Airbus-AC A319 May2014

@AIRBUS A319/A319NEO AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus. © AIRBUS S.A.S. 2005. All rights reserved. AIRBUS S.A.S. Customer Services Technical Data Support and Services 31707 Blagnac Cedex FRANCE Issue: Jul 01/95 Rev: May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING HIGHLIGHTS Revision No. 12 - May 01/14 LOCATIONS CHAPTER 1 Section 1-1 Subject 1-1-0 CHG CODE R R R Purpose R Section 1-2 Subject 1-2-0 N N Glossary N CHAPTER 2 Section 2-1 Subject 02-01-00 R R D Subject 2-1-1 R General Aircraft Characteristics Data Section 2-2 Subject 2-2-0 R DESCRIPTIONS OF CHANGE PART EFFECTIVITY ADDED/REVISED/DELETED DESCRIPTION TITLE UPDATED PART EFFECTIVITY ADDED/REVISED/DELETED R R General Aircraft Dimensions R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE General Aircraft Dimensions Wing Tip Fence R FIGURE General Aircraft Dimensions N REVISED ILLUSTRATIONS TO SHOW THE DIMENSIONS ON WING AND HTP. ILLUSTRATION REVISED ADDED ILLUSTRATIONS TO SHOW GENERAL AIRCRAFT DIMENSIONS FOR NEO VERSION. ILLUSTRATION ADDED Section 2-3 Subject 2-3-0 Ground Clearances R R R PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED HIGHLIGHTS Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Ground Clearances CHG CODE R DESCRIPTIONS OF CHANGE DELETED THE GROUND CLEARANCE DIMENSIONS OF MRW (64T) IN THE TABLE. IMPROVED LAYOUT. ILLUSTRATION REVISED DELETED THE GROUND CLEARANCE DIMENSIONS OF MRW (64T) IN THE TABLE. IMPROVED LAYOUT. ILLUSTRATION REVISED ADDED ILLUSTRATION OF GROUND CLEARANCES FOR NEO VERSION. ILLUSTRATION ADDED DELETED THE GROUND CLEARANCE DIMENSIONS FOR THE MTOW OF 64T AND 70T. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Ground Clearances - Ground Clearances with Sharklets R FIGURE Ground Clearances N FIGURE Ground Clearances - Flaps and Flap Track Fairings When Flaps Fully Extended R FIGURE Ground Clearances - Flap Track Fairings Up R DELETED THE GROUND CLEARANCE DIMENSIONS FOR THE MTOW OF 64T AND 70T. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Ground Clearances - Aileron Down R DELETED THE GROUND CLEARANCE DIMENSIONS FOR THE MTOW OF 64T AND 70T. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Ground Clearances - Aileron Up and Spoilers 1 to 5 Extended R DELETED THE GROUND CLEARANCE DIMENSIONS FOR THE MTOW OF 64T AND 70T. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED HIGHLIGHTS Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Ground Clearances - Slats Extended CHG CODE R Section 2-4 Subject 02-04-00 R D Subject 2-4-1 R DESCRIPTIONS OF CHANGE DELETED THE GROUND CLEARANCE DIMENSIONS FOR THE MTOW OF 64T AND 70T. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Interior Arrangements - Plan View R DESCRIPTION TITLE UPDATED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Interior Arrangements - Plan View - Typical Configuration - SingleClass, High Density R ADDED ”INTERIOR ARRANGEMENTS PLAN VIEW” TO THE TITLE. ILLUSTRATION REVISED FIGURE Interior Arrangements - Plan View - Typical Configuration - Two-Class R ADDED ”INTERIOR ARRANGEMENTS PLAN VIEW” TO THE TITLE. ILLUSTRATION REVISED Section 2-5 Subject 2-5-0 R R Interior Arrangements - Cross Section R DESCRIPTION TITLE UPDATED FIGURE Interior Arrangements - Cross Section - Typical Configuration R FIGURE Interior Arrangements - Cross Section - Economy Class, 6 Abreast Wider Aisle FIGURE Interior Arrangements - Cross Section - First-Class R REVISED TITLE TO ”INTERIOR ARRANGEMENTS - CROSS SECTION”. ILLUSTRATION REVISED REVISED TITLE TO ”INTERIOR ARRANGEMENTS - CROSS SECTION”. ILLUSTRATION REVISED REVISED TITLE TO ”INTERIOR ARRANGEMENTS - CROSS SECTION”. ILLUSTRATION REVISED Section 2-6 Subject 2-6-0 Cargo Compartments R R R R PART EFFECTIVITY ADDED/REVISED/DELETED HIGHLIGHTS Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Cargo Compartments Locations, Dimensions and Loading Combinations Section 2-7 Subject 2-7-0 CHG CODE R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED R R Door Clearances R FIGURE Door Identification and Location - Door Identification N Subject 2-7-1 DESCRIPTIONS OF CHANGE DESCRIPTION TITLE UPDATED NOTE AMENDED ADDED ILLUSTRATIONS FOR DOOR IDENTIFICATION AND LOCATION. ILLUSTRATION ADDED R Forward Passenger / Crew Doors R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Doors Clearances - Forward Passenger / Crew Doors R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 2-7-2 R Emergency Exits R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Doors Clearances - Emergency Exits R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 2-7-3 R Aft Passenger / Crew Doors R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Doors Clearances - Aft Passenger / Crew Doors R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 2-7-4 R Forward Cargo Compartment Door R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Door Clearances - Forward Cargo Compartment Door R IMPROVED LAYOUT. ILLUSTRATION REVISED HIGHLIGHTS Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Door Clearances - Forward Cargo Compartment Door Subject 2-7-5 CHG CODE N DESCRIPTIONS OF CHANGE ADDED ILLUSTRATION OF FORWARD CARGO COMPARTMENT DOOR CLEARANCES FOR NEO VERSION. ILLUSTRATION ADDED R Aft Cargo Compartment Door R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Doors Clearances - Aft Cargo Compartment Door R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 2-7-7 R Main Landing Gear Doors R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Doors Clearances - Main Landing Gear Doors R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 2-7-8 R Radome R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Doors Clearances - Radome R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 2-7-9 R APU and Nose Landing Gear Doors R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Doors Clearances - APU and Nose Landing Gear Doors R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 2-8 Subject 2-8-0 Escape Slides R R R PART EFFECTIVITY ADDED/REVISED/DELETED HIGHLIGHTS Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Escape Slides - Location FIGURE Escape Slides - Dimensions Section 2-9 Subject 2-9-0 CHG CODE R R DESCRIPTIONS OF CHANGE ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED R R Landing Gear R PART EFFECTIVITY ADDED/REVISED/DELETED CROSS REFERENCED DOCUMENTARY UNIT ADDED/REVISED/DELETED FIGURE Landing Gear - Main Landing Gear - Twin-Wheel R DELETED TECHNICAL SPECIFICATION STANDARD ”MS28889” IN SHEET 2. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Landing Gear - Main Landing Gear Dimensions - Twin-Wheel R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Landing Gear - Nose Landing Gear R DELETED TECHNICAL SPECIFICATION STANDARD ”MS28889” IN SHEET 2. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Landing Gear - Nose Landing Gear Dimensions R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Landing Gear Maintenance Pits R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Landing Gear Maintenance Pits Maintenance Pit Envelopes R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Landing Gear Maintenance Pits Maintenance Pit Envelopes R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED HIGHLIGHTS Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS Section 2-10 Subject 2-10-0 CHG CODE R R DESCRIPTIONS OF CHANGE Exterior Lighting R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Exterior Lighting R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Exterior Lighting R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Exterior Lighting R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Exterior Lighting R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 2-11 Subject 2-11-0 R R Antennas and Probes Location R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Antennas and Probes - Location R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 2-12 Subject 2-12-0 R R Auxiliary Power Unit R FIGURE Auxiliary Power Unit - Access Doors FIGURE Auxiliary Power Unit - General Layout R ILLUSTRATION REVISED R ILLUSTRATION REVISED Engine and Nacelle R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Power Plant Handling - Major Dimensions - CFM56 Series Engine R ILLUSTRATION REVISED HIGHLIGHTS Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS CHG CODE R ILLUSTRATION REVISED FIGURE Power Plant Handling - Fan Cowls - CFM56 Series Engine R ILLUSTRATION REVISED FIGURE Power Plant Handling - Thrust Reverser Cowls - CFM56 Series Engine R ILLUSTRATION REVISED FIGURE Power Plant Handling - Major Dimensions - IAE V2500 Series Engine R ILLUSTRATION REVISED FIGURE Power Plant Handling - Major Dimensions - IAE V2500 Series Engine R ILLUSTRATION REVISED FIGURE Power Plant Handling - Fan Cowls - IAE V2500 Series Engine R ILLUSTRATION REVISED FIGURE Power Plant Handling - Thrust Reverser Halves - IAE V2500 Series Engine R ILLUSTRATION REVISED FIGURE Power Plant Handling - Major Dimensions - PW 1100G Engine N FIGURE Power Plant Handling - Fan Cowls - PW 1100G Engine