed on the autopilot panel
and will be noted on ADLS.
2)
Two or more
Autopilot Systems
Installed
C
-
1
(M) (O) May be inoperative provided
remaining system(s) operate normally.
Ensure the inoperative autopilot
circuit breaker is in, and the
annunciation for inoperative
autopilot is activated.
Pilot must not engage
inoperative autopilot and
must observe AFM
limitations.
Place a placard in the cockpit
stating that the inoperative
autopilot is to remain
disengaged. An inoperative
placard will be placed on the
autopilot panel and will be
noted on ADLS.
2.
Yaw Damper System
C
1
0
(M) (O) May be inoperative provided:
a) En route operations, including
RVSM, RNP-5 and RNP-10, do
not require its use and
b) AFM limitations are observed.
Ensure the autopilot circuit
breaker is in and the white YD
DISENG annunciator is
illuminated on the PFDs.
Pilots must not engage yaw
damper and must observe
AFM limitations.
Place a placard in the cockpit
stating that the yaw damper
system is to remain
disengaged. An inoperative
placard will be placed on the
autopilot panel and will be
noted on ADLS.
3.
Autopilot Disconnect
C
-
-
One may be inoperative provided the
autopilot is not utilized at less than initial
approach altitude.
None required
None required.
An inoperative placard will
be placed on the autopilot
panel and will be noted on
ADLS.
22-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
23.
COMMUNICATIONS
1.
Communication Systems
(VHF, UHF)
1)
23-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
D
-
-
a) Frequency Transfer C
Light
-
b) Frequency
Transfer Switch
C
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
Any in excess of those required by FAR
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.
An inoperative placard will
be placed 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 placed 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 placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
c) Frequency Selector C
Knob
-
2
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) Frequency
Indication
-
2
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.
VHF Comm
C
23-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
23.
2.
3.
23-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
COMMUNICATIONS
Cockpit Voice
Recorder (CVR)
(With Flight Data
Recorder (FDR) installed)
A
1
0
May be inoperative provided:
a) Flight Data Recorder (FDR)
operates normally and
b) Repairs are made within three
flight days.
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.
Cockpit Voice
Recorder (CVR)
(Without Flight Data
Recorder (FDR) installed)
A
1
0
May be inoperative provided repairs are
made within three flight days.
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
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.
Pilots must ensure that
passengers are adequately
briefed verbally regarding
normal and emergency
procedures, and operating
restrictions.
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:
a) PA not required by FAR and
b) Alternate, normal and emergency
procedures and / or operating
restrictions are established and
used.
None required.
Pilots must ensure that
passengers are adequately
briefed verbally regarding
normal and emergency
procedures, and operating
restrictions.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Passenger Address
(PA) System
1)
Passenger
Configuration
NOTE: Any station function (s) that
operate normally may be used.
23-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
23.
3.
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
5.
3.
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
6.
7.
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
COMMUNICATIONS
Passenger Address (PA) System
(continued)
2)
4.
23-3
NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
PAGE NUMBER:
Cargo Configuration
D
1
0
May be inoperative provided procedures do None required.
not require its use.
None required.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
Boom Microphones
(COCKPIT VOICE RECORDER
WITH FLIGHT DATA
RECORDER INSTALLED)
1)
Cockpit Voice
A
Recorder equipped to
record Boom Microphones
per FAR 135.151 (d) or
121.139 (g).
-
0
May be inoperative provided:
a) Flight Data Recorder (FDR)
operates normally and
b) Repairs are made within three
flight days.
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)
Cockpit Voice
D
Recorder not equipped
to record Boom
Microphones.
-
0
Any in excess of those required by FAR
may be inoperative.
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 on Next Page)
23-3
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
23.
4.
23-4
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
COMMUNICATIONS
Boom Microphones
(Continued)
(COCKPIT VOICE RECORDER
WITHOUT FLIGHT DATA
RECORDER INSTALLED)
1)
Cockpit Voice
A
Recorder equipped to
record Boom Microphones
per FAR 135.151 (d) or
121.139 (g).
-
0
May be inoperative provided repairs are
made within three flight days.
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)
Cockpit Voice
D
Recorder not equipped to
record Boom Microphones.
-
0
Any in excess of those required by FAR
may be inoperative.
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.
(O)
None required.
Pilots must ensure that
passengers are adequately
briefed.
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.
5. Recorded Passenger
*** Briefing System
C
1
0
6. Selective Call System
*** (SELCAL)
C
1
0
23-4
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
23.
23-5
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
COMMUNICATIONS
7.
Cockpit Speakers
C
2
0
May be inoperative provided headsets are
installed and operate normally.
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.
Headsets
C
2
1
One pilot’s headset may be inoperative
provided operations do require its use and
both pilot cockpit speakers operate
normally.
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.
High Frequency (HF)
Communication System
D
-
-
Any in excess of those required by FAR
may be inoperative.
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
-
1
(O) May be inoperative while conducting
operations that require two LRCS
provided:
a) SATCOM (High or Low Gain)
Data Link system operates
normally, and
b) SATCOM Data Link
communication operates
normally over the intended route
of the flight.
None required.
Flight crew must ensure that
SATCOM Data Link system
is operating normally.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
23-5
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
23.