N FIGURE Power Plant Handling - Thrust Reverser Halves - PW 1100G Engine N ADDED ILLUSTRATION TO SHOW THE MAJOR DIMENSIONS OF PW 1100G ENGINE. ILLUSTRATION ADDED ADDED ILLUSTRATION TO SHOW THE DIMENSIONS WHEN ENGINE FAN COWLS ARE IN OPEN POSITION. ILLUSTRATION ADDED ADDED ILLUSTRATION TO SHOW THE DIMENSIONS WHEN THRUST REVERSERS ARE IN OPEN POSITION. ILLUSTRATION ADDED FIGURE Power Plant Handling - Major Dimensions - CFM56 Series Engine Section 2-13 Subject 2-13-0 DESCRIPTIONS OF CHANGE R R Leveling, Symmetry and Alignment R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Location of the Leveling Points R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 2-14 R HIGHLIGHTS Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS Subject 2-14-0 CHG CODE R DESCRIPTIONS OF CHANGE Jacking for Maintenance R PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED ADDED TABLE FOR THE LOCATION OF JACKING POINTS AND THE MAXIMUM ELIGIBLE LOAD ON EACH JACKING POINT. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Jacking for Maintenance Jacking Point Locations R FIGURE Jacking for Maintenance Forward Jacking Point R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Jacking for Maintenance - Wing Jacking Points R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Jacking for Maintenance - Safety Stay R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Jacking for Maintenance Jacking Design R UPDATED JACKING CONFIGURATION AND CORRECTED THE POSITION OF JACKS. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Loads at the Aircraft Jacking Points - Wing Jacking Point and Forward Fuselage Jacking Point R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Jacking for Maintenance Location of Shoring Cradles R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Jacking of the Landing Gear R DESCRIPTION TITLE UPDATED PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED HIGHLIGHTS Page 9 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Jacking of the Landing Gear MLG Jacking Point Location - Twin Wheels FIGURE Jacking of the Landing Gear MLG Jacking with Cantilever Jack - Twin Wheels FIGURE Jacking of the Landing Gear Loads at MLG Jacking Points - Twin Wheels FIGURE Jacking of the Landing Gear Loads at MLG Jacking Points - 75 500 kg CHG CODE R R R R FIGURE Jacking of the Landing Gear NLG Jacking - Point Location R FIGURE Jacking of the Landing Gear Loads at NLG Jacking Points R FIGURE Jacking of the Landing Gear Loads at NLG Jacking Points - 75 500 kg R CHAPTER 3 Section 3-1 Subject 3-1-0 R R R General Information Section 3-2 Subject 03-02-00 N R D Subject 3-2-1 R DESCRIPTIONS OF CHANGE REVISED TITLE TO ”JACKING LANDING GEAR”. ILLUSTRATION REVISED REVISED TITLE TO ”JACKING LANDING GEAR”. ILLUSTRATION REVISED REVISED TITLE TO ”JACKING LANDING GEAR”. ILLUSTRATION REVISED REVISED TITLE TO ”JACKING LANDING GEAR”. ILLUSTRATION REVISED REVISED TITLE TO ”JACKING LANDING GEAR”. ILLUSTRATION REVISED REVISED TITLE TO ”JACKING LANDING GEAR”. ILLUSTRATION REVISED REVISED TITLE TO ”JACKING LANDING GEAR”. ILLUSTRATION REVISED OF THE OF THE OF THE OF THE OF THE OF THE OF THE ISA Conditions R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Payload/Range N FIGURE Payload/Range - Sharklet N ADDED ILLUSTRATION TO SHOW PAYLOAD/RANGE AT ISA CONDITIONS. ILLUSTRATION ADDED ADDED ILLUSTRATION TO SHOW PAYLOAD/RANGE AT ISA CONDITIONS. ILLUSTRATION ADDED HIGHLIGHTS Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Payload/Range CHG CODE N Section 3-3 Subject 03-03-00 R D Subject 3-3-1 R DESCRIPTIONS OF CHANGE ADDED ILLUSTRATION TO SHOW PAYLOAD/RANGE AT ISA CONDITIONS. ILLUSTRATION ADDED Take-Off Weight Limitation - ISA Conditions FIGURE Take-Off Weight Limitation ISA Conditions - CFM56 Series Engine R DESCRIPTION TITLE UPDATED R DELETED ”FAR/JAR” FROM THE TITLE. ILLUSTRATION REVISED FIGURE Take-Off Weight Limitation ISA Conditions - IAE V2500 Series Engine R DELETED ”FAR/JAR” FROM THE TITLE. ILLUSTRATION REVISED Subject 3-3-2 R Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions R DESCRIPTION TITLE UPDATED FIGURE Take-Off Weight Limitation ISA +15˚C (+59˚F) Conditions - CFM56 Series Engine R DELETED ”FAR/JAR” FROM THE TITLE. ILLUSTRATION REVISED FIGURE Take-Off Weight Limitation ISA +15˚C (+59˚F) Conditions - IAE V2500 Series Engine R DELETED ”FAR/JAR” FROM THE TITLE. ILLUSTRATION REVISED Section 3-4 Subject 03-04-00 R D Subject 3-4-1 R Landing Field Length - ISA Conditions R DESCRIPTION TITLE UPDATED FIGURE Landing Field Length - ISA Conditions - CFM56-5A Series Engine R FIGURE Landing Field Length - ISA Conditions - IAE V2500 Series Engine R REVISED TITLE TO ”LANDING FIELD LENGTH - ISA CONDITIONS”. REVISED ILLUSTRATION TO DELETE ”FAR” AND IMPROVED LAYOUT. ILLUSTRATION REVISED REVISED TITLE TO ”LANDING FIELD LENGTH - ISA CONDITIONS”. REVISED ILLUSTRATION TO DELETE ”FAR” AND IMPROVED LAYOUT. ILLUSTRATION REVISED HIGHLIGHTS Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS Section 3-5 Subject 3-5-0 Final Approach Speed CHG CODE R R DESCRIPTIONS OF CHANGE R CHAPTER 4 Section 4-1 Subject 4-1-0 R R R General Information Section 4-2 Subject 4-2-0 N R R Turning Radii R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 4-3 Subject 4-3-0 R R Minimum Turning Radii R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Minimum Turning Radii R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 4-4 Subject 4-4-0 R R Visibility from Cockpit in Static Position R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Visibility from Cockpit in Static Position R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED HIGHLIGHTS Page 12 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Binocular Visibility Through Windows from Captain Eye Position Section 4-5 Subject 4-5-0 Runway and Taxiway Turn Paths Subject 4-5-1 CHG CODE R DESCRIPTIONS OF CHANGE ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED R R R PART EFFECTIVITY ADDED/REVISED/DELETED R 135˚ Turn - Runway to Taxiway R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over Centerline Method R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE 135˚ Turn - Runway to Taxiway - Judgemental Oversteering Method R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 4-5-2 R 90˚ Turn - Runway to Taxiway R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE 90˚ Turn - Runway to Taxiway Cockpit Over Centerline Method R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE 90˚ Turn - Runway to Taxiway Judgemental Oversteering Method R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 4-5-3 R 180˚ Turn on a Runway R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE 180˚ Turn on a Runway - Edge of Runway Method R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 4-5-4 135˚ Turn - Taxiway to Taxiway R R PART EFFECTIVITY ADDED/REVISED/DELETED HIGHLIGHTS Page 13 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline Method Subject 4-5-5 CHG CODE R DESCRIPTIONS OF CHANGE ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED R 90˚ Turn - Taxiway to Taxiway R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline Method R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 4-6 Subject 4-6-0 R R Runway Holding Bay (Apron) R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Runway Holding Bay (Apron) R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 4-7 Subject 4-7-0 R R Minimum Line-Up Distance Corrections R DESCRIPTION TITLE UPDATED FIGURE Minimum Line-Up Distance Corrections - 90˚ Turn on Runway Entry N FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn on Runway Turn Pad FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn on Runway Width Section 4-8 Subject 4-8-0 N ADDED ILLUSTRATION FOR 90˚ TURN ON RUNWAY ENTRY. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR 180˚ TURN ON RUNWAY TURN PAD. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR 180˚ TURN ON RUNWAY WIDTH. ILLUSTRATION ADDED N N N Aircraft Mooring N FIGURE Aircraft Mooring N CHAPTER 5 Section 05-00 ILLUSTRATION ADDED R D HIGHLIGHTS Page 14 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS Section 5-1 Subject 05-01-00 Subject 5-1-1 Aircraft Servicing Arrangements Subject 5-1-2 CHG CODE R D DESCRIPTIONS OF CHANGE R R DESCRIPTION TITLE UPDATED PART EFFECTIVITY ADDED/REVISED/DELETED R Typical Ramp Layout -- Open Apron R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Typical Ramp Layout - Open Apron - Bulk Loading R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Typical Ramp Layout - Open Apron - ULD Loading R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 5-1-3 R Typical Ramp Layout - Gate R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Typical Ramp Layout - Gate R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Section 5-2 Subject 5-2-0 R R Terminal Operations - Full Servicing Turn Round Time R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Full Servicing Turn Round Time Chart R REVISED TRT TO 37 MIN. UPDATED TRT CHART AND ILLUSTRATION TITLE. ILLUSTRATION REVISED Section 