23-6
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
COMMUNICATIONS
10. Hand Held Microphones
C
-
0
11. Flight Phone
*** Systems
D
-
0
12. Automatic Cabin
*** Briefing System
D
May be inoperative provided:
a) Both cockpit crewmembers use a
boom microphone and
b) Both control wheel push-to-talk
switches operate normally.
(O) May be inoperative provided alternate
procedures are established and used.
23-6
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.
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.
None required.
Pilots must ensure that
passengers are adequately
briefed verbally regarding
normal and emergency
procedures, and operating
restrictions.
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 G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
24.
24-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
ELECTRICAL POWER
1.
DC Voltmeters
DELETED REVISION 2
2.
DC Ammeters
DELETED REVISION 2
3.
Inverters
B
2
1
One may be inoperative provided airplane
is operated in day Visual Meteorological
Conditions (VMC).
None required.
None required.
An inoperative placard will
be placed on the overhead
panel and will be noted on
ADLS.
Inverters
(AHRS Equipped)
B
2
1
One may be inoperative provided:
a) Aircraft is equipped with the
Collins AHRS system and
b) All other ac electrical system
components are operative.
None required.
None required.
An inoperative placard will
be placed on the overhead
panel and will be noted on
ADLS.
4.
AC Voltmeters
B
2
1
One may be inoperative.
None required.
None required.
An inoperative placard will
be placed on the overhead
panel and will be noted on
ADLS.
5.
Battery Temperature
Indicator
C
1
0
One may be inoperative provided NI-CAD
batteries are not installed.
None required.
None required.
An inoperative placard will
be placed adjacent to the
battery temperature indicator
and will be noted on ADLS.
24-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
24-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
24.
ELECTRICAL POWER
6.
Nose Compartment
Blower
C
-
0
7.
External Power System
C
1
0
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
May be inoperative provided AFM
procedures are observed.
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.
None required.
None required.
An inoperative placard will
be placed on the overhead
panel and will be noted on
ADLS.
8.
Baggage
Compartment Heat
C
1
0
(M) May be inoperative provided:
Pull and tag Baggage
Baggage Compartment Heat Switch is Compartment Heat circuit
in the OFF position for the duration of breakers.
the flight.
None required.
An inoperative placard will
be placed on the overhead
panel and will be noted on
ADLS.
9.
60 Hertz AC
Electrical System
C
1
0
(M)
None required.
An inoperative placard will
be placed on the overhead
panel and will be noted on
ADLS.
Pull and tag 60 Hz CNTL
circuit breaker.
24-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
25-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
1.
Passenger Seat(s)
C
-
-
May be inoperative provided:
a) Seat does not block an
emergency exit,
b) Seat does not restrict any
passenger from access to the
main aircraft aisle and
c) Affected seat(s) is blocked and
placarded "DO NOT OCCUPY".
None required.
None required.
A placard stating “DO NOT
OCCUPY” will be placed on
each affected seat and will be
noted on ADLS.
None required.
None required.
A placard stating “SEAT
MUST REMAIN SECURED
IN UPRIGHT POSITION”
will be placed on each
affected seat and will be
noted on ADLS.
NOTE 1: A seat with an inoperative
seatbelt is considered to be inoperative.
NOTE 2: Affected seat(s) may include the
seat(s) behind and / or adjacent outboard
seats.
1) Recline Mechanism
C
-
-
May be inoperative and seat occupied
provided seat is secured in the upright
position.
25-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
25-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
2.
Passenger
Convenience Item(s)
-
0
Passenger convenience items, as expressed
in this MMEL, are those related to
passenger convenience, comfort or
entertainment such as, but not limited to
galley equipment, ash trays, stereo
equipment, overhead reading lamps. Items
addressed elsewhere in this document shall
not be included. (M) or (O) procedures
may be required and included in the air
carriers appropriate document.
None required.
None required.
An inoperative placard will
be adjacent to the inoperative
item and will be noted on
ADLS.
NOTE: EXTERIOR LAVATORY DOOR
ASHTRAYS ARE NOT CONSIDERED
CONVENIENCE ITEMS.
3.
Emergency Medical
Equipment
D
-
-
Any in excess of those required by FAR
may be inoperative or missing provided
required distribution is maintained.
None required.
None required.
If installed, an inoperative
placard will be placed on first
aid kit cover and will be
noted on ADLS.
4.
Flotation Devices
D
-
-
Any in excess of those required by FAR
may be inoperative or missing.
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.
25-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
25-3
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
5.
Emergency Locator
Transmitter (ELT)
C
1
0
As required by FAR.
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
1
0
May be inoperative for published
scheduled flights in scheduled air carrier
service.
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.
6.
“Fasten Seat Belt While
Seated” Sign or Placard
C
-
-
One or more signs or placards may be
illegible or missing provided a legible sign
or placard is visible from each occupied
passenger seat.
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.
Cargo Restraint System(s)
C
-
-
(O) May be inoperative or missing
provided acceptable cargo loading limits
from an approved source, i.e., an Approved
Cargo Loading Manual, Cargo Handling
Manual or Weight and Balance Documents
are observed.
None required.
Flight crew will comply with
proviso in Remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
-
May be inoperative or missing provided
procedures are established and used to
ensure the associated compartment remains
empty, or is verified to contain only empty
Cargo Handling Equipment, Ballast and /
or Fly Away Kits.