5-3 Subject 5-3-0 Terminal Operations - Outstation Turn Round Time FIGURE Outstation Turn Round Time Chart R R R DESCRIPTION TITLE UPDATED R REVISED ILLUSTRATION TITLE AND TRT CHART. ILLUSTRATION REVISED HIGHLIGHTS Page 15 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS Section 5-4 Subject 05-04-00 Subject 5-4-1 CHG CODE R D DESCRIPTIONS OF CHANGE R Ground Service Connections Layout R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Ground Service Connections Layout R IMPROVED LAYOUT AND ADDED THE LOCATIONS OF OXYGEN SYSTEM (2), OVERPRESSURE PROTECTORS (10) AND NACA VENT INTAKE (13). ILLUSTRATION REVISED Subject 5-4-2 R Grounding (Earthing) Points R FIGURE Ground Service Connections Grounding (Earthing) Points - Landing Gear R FIGURE Ground Service Connections Grounding (Earthing) Points - Wing (If Installed) R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Ground Service Connections Grounding (Earthing) Point - Avionics Compartment Door-Frame N FIGURE Ground Service Connections Grounding (Earthing) Point - Engine Air Intake (If Installed) N ADDED ILLUSTRATION FOR GROUNDING (EARTHING) POINT ON THE AVIONICS COMPARTMENT DOOR-FRAME. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR GROUNDING (EARTHING) POINT ON THE ENGINE AIR INTAKE. ILLUSTRATION ADDED Subject 5-4-3 Hydraulic System DESCRIPTION TITLE UPDATED PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED REVISED THE ILLUSTRATION TO ADD THE WORD ”EARTHING” TO THE TERM ”GROUNDING”. IMPROVED LAYOUT. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED R R PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED HIGHLIGHTS Page 16 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Hydraulic System - Green System Ground Service Panel CHG CODE R DESCRIPTIONS OF CHANGE REVISED ILLUSTRATION TO LOCATE ”RESERVOIR DEPRESSURIZATION CONNECTION AND SELECTOR VALVE”. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Hydraulic System - Blue System Ground Service Panel R REVISED ILLUSTRATION TO LOCATE ”RESERVOIR DEPRESSURIZATION VALVE AND DRAIN VALVE”. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Hydraulic System - Yellow System Ground Service Panel R REVISED ILLUSTRATION TO LOCATE ”RESERVOIR DEPRESSURIZATION VALVE AND HAND PUMP LEVER”. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED Subject 5-4-4 R Electrical System R FIGURE Ground Service Connections External Power Receptacles R Subject 5-4-5 R Oxygen System R FIGURE Ground Service Connections Oxygen System N Subject 5-4-6 PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED ADDED ILLUSTRATION FOR OXYGEN SYSTEM SERVICING. ILLUSTRATION ADDED R Fuel System R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Ground Service Connections Refuel/Defuel Control Panel R REVISED ILLUSTRATION TITLE TO ”REFUEL/DEFUEL CONTROL PANEL”. ILLUSTRATION REVISED HIGHLIGHTS Page 17 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Ground Service Connections Refuel/Defuel Couplings CHG CODE R FIGURE Ground Service Connections Overwing Gravity-Refuel Cap (If Installed) R FIGURE Ground Service Connections Overpressure Protectors and NACA Vent Intake R Subject 5-4-7 DESCRIPTIONS OF CHANGE ILLUSTRATION REVISED REVISED ILLUSTRATION TITLE TO ”OVERWING GRAVITY-REFUEL CAP”. ADDED ”(IF INSTALLED)” IN THE ILLUSTRATION TITLE. ILLUSTRATION REVISED REVISED ILLUSTRATION TO SHOW THE WING TANK OVERPRESSUREPROTECTOR. ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED R Pneumatic System N FIGURE Ground Service Connections - LP and HP Ground Connectors N ADDED ILLUSTRATION ABOUT GROUND SERVICE CONNECTIONS FOR PNEUMATIC SYSTEM. ILLUSTRATION ADDED Subject 5-4-8 R Oil System R DESCRIPTION TITLE UPDATED FIGURE Ground Service Connections Engine Oil Tank -- CFM56 Series Engine N FIGURE Ground Service Connections IDG Oil Tank -- CFM56 Series Engine N FIGURE Ground Service Connections Starter Oil Tank -- CFM56 Series Engine N FIGURE Ground Service Connections Engine Oil Tank -- IAE V2500 Series Engine N MIGRATED ”OIL SYSTEM” FROM SECTION ”05-04-09” TO ”05-04-08”. ILLUSTRATION ADDED MIGRATED ”OIL SYSTEM” FROM SECTION ”05-04-09” TO ”05-04-08”. ILLUSTRATION ADDED MIGRATED ”OIL SYSTEM” FROM SECTION ”05-04-09” TO ”05-04-08”. ILLUSTRATION ADDED MIGRATED ”OIL SYSTEM” FROM SECTION ”05-04-09” TO ”05-04-08”. ILLUSTRATION ADDED FIGURE Ground Service Connections IDG Oil Tank -- IAE V2500 Series Engine N MIGRATED ”OIL SYSTEM” FROM SECTION ”05-04-09” TO ”05-04-08”. ILLUSTRATION ADDED HIGHLIGHTS Page 18 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Ground