None required.
Flight crew will comply with
proviso in Remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
25-3
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
25-4
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
25. EQUIPMENT/FURNISHINGS
8. Life Rafts
D
-
-
Any in excess of those required by FAR
may be inoperative or missing.
25-4
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 G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
26.
26-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
FIRE PROTECTION
1.
Portable Fire
Extinguishers
D
2.
Lavatory Smoke
Detection System
DELETED REVISION 2.
3.
Lavatory Fire
Extinguisher System
DELETED REVISION 2.
4.
Fire Bottle Thermal
Discharge Indicator
(Disc)
C
-
2
-
0
Any in excess of those required by FAR
may be inoperative or missing provided:
a) The inoperative fire extinguisher
is tagged inoperative, removed
from the installed location and
placed out of sight so it can not
be mistaken for a functional unit
and
b) Required distribution is
maintained.
(M) May be inoperative provided the
pressure gage on the bottle(s) is checked
for correct pressure prior to each departure.
26-1
None required.
None required.
If installed, an inoperative
placard will be placed on
pressure charge gage of
affected extinguisher and will
be noted on ADLS.
Prior to each flight the pressure
gage on each engine fire bottle
must be checked to verify the
bottle is full.
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 G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
27.
27-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
FLIGHT CONTROLS
1.
Slat and Flap
Position Indicator
DELETED REVISION 2.
2.
Horizontal Stabilizer
Trim Indicator
C
1
0
May be inoperative provided:
a) Flight crew verifies by visual
inspection that stabilizer setting
agrees with trim markings on
vertical fin before each flight and
b) Rudder and aileron trim
indicators are operative.
None required.
None required.
An inoperative placard will
be placed on control pedestal
and will be noted on ADLS.
3.
Aileron Trim
Indicator
C
1
0
May be inoperative provided:
a) Flight crew verifies by visual
inspection that ailerons are in
neutral position before each
flight and
b) Horizontal stabilizer and rudder
trim indicators are operative.
None required.
None required.
An inoperative placard will
be placed on control pedestal
and will be noted on ADLS.
4.
Rudder Trim
Indicator
C
1
0
May be inoperative provided:
a) Flight crew verifies by visual
inspection that rudder trim is
neutral before each flight and
b) Horizontal stabilizer and aileron
trim indicators are operative.
None required.
None required.
An inoperative placard will
be placed on control pedestal
and will be noted on ADLS.
5.
Automatic Slat
Extension System
C
1
0
May be inoperative provided:
a) The airplane is not operated into
known or forecast icing
conditions.
b) The airplane is operated in day
VMC and
c) AFM limitations are complied
with.
None required.
None required.
An inoperative placard will
be placed on control pedestal
and will be noted on ADLS.
27-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
28.
28-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
FUEL
1.
Interconnect Valves
C
2
1
One may be inoperative provided fuel
jettison system is operative.
None required.
None required.
An inoperative placard will
be placed on overhead panel
and will be noted on ADLS.
2.
Transfer Valves
C
2
1
One may be inoperative provided:
a) Fuel is limited to 4000 lbs.
maximum and
b) Interconnect valves operate
normally.
None required.
None required.
An inoperative placard will
be placed on overhead panel
and will be noted on ADLS.
3.
Jettison Valves
C
2
1
One may be inoperative provided
interconnect valves operate normally.
None required.
None required.
An inoperative placard will
be placed on overhead panel
and will be noted on ADLS.
C
2
0
May be inoperative provided:
a) Airplane is not operated above
18,000 lbs takeoff weight and
b) Interconnect valves operate
normally.
None required.
None required.
An inoperative placard will
be placed on overhead panel
and will be noted on ADLS.
Fuel Low Level
Light
C
1
0
May be inoperative provided fuel quantity
displays operate normally.
None required.
None required.
An inoperative placard will
be placed on center
instrument panel and will be
noted on ADLS.
5. Pressure Fueling
System
C
1
0
None required.
Flight crew to use gravity
refueling procedures.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4.
28-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
28.
6.
28-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ’D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
FUEL
Fuel Management Indicator
1)
Wing Tank Fuel
Quantity Display
C
2
1
One may be inoperative provided:
a) All other functions of fuel
management indicator are
operative,
b) Fuel transfer valves are operative
and
c) A minimum fuel quantity of
4000 lbs. is required for takeoff.
None required.
None required.
An inoperative placard will
be placed on center
instrument panel and will be
noted on ADLS.
2)
Fuselage Tank Fuel
Display
C
1
0
May be inoperative provided:
a) All other functions of fuel
management indicator are
operative and
b) Fuel transfer valves are
operative.
None required.
None required.
An inoperative placard will
be placed on center
instrument panel and will be
noted on ADLS.
3)
Fuel Consumed
Display
C
1
0
May be inoperative provided all other
functions of fuel management indicator are
operative.
None required.
None required.
An inoperative placard will
be placed on center
instrument panel and will be
noted on ADLS.
4)
Fuel Remaining
Display
C
1
0
May be inoperative provided all other
functions of fuel management indicator are
operative.
None required.
None required.
An inoperative placard will
be placed on center
instrument panel and will be
noted on ADLS.
(Continued on Next Page)
28-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
28.
6.
28-3
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ’D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
FUEL
Fuel Management
Indicator
(Continued)
5)
Fuel Flow
Display
C
2
1
One may be inoperative provided:
a) Fuel quantity indicators are
operative,
b) Remaining engine indicators for
the associated engine are
operative.
c) Fuel flow on flight management
system is operative.
28-3
None required.
None required.
An inoperative placard will
be placed on center
instrument panel and will be
noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
29.
1.
29-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
HYDRAULIC POWER
Hydraulic Tank
Pressurization
C
1
0
May be inoperative provided:
a) All other hydraulic components
are operative,
b) Aircraft is not operated above FL
350 and
c) Landing gear is not extended or
operated above 8,000 ft altitude.
29-1
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.
PAGE NUMBER:
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
30.
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
30-1
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
ICE AND RAIN PROTECTION
1.
Windshield Wipers
C
2
-
May be inoperative provided the airplane is None required.
not operated in precipitation within 5 NM
of the airport of takeoff or intended
landing.
None required.
An inoperative placard will
be placed adjacent to
WINDSHIELD WIPERS
switches and will be noted on
ADLS.
2.
Pitot-Static Heater
System
B
2
1
(O) One may be inoperative, except where
en route operations, including RVSM,
RNP-5 and RNP-10, require its use
provided:
a) The airplane is not operated into
known or forecast icing
conditions,
b) The airplane is operated in day
VMC and
c) AFM limitations for the
automatic slat extension system
inoperative are complied with.
None required.
Verify operation of remaining
system by monitoring current
on amp gauge while selecting
pitot-static heat system off,
then on.
An inoperative placard will
be placed adjacent to HEAT
PROBES switch and will be
noted on ADLS.
3.
Windshield Heat
C
2
0
May be inoperative provided:
a) De-fog system is operative and
b) The airplane is not operated into
known or forecast icing
conditions.
None required.
None required.
An inoperative placard will
be placed adjacent to HEAT
WINDSHIELD switches and
will be noted on ADLS.
4.
Pneumatic De-icing
Boot System
C
2
0
(M) May be inoperative provided:
a) The airplane is not operated into
known or forecast icing
conditions,
b) System is secured to ensure that
boots remain deflated by suction.
With either or both engines
None required.
operating, verify that air is
exiting from the de-ice boot
ejector and the SURFACE
DEICE ALT and NORM circuit
breakers are pulled and disabled.
Place a placard in the cockpit
that states the aircraft must
not be flown into known or
forecasted icing conditions,
and that the wing de-ice
system must not be used. An
inoperative placard will be
placed adjacent DEICE
WING & TAIL switches and
will be noted on ADLS.
30-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
30.
5.
30-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
ICE AND RAIN PROTECTION
Surface De-icing
System Control
a)
Normal System
C
1
0
May be inoperative provided the alternate
system is operative.
None required.
None required.
An inoperative placard will be
placed adjacent DEICE
WING & TAIL switches and
will be noted on ADLS.
b)
Alternate System
C
1
0
May be inoperative provided the normal
system is operative.
None required.
None required.
An inoperative placard will be
placed adjacent DEICE
WING & TAIL switches and
will be noted on ADLS.
6.
Defog System
C
1
0
May be inoperative provided both
windshield heat systems are operative.
None required.
None required.
An inoperative placard will be
placed on control pedestal and
will be noted on ADLS.
7.
Engine Inlet
Anti-Icing Valve
(TAI Valve)
SPX only
C
2
0
May be inoperative in the open position
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
May be inoperative in the closed position
provided aircraft is not operated in known
or forecast conditions.
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.
30-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
31.
1.
31-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
INDICATING/RECORDING
SYSTEMS
Clocks
2. Flight Data
*** Recorder (FDR)
System
(Continued on Next Page)
C
-
0
Any in excess of those required by FAR
may be inoperative.
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative clock and will be
noted on ADLS.
C
-
1
Any in excess of those required by FAR
may be inoperative.
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.
A
-
0
May be inoperative provided:
None required.
a) Cockpit Voice Recorder (CVR)
operates normally,
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 prior to
takeoff, or
2. The FDR repair was
attempted but was not
successful.
c) In those cases where repair is
attempted but not successful, the
aircraft 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 must be made within
three flight days.
None required.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
31-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
31.
31-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
INDICATING/RECORDING
SYSTEMS
2. Flight Data
*** Recorder (FDR)
System
(Continued)
3.
FDR Recording Parameters
required by FAR
A -
-
May be inoperative provided:
a) Cockpit Voice Recorder (CVR)
operates normally, and
b) Repairs are made within 20
calendar days.
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.
FDR Recording Parameters
not required by FAR
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 placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
Pilots must ensure that the
actual flight time is
adequately recorded after
each flight until the flight
hour recorder is repaired.
An inoperative placard will
be placed adjacent to clock
and will be noted on ADLS.
Cockpit Voice Recorder
4. Flight Hour Recorder
***
Moved to ATA Chapter 23.
C
1
0
(O)
31-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
32.
1.
32-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
LANDING GEAR
Antiskid System
C
1
0
May be inoperative provided AFM is
complied with.