Service Connections Starter Oil Tank -- IAE V2500 Series Engine FIGURE Ground Service Connections APU Oil Tank Subject 5-4-9 CHG CODE N N DESCRIPTIONS OF CHANGE MIGRATED ”OIL SYSTEM” FROM SECTION ”05-04-09” TO ”05-04-08”. ILLUSTRATION ADDED MIGRATED ”OIL SYSTEM” FROM SECTION ”05-04-09” TO ”05-04-08”. ILLUSTRATION ADDED R Potable Water System R DESCRIPTION TITLE UPDATED FIGURE Ground Service Connections Potable Water Ground Service Panels N FIGURE Ground Service Connections Potable Water Tank Location N MIGRATED ”POTABLE WATER SYSTEM” FROM SECTION ”05-04-08” TO ”05-04-09”. ILLUSTRATION ADDED ADDED ILLUSTRATION OF THE POTABLE WATER TANK LOCATION. ILLUSTRATION ADDED Subject 5-4-10 R Vacuum Toilet System R FIGURE Ground Service Connections Waste Water Ground Service Panel R FIGURE Ground Service Connections Waste Tank Location Section 5-5 Subject 5-5-0 N PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED ILLUSTRATION ADDED R R Engine Starting Pneumatic Requirements R PART EFFECTIVITY ADDED/REVISED/DELETED CROSS REFERENCED DOCUMENTARY UNIT ADDED/REVISED/DELETED FIGURE Example for Use of the Charts N FIGURE Engine Starting Pneumatic Requirements - IAE V2500 Series Engine N ADDED ILLUSTRATION TO SHOW HOW TO USE THE CHARTS. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR THE IAE V2500 SERIES ENGINE. ILLUSTRATION ADDED HIGHLIGHTS Page 19 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Engine Starting Pneumatic Requirements - CFM56 Series and CFM LEAP-1A NEO Engine FIGURE Engine Starting Pneumatic Requirements - PW 1100G NEO Engine CHG CODE N N Subject 05-05-01 D Subject 05-05-02 D Subject 05-05-03 D Section 5-6 Subject 5-6-0 R R Ground Pneumatic Power Requirements N FIGURE Ground Pneumatic Power Requirements - Heating N FIGURE Ground Pneumatic Power Requirements - Cooling N Subject 05-06-01 D Subject 05-06-02 D Section 5-7 Subject 5-7-0 R R DESCRIPTIONS OF CHANGE ADDED ILLUSTRATION FOR THE CFM56 SERIES AND CFM LEAP-1A NEO ENGINE. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR THE PW 1100G NEO ENGINE. ILLUSTRATION ADDED ADDED ILLUSTRATION OF PULL UP PERFORMANCE FOR HEATING THE CABIN. ILLUSTRATION ADDED ADDED ILLUSTRATION OF PULL DOWN PERFORMANCE FOR COOLING THE CABIN. ILLUSTRATION ADDED Preconditioned Airflow Requirements N UPDATED SCOPE FOR PRECONDITIONED AIRFLOW REQUIREMENTS. FIGURE Preconditioned Airflow Requirements N REVISED THE COOLING/HEATING PERFORMANCE GRAPH AS PER THE NEW CONDITIONS. ILLUSTRATION ADDED Section 5-8 Subject 5-8-0 Ground Towing Requirements R R R CROSS REFERENCED MANUAL(S) ADDED/REVISED/DELETED NOTE AMENDED HIGHLIGHTS Page 20 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Ground Towing Requirements Section 5-9 Subject 5-9-0 De-Icing and External Cleaning CHAPTER 6 Section 6-1 Subject 6-1-0 Engine Exhaust Velocities and Temperatures Subject 6-1-1 CHG CODE R DESCRIPTIONS OF CHANGE IMPROVED LAYOUT AND REVISED BREAKAWAY RESISTANCE TO 4%. ILLUSTRATION REVISED R R R PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED R R R R R Engine Exhaust Velocities Contours Ground Idle Power FIGURE Engine Exhaust Velocities Ground Idle Power -- CFM56 series engine R R ILLUSTRATION REVISED FIGURE Engine Exhaust Velocities Ground Idle Power -- IAE V2500 series engine R ILLUSTRATION REVISED Subject 6-1-2 R Engine Exhaust Temperatures Contours Ground Idle Power FIGURE Engine Exhaust Temperatures Ground Idle Power -- CFM56 series engine R R ILLUSTRATION REVISED FIGURE Engine Exhaust Temperatures Ground Idle Power -- IAE V2500 series engine R ILLUSTRATION REVISED Subject 6-1-5 Engine Exhaust Velocities Contours Takeoff Power FIGURE Engine Exhaust Velocities Takeoff Power -- CFM56 series engine R R R ILLUSTRATION REVISED HIGHLIGHTS Page 21 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Engine Exhaust Velocities Takeoff Power -- IAE V2500 series engine Subject 6-1-6 CHG CODE R DESCRIPTIONS OF CHANGE ILLUSTRATION REVISED R Engine Exhaust Temperatures Contours Takeoff Power FIGURE Engine Exhaust Temperatures Takeoff Power -- CFM56 series engine R R ILLUSTRATION REVISED FIGURE Engine Exhaust Temperatures Takeoff Power -- IAE V2500 series engine R ILLUSTRATION REVISED Section 6-2 Subject 6-2-0 Airport and Community Noise Subject 6-2-1 R R R R Noise Data FIGURE Airport and Community Noise CFM56-5A Series Engine R R FIGURE Airport and Community Noise CFM56-5B Series Engine R ADDED UNIT ”dB (A)” IN THE TABLE. ILLUSTRATION REVISED FIGURE Airport and Community Noise IAE