32-1
None required.
None required.
An inoperative placard will
be placed adjacent to ANTI
SKID switch and will be
noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
33.
33-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
LIGHTS
1.
Cockpit / Flight Deck /
C
Flight Compartment and
Instrument Lighting System
-
-
Individual lights may be inoperative
None required.
provided remaining lights are:
a) Sufficient to clearly illuminate all
required instruments, controls
and other devices for which it is
provided,
b) 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 adjacent to
inoperative light control and
will be noted on ADLS.
2.
Cabin Interior
Illumination System
C
-
-
May be inoperative provided:
a) Cabin emergency lighting is
operative and
b) Lighting configuration at
dispatch is acceptable to the
flight crew.
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative light control and
will be noted on ADLS.
3.
Passenger Notice
System (Fasten Seat Belts,
No Smoking)
C
1
0
(O) May be inoperative provided
appropriate verbal briefings are given to
passengers.
None required.
Pilots must provide
appropriate verbal briefings
to the passengers.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4.
Baggage Compartment
Light System
C
1
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.
33-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
33.
33-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
LIGHTS
5.
Anti-Collision Light
System (Top and / or
Bottom Strobes)
B
1
0
May be inoperative provided the airplane is None required.
operated day only.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – ANTICOL switch
and will be noted on ADLS.
6.
Wing Tip Strobes
C
2
0
None required.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – POSITION switch
and will be noted on ADLS.
7.
Taxi Light System
C
1
0
None required.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – TAXI switch and
will be noted on ADLS.
8.
Landing Light
System
C
2
1
One may be inoperative for night
operations provided taxi lights operate
normally.
None required.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – LANDING switch
and will be noted on ADLS.
2
0
May be inoperative for day operations.
None required.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – LANDING switch
and will be noted on ADLS.
C
2
0
May be inoperative provided a portable
lamp / light of adequate capacity for wing
and / or control surface inspection is
available for night operations in icing
conditions.
None required.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – WING switch and
will be noted on ADLS.
C
1
0
May be inoperative provided the airplane is None required.
operated day only.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – POSITION switch
and will be noted on ADLS.
C
9.
Wing Inspection Lights
10. Position Lights
System
33-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
33.
33-3
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
LIGHTS
11. Emergency Exit
Lighting System
C
1
0
May be inoperative for all cargo operations
only.
None required.
None required.
An inoperative placard will
be adjacent to EMERGENCY
LTS switch and will be noted
on ADLS.
12. Floor Proximity
*** Emergency Escape
Path Marking System
Lights
C
-
-
Individual lights may be inoperative
None required.
provided it is verified that the FAA
approved minimum acceptable lighting
levels specified in one of the following
documents are complied with:
a) FAA Engineering approval letter.
b) FAA approved report of the Type
Design holder.
c) Limitations and Conditions
section of the applicable
Supplemental Type Certificate
(STC) or
d) An FAA approved report
incorporated in the master
drawing list for the applicable
STC.
None required.
An inoperative placard will
be adjacent to EMERGENCY
LTS switch and will be noted
on ADLS.
None required.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – LANDING switch
and will be noted on ADLS.
None required.
None required.
An inoperative placard will
be adjacent to EXTERIOR
LIGHTS – TAIL OFF WING
switch and will be noted on
ADLS.
13. Strobes
Moved to No. 6.
14. Pulselite Landing
*** Light System
D
-
0
15. Logo Lights
***
D
-
0
May be inoperative provided both Landing
Lights operate normally.
33-3
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
NAVIGATION
1.
Mach / Airspeed
Indicator
34-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
Mach Indicator
C
2
0
May be inoperative provided:
a) The airplane is not operated
above FL 250,
b) Overspeed warning is operative
and
c) AFM limitations are observed.
None required.
None required.
An inoperative placard will
be adjacent to Mach indicator
and will be noted on ADLS.
2.
Mach / Airspeed
Overspeed Warning
System
C
1
0
May be inoperative provided:
a) Both mach meters are operative,
and
b) The following airspeed
limitations are observed and
placarded in plain view of each
pilot station;
1) Vmo – 350 KIAS below FL
250.
2) Mmo -.81 MACH FL 250
and above.
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. Placard will include
airspeed limitations as noted
in Remarks.
3.
RAT / CABIN / FUEL
TEMP Indicator
C
1
0
May be inoperative provided SAT and TAS None required.
information is available.
None required.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
RAT Mode
34-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
4.
34-2
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
Turn and Bank Indicator
a)
Slip Indicator
b)
Turn Indicator
DELETED REVISION 2
B
2
1
One may be inoperative.
An inoperative placard will
be placed adjacent to
inoperative Slip Indicator and
will be noted on ADLS.
DELETED REVISION 2.
5.
Vertical Navigation
System
C
1
0
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative Vertical
Navigation Indicator and will
be noted on ADLS.
6.
Flight Director
System
C
2
0
May be inoperative provided landing
weather minimums do not require its use.
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.
Distance Measuring
Equipment (DME)
D
-
-
Any in excess of those required by FAR
may be inoperative.
None required.
None required.
An inoperative placard will
be placed adjacent to EHSI
and will be noted on ADLS.
8.
Marker Beacon
Receiver
C
1
0
May be inoperative provided approach
procedures do not require its use.
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.
Weather Radar
C
1
-
As required by FAR.
None required.
None required.
An inoperative placard will
be placed adjacent to MFD
and will be noted on ADLS.
34-2
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-3
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
10. Automatic Direction
Finding (ADF) System
C
-
-
11. Radio Magnetic Indicator
(RMI)
C
-
12. AOA Indicator
C
None required.
None required.
An inoperative placard will
be placed adjacent to ADF
control unit and will be noted
on ADLS.
0
None required.
None required.
An inoperative placard will
be placed adjacent to RMI
and will be noted on ADLS.
1
0
None required.
None required.
An inoperative placard will
be placed adjacent to AOA
indicator and will be noted on
ADLS
13. Navigation Equipment
C
(VOR / ILS, Loran, RNAV,
Omega / VLF, INS, GPS,
Doppler, FMS)
-
-
Any in excess of those required by FAR
may be inoperative.
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. Radio Altimeter
1
0
May be inoperative provided en route or
approach procedures do not require its use.
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
Any in excess of those required by FAR
may be inoperative.
NOTE: Inoperative Radio Altimeter may
affect the Ground Proximity Warning
System (GPWS) and Traffic Collision and
Avoidance System (TCAS).
34-3
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-4
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
15. Multi-Function
Display (MFD)
Symbol Generator
a)
1125
C
1
0
b)
1125 SPX
C
2
1
B
-
D
-
16. ATC Transponders
and Automatic Altitude
Reporting Systems
None required.
None required.
An inoperative placard will
be placed adjacent to MFD
and will be noted on ADLS.
One may be inoperative provided both
Primary Flight Displays (PFD) are
operative.
None required.
None required.
An inoperative placard will
be placed adjacent to MFD
and will be noted on ADLS.
0
May be inoperative provided:
a) En route operations do not
require its use, and
b) Prior to 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 in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
1
Any in excess of those required by FAR
may be inoperative.
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.
34-4
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-5
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
17. Altitude Alerting
System
A
-
0
(O) May be inoperative provided:
a) Autopilot with altitude hold is
operative,
b) En route operations including
RVSM, RNP-5 and RNP-10
operations do not require its use.
c) Repairs are made within three
flight days.
None required.
Flight crew will comply with
proviso in Remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
May be inoperative provided it is not
required by FAR.
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.
18. Remote Tuning Unit
(RTU)
C
2
1
One may be inoperative provided at least
one FMS is operative.
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative RTU and will be
noted on ADLS.
19. Airborne Flight
*** Information System
C
1
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.
20. Maintenance Diagnostic
*** System
C
1
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.
34-5
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-6
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
21. Ground Proximity
*** Warning System (GPWS)
1)
Modes 1-4
A
-
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used and
b) Repairs are made within two
flight days.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(O) May be inoperative provided:
a) It is not required by FAR, and
b) Alternate procedures are
established and used.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
A
-
0
(O) May be inoperative provided:
a) Alternate procedures are
established used and
b) Repairs are made within two
flight days.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C
-
0
(O) May be inoperative provided:
a) It is not required by FAR, and,
b) Alternate procedures are
established and used.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(Continued on Next Page)
34-6
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-7
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
21. Ground Proximity
*** Warning System (GPWS)
(Continued)
2)
3)
***4)
Test Mode
Glideslope Deviation
(Mode 5)
Advisory Callouts
A
1
0
May be inoperative provided:
a) The GPWS is considered
inoperative and
b) Repairs are made within two
flight days.
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
1
0
May be inoperative provided:
a) It is not required by FAR, and,
b) GPWS is considered inoperative.
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
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
May be inoperative provided it is not
required by FAR.
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
-
0
(O) May be inoperative provided alternate
procedures are established and used.
None required.
Pilots must use alternate
procedures for advisory
callouts
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
34-7
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-8
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
21. Ground Proximity
*** Warning System
(Continued)
5)
***6)
Windshear Mode
C
-
0
TAWS
C
-
0
C
2
1
C
2
1
22. Air Data
Computers (ADC)
(O) May be inoperative provided:
a) Alternate procedures are
established and used and
b) Takeoffs and landings are not
conducted in known or forecast
windshear conditions.
None required.
Pilots must use alternative
procedures for windshear
mode advisories.
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.
(O) Except where en route operations,
including RVSM, RNP-5 and RNP-10
operations, require its use, one may be
inoperative provided flight instruments on
right side are pneumatic.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
(O) One may be inoperative except where
en route operations, including RVSM,
RNP-5 and RNP-10 operations, require its
use, provided all air data instrumentation
functions normally.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
34-8
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-9
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
23. Non-Stabilized
Magnetic Compass
B
1
0
May be inoperative provided any
combination of three gyro or INS (IRU)
stabilized compass systems are operative.
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative compass and will
be noted on ADLS.
B
1
0
May be inoperative provided:
None required.
a) Any combination of two
stabilized gyro or INS stabilized
compass systems are operative,
and
b) Aircraft is operated with dual
independent navigation capability
and under positive radar control
by ATC on the en route portion
of the flight.
None required.
An inoperative placard will
be placed adjacent to
inoperative compass and will
be noted on ADLS.
B
1
0
May be inoperative for flights that are
None required.
entirely within areas of magnetic
unreliability provided at least two stabilized
directional gyro systems are installed,
operative and used in conjunction with
approved free gyro navigation techniques.
None required.
An inoperative placard will
be placed adjacent to
inoperative compass and will
be noted on ADLS.
34-9
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
NAVIGATION
24.
Traffic Collision
Avoidance System I
(TCAS I)
34-10
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
B
-
0
(M) (O) May be inoperative provided:
a) System is deactivated and
secured and
b) En route or approach procedures
do not require its use.
Pull and tag the TCAS circuit
breaker.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed 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) It is not required by FAR,
b) System is deactivated and
secured and
c) En route or approach procedures
do not require its use.
Pull and tag the TCAS circuit
breaker.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
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.
Pull and tag the TCAS circuit
breaker.
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
-
0
(M) (O) May be inoperative provided:
Pull and tag the TCAS circuit
a) Not required by FAR,
breaker.
b) System is deactivated and
secured, and
c) Enroute or Approach procedures
do not require its use.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***1) Combined Traffic
C
Alert (TA) and Resolution
Advisory (RA) Dual
Display Systems
-
0
(O) One may be inoperative on the nonflying pilot 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 the flying pilot
side.
Pilots must ensure that the
TA and RA elements, as well
as audio functions, are
operative on the flying pilot
side.
Place a placard in the cockpit
on the non-flying pilot side
stating that TCAS II TA and
RA functions are inoperative,
and that TA and RA
functions on the flying pilot
side must be used and will be
noted on ADLS.
25.
Traffic Collision and
Avoidance System II
(TCAS II)
(Continued on Next Page)
34-10
None required.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
SYSTEM &
SEQUENCE
NUMBERS
34.
NAVIGATION
25.
Traffic Collision and
Avoidance System II
(TCAS II)
(Continued)
2) Resolution Advisory
(RA) System(s)
3) Traffic Display
System(s)
PAGE NUMBER:
34-11
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
5.
3.
NUMBER REQ’D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
C
2
1
(O) One may be inoperative on the nonflying pilot side.
None required.
Flight crew will comply with
proviso in remarks column.
Place a placard in the cockpit
on the non-flying pilot side
stating that the TCAS II RA
display is inoperative and will
be noted on ADLS.
C
-
0
(O) May be inoperative provided:
a) All Traffic Alert (TA) display
elements 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.
Pilots must select TA mode
only and ensure all TA
display elements and audio
functions are operative.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
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.
Pilots must ensure that the
RA visual and audio
functions are operative.
Place a placard in the cockpit
stating that the TCAS II TA
function is inoperative and
will be noted on ADLS.
34-11
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
NAVIGATION
26.
***
Moving Map Display
5.
3.
27.
***
Windshear Detection
and Guidance Systems
NUMBER REQ'D FOR DISPATCH
4.
D
-
34-12
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
PAGE NUMBER:
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
-
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.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
DELETED REVISION 3
(Now items 30 and 31)
28. Flight Management
*** System (FMS)
Navigation Databases
C
-
-
(O) May be out of currency provided:
a) Current aeronautical charts are
used to verify navigation fixes
prior to dispatch,
b) Procedures are established and
used to verify status suitability of
navigation facilities used to
define route of flight and
c) Approach navigation radios are
manually tuned and identified.
34-12
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
34-13
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NAVIGATION
29. Navigation Management
*** System
Navigation Databases
C
-
-
D
-
-
Windshear Warning and
C
and Flight Guidance System
-
0
C
-
0
30. Stormscope
(O) May be out of currency provided:
a) Current aeronautical charts are
used to verify navigation fixes
prior to 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.
Flight crew will comply with
proviso in remarks column.
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.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
***
31.
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Windshear detection and
avoidance system operates
normally.
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Takeoffs and landings are not
conducted in known or forecast
windshear conditions.
34-13
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
NAVIGATION
32.
Windshear Detection and
Avoidance System
33.
Automatic Dependent
Surveillance – Broadcast
(ADS – B) System
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
5.
3.
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
6.
7.
OPERATIONAL
PROCEDURES
Link and Display
Processor Unit (LDPU)
C
-
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Windshear warning and
guidance system operates
normally.
C
-
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Takeoffs and landings are not
conducted in known or forecast
windshear conditions.
D
-
0
May be inoperative provided it is not
required by FAR.
D
-
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
None required.
Flight crew will comply with
proviso in remarks column.
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.
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.
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: Cockpit Display Traffic
Information (CDTI) display of data from
other aircraft systems may be used.
2)
Cockpit Display and
Traffic Information
(CDTI)
(Continued on Next Page)
D
-
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
NOTE: If ADS – B is installed in lieu of or
as a replacement for FAR-required
equipment, the repair category in the
operator’s MEL will be the same as that of
the FAR-required equipment.
1)
34-14
NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
PAGE NUMBER:
0
NOTE: ADS – B data transmissions may
continue.
34-14
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
34.
NAVIGATION
33.
Automatic Dependent
Surveillance – Broadcast
(ADS – B) System
(Continued)
5.
3.
NUMBER REQ'D FOR DISPATCH
4.
3)
CDTI Control Panel
D
-
0
4)
Data Link
Transmitter(s)
D
-
0
5)
Data Link Receiver(s)
D
-
0
-
0
34. Standby Attitude Indicator
C
34-15
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
PAGE NUMBER:
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
May be inoperative provided:
a) Flight ID can be set and
b) Screen display is acceptable to
the flight crew.
May be inoperative provided:
a) Operations are conducted in Day
VMC only, and
b) Operations are not conducted
into known or forecast VFR-onTop conditions.
34-15
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.
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.
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.
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 G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
35.
35-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
OXYGEN
1.
Oxygen System and
Supply (Passenger)
C
-
-
As required by FAR.
None required.
None required.
An inoperative placard will
be placed on the passenger
oxygen panel and will be
noted on ADLS.
2.
Oxygen Blow Out
Disc
C
1
0
(O) May be missing provided adequate
oxygen is available for number of people
on board including crew.
None required.
Ensure that the oxygen shutoff valve is open and the
pressure gage on the
passenger oxygen panel
indicates adequate oxygen is
available for the number of
people on board the aircraft,
including the crew.
A placard will be placed on
the passenger oxygen panel
stating that oxygen levels
must be verified prior to each
flight and will be noted on
ADLS.
D
-
-
Any in excess of those required by FAR
may be inoperative.
None required.
None required.
An inoperative placard will
be placed on the equipment
and will be noted on ADLS.
3. Protective Breathing
*** Equipment
35-1
PAGE NUMBER:
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
SYSTEM &
SEQUENCE
NUMBERS
49.
49-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
5.
3.
NUMBER REQ'D FOR DISPATCH
4. MMEL REMARKS OR
EXCEPTIONS
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
AIRBORNE AUXILIARY
POWER
1. Auxiliary Power
*** Unit (APU)
B
1
0
May be inoperative provided APU is
secured and other procedures do not
require its use.
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)
Speed System
C
1
0
May be inoperative provided the APU 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.
2)
Temperature System
C
1
0
May be inoperative provided the APU 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.
3)
Fire Protection
System
C
1
0
May be inoperative provided the APU 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.
B
1
0
(O) May be inoperative provided:
a) Both engine-driven generators
are operative and
b) Other procedures do not require
its use.
None required.
Ensure that APU generator
switch is OFF and remains
OFF for the entire flight.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2. APU Generator
***
49-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
52.
1.
52-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
DOORS
Door Warning Light
System
C
1
0
May be inoperative provided a
crewmember verifies by visual inspection
before each departure that the door(s) is
closed and locked.
52-1
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 G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
SYSTEM &
SEQUENCE
NUMBERS
77.
PAGE NUMBER:
77-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
5.
3.
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
ENGINE INDICATING
1.
N1 Indicator
Digital Display
C
2
0
May be inoperative provided associated
analog display is operative.
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative display and will
be noted on ADLS.
2.
N2 Indicator
Digital Display
C
2
0
May be inoperative provided associated
analog display is operative.
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative display and will
be noted on ADLS.
3.
ITT Indicator
Digital Display
C
2
0
May be inoperative provided associated
analog display is operative.
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative display and will
be noted on ADLS.
4.
Automatic Power
Reserve (APR)
(SPX only)
C
1
0
(O) May be inoperative provided AFM is
complied with.
None required.
Flight crew will comply with
proviso in remarks column.
An inoperative placard will
be placed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
5.
Engine Synchronizer
(ENG SYNC)
C
1
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.
A
2
1
None required.
None required.
An inoperative placard will
be placed adjacent to
inoperative display and will
be noted on ADLS.
6. Liquid Crystal
*** Displays
One may be inoperative provided:
a) Reversionary mode is operative
and
b) Repairs are made within one
flight day.
77-1
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
78.
1.
78-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
5.
3.
SEQUENCE
NUMBERS
PAGE NUMBER:
NUMBER REQ'D FOR DISPATCH
4.
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES
MMEL REMARKS OR
EXCEPTIONS
ENGINE EXHAUST
Thrust Reversing
System
C
2
0
(M) May be inoperative provided
inoperative thrust reverser system(s) is
secured in the forward thrust position.
78-1
Thrust reverser may be secured None required.
in the forward thrust position by
pulling and disabling the
respective circuit breaker and
securing the lock mechanism in
the forward thrust position as
described in the Maintenance
Manual.
Place a placard in the cockpit
stating that the respective
thrust reverser is inoperative
and will be noted on ADLS.
GULFSTREAM AEROSPACE CORPORATION
AIRCRAFT:
GULFSTREAM AEROSPACE MODEL G100
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL
1.
2.
79.
1.
5.
3.
NUMBER REQ'D FOR DISPATCH
4.
MMEL REMARKS OR
EXCEPTIONS
ENGINE OIL
Low Oil Pressure
Warning Light
79-1
MMEL REV. NO.: 5a
MOP REV. NO.: 5a
MMEL DATE: 11/30/2009
MOP DATE: 11/30/2009
6.
7.
NUMBER INSTALLED
SYSTEM &
SEQUENCE
NUMBERS
PAGE NUMBER:
DELETED REVISION 2.
79-1
MAINTENANCE
PROCEDURES
OPERATIONAL
PROCEDURES
PLACARDING
PROCEDURES