V2500 Series Engine R ADDED UNIT ”dB (A)” IN THE TABLE. ILLUSTRATION REVISED Section 6-3 Subject 6-3-0 Danger Areas of Engines Subject 6-3-1 ADDED UNIT ”dB (A)” IN THE TABLE. ILLUSTRATION REVISED R R R R Ground Idle Power FIGURE Danger Areas of the Engines CFM56 series engine R R ILLUSTRATION REVISED FIGURE Danger Areas of the Engines IAE V2500 series engine R ILLUSTRATION REVISED Subject 6-3-2 Takeoff Power FIGURE Danger Areas of the Engines CFM56 series engine R R R ILLUSTRATION REVISED HIGHLIGHTS Page 22 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Danger Areas of the Engines IAE V2500 series engine CHG CODE R Section 6-4 Subject 06-04-00 R D Subject 6-4-1 R DESCRIPTIONS OF CHANGE ILLUSTRATION REVISED APU - APIC & GARRETT R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Exhaust Velocities and Temperatures - APU -- APIC & GARRETT R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED CHAPTER 7 Section 7-1 Subject 7-1-0 General Information Section 7-2 Subject 7-2-0 R R R R PART EFFECTIVITY ADDED/REVISED/DELETED CROSS REFERENCED DOCUMENTARY UNIT ADDED/REVISED/DELETED R R Landing Gear Footprint R PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED CROSS REFERENCED DOCUMENTARY UNIT ADDED/REVISED/DELETED FIGURE Landing Gear Footprint R FIGURE Landing Gear Footprint N REVISED ILLUSTRATION TO SHOW THE LANDING GEAR FOOTPRINT DATA FOR ALL THE WEIGHT VARIANTS OF A319-100. ILLUSTRATION REVISED ADDED ILLUSTRATION TO SHOW THE LANDING GEAR FOOTPRINT DATA FOR ALL THE WEIGHT VARIANTS OF A319 NEO. ILLUSTRATION ADDED Section 7-3 R HIGHLIGHTS Page 23 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS Subject 7-3-0 CHG CODE R DESCRIPTIONS OF CHANGE Maximum Pavement Loads R PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED CROSS REFERENCED DOCUMENTARY UNIT ADDED/REVISED/DELETED FIGURE Maximum Pavement Loads R FIGURE Maximum Pavement Loads N REVISED ILLUSTRATION TO SHOW THE MAXIMUM PAVEMENT LOADS FOR ALL THE WEIGHT VARIANTS OF A319-100. ILLUSTRATION REVISED ADDED ILLUSTRATION TO SHOW THE MAXIMUM PAVEMENT LOADS FOR ALL THE WEIGHT VARIANTS OF A319 NEO. ILLUSTRATION ADDED Section 7-4 Subject 7-4-0 R R Landing Gear Loading on Pavement R FIGURE Landing Gear Loading on Pavement - WV012, MRW 62 400 kg, CG 36% N FIGURE Landing Gear Loading on Pavement - WV010, MRW 76 900 kg, CG 36% N FIGURE Landing Gear Loading on Pavement - WV050, MRW 64 400 kg, CG 39% N FIGURE Landing Gear Loading on Pavement - WV054, MRW 75 900 kg, CG 36% N Subject 07-04-01 D Section 7-5 R PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED ADDED ILLUSTRATION FOR LANDING GEAR LOADING ON PAVEMENT FOR WV012. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR LANDING GEAR LOADING ON PAVEMENT FOR WV010. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR LANDING GEAR LOADING ON PAVEMENT FOR WV050 AND WV051. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR LANDING GEAR LOADING ON PAVEMENT FOR WV054 AND WV055. ILLUSTRATION ADDED HIGHLIGHTS Page 24 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS Subject 7-5-0 CHG CODE R DESCRIPTIONS OF CHANGE Flexible Pavement Requirements - US Army Corps of Engineers Design Method R DESCRIPTION TITLE UPDATED NOTE AMENDED FIGURE Flexible Pavement Requirements - WV012, MRW 62 400 kg, CG 36 % N FIGURE Flexible Pavement Requirements - WV010, MRW 76 900 kg, CG 36 % N FIGURE Flexible Pavement Requirements - WV050, MRW 64 400 kg, CG 39 % N FIGURE Flexible Pavement Requirements - WV054, MRW 75 900 kg, CG 36 % N ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV012. ILLUSTRATION ADDED ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV010. ILLUSTRATION ADDED ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV050 AND WV051. ILLUSTRATION ADDED ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV054 AND WV055. ILLUSTRATION ADDED Subject 07-05-01 D Section 7-6 Subject 7-6-0 R R Flexible Pavement Requirements - LCN Conversion R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Flexible Pavement Requirements - LCN Table N FIGURE Flexible - LCN - WV012, % FIGURE Flexible - LCN - WV010, % FIGURE Flexible - LCN Table Pavement Requirements MRW 62 400 kg, CG 36 N Pavement Requirements MRW 76 900 kg, CG 36 N Pavement Requirements N ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS - LCN DATA. ILLUSTRATION ADDED ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV012. ILLUSTRATION ADDED ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV010. ILLUSTRATION ADDED ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS - LCN DATA. ILLUSTRATION ADDED HIGHLIGHTS Page 25 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Flexible Pavement Requirements - LCN - WV050, MRW 64 400 kg, CG 39 % FIGURE Flexible Pavement Requirements - LCN - WV054, MRW 75 900 kg, CG 36 % CHG CODE N N Subject 07-06-01 D Section 7-7 Subject 7-7-0 R R Rigid Pavement Requirements - Portland Cement Association Design Method R FIGURE Rigid Pavement Requirements WV012, MRW 62 400 kg, CG 36 % N FIGURE Rigid Pavement Requirements WV010, MRW 76 900 kg, CG 36 % N FIGURE Rigid Pavement Requirements WV050, MRW 64 400 kg, CG 39 % N FIGURE Rigid Pavement Requirements WV054, MRW 75 900 kg, CG 36 % N Subject 07-07-01 D Section 7-8 Subject 7-8-0 R N Rigid Pavement Requirements - LCN Conversion FIGURE Rigid Pavement Requirements LCN Table FIGURE Rigid Pavement Requirements LCN Table DESCRIPTIONS OF CHANGE ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV050 AND WV051. ILLUSTRATION ADDED ADDED ILLUSTRATION OF FLEXIBLE PAVEMENT REQUIREMENTS FOR WV054 AND WV055. ILLUSTRATION ADDED PART EFFECTIVITY ADDED/REVISED/DELETED NOTE AMENDED ADDED ILLUSTRATION OF RIGID PAVEMENT REQUIREMENTS FOR ILLUSTRATION ADDED ADDED ILLUSTRATION OF RIGID PAVEMENT REQUIREMENTS FOR ILLUSTRATION ADDED ADDED ILLUSTRATION OF RIGID PAVEMENT REQUIREMENTS FOR AND WV051. ILLUSTRATION ADDED ADDED ILLUSTRATION OF RIGID PAVEMENT REQUIREMENTS FOR AND WV055. ILLUSTRATION ADDED WV012. WV010. WV050 WV054 N N ILLUSTRATION ADDED N ILLUSTRATION ADDED HIGHLIGHTS Page 26 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Radius of Relative Stiffness (L) FIGURE Rigid Pavement Requirements LCN - WV012, MRW 62 400 kg, CG 36 % FIGURE Rigid Pavement Requirements LCN - WV010, MRW 76 900 kg, CG 36 % FIGURE Rigid Pavement Requirements LCN - WV050, MRW 64 400 kg, CG 39 % FIGURE Rigid Pavement Requirements LCN - WV054, MRW 75 900 kg, CG 36 % FIGURE Radius of Relative Stiffness (Effect of E and µ on ”L” Values) CHG CODE N ILLUSTRATION ADDED N ILLUSTRATION ADDED N ILLUSTRATION ADDED N ILLUSTRATION ADDED N ILLUSTRATION ADDED N ILLUSTRATION ADDED Subject 07-08-01 D Subject 07-08-02 D Subject 07-08-03 D Subject 07-08-04 D Section 7-9 Subject 7-9-0 R R DESCRIPTIONS OF CHANGE Aircraft Classification Number - Flexible and Rigid Pavements R DESCRIPTION TITLE UPDATED NOTE AMENDED FIGURE Aircraft Classification Number ACN Table FIGURE Aircraft Classification Number Flexible Pavement - WV012, MRW 62 400 kg, CG 36 % N FIGURE Aircraft Classification Number Flexible Pavement - WV010, MRW 76 900 kg, CG 36 % N FIGURE Aircraft Classification Number ACN Table N ADDED ILLUSTRATION FOR ACN TABLE. ILLUSTRATION ADDED ADDED ILLUSTRATIONS OF FLEXIBLE AND RIGID PAVEMENT GRAPHS FOR WV012. ILLUSTRATION ADDED ADDED ILLUSTRATIONS OF FLEXIBLE AND RIGID PAVEMENT GRAPHS FOR WV010. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR ACN TABLE. ILLUSTRATION ADDED N HIGHLIGHTS Page 27 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Aircraft Classification Number Flexible Pavement - WV050, MRW 64 400 kg, CG 39 % FIGURE Aircraft Classification Number Flexible Pavement - WV054, MRW 75 900 kg, CG 36 % CHG CODE N N Subject 07-09-01 D Subject 07-09-02 D CHAPTER 8 Section 8-0 Subject 8-0-0 R R R DESCRIPTIONS OF CHANGE ADDED ILLUSTRATIONS OF FLEXIBLE AND RIGID PAVEMENT GRAPHS FOR WV050 AND WV051. ILLUSTRATION ADDED ADDED ILLUSTRATIONS OF FLEXIBLE AND RIGID PAVEMENT GRAPHS FOR WV054 AND WV055. ILLUSTRATION ADDED Scaled Drawings R PART EFFECTIVITY ADDED/REVISED/DELETED FIGURE Scaled Drawing R ILLUSTRATION REVISED PART EFFECTIVITY ADDED/REVISED/DELETED CHAPTER 10 Section 10-0 Subject 10-0-0 R R Aircraft Rescue and Fire Fighting N FIGURE Front Page N FIGURE Highly Flammable and Hazardous Materials and Components N FIGURE Batteries Location and Access N FIGURE Wheel/Brake Overheat - Wheel Safety Area N ADDED ”A319 neo” IN THE FRONT PAGE. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED ADDED ILLUSTRATION FOR BATTERIES LOCATION AND ACCESS. ILLUSTRATION ADDED REVISED TITLE TO ”WHEEL/BRAKE OVERHEAT”. ILLUSTRATION ADDED HIGHLIGHTS Page 28 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LOCATIONS FIGURE Composite Materials CHG CODE N FIGURE L/G Ground Lock Safety Devices N FIGURE Emergency Evacuation Devices N FIGURE Pax/Crew Doors N FIGURE Emergency Exit Hatch N FIGURE FWD and AFT Lower Deck Cargo Doors N FIGURE Control Panels N FIGURE APU Access Door N FIGURE Aircraft Ground Clearances N FIGURE Structural Break-in Points N DESCRIPTIONS OF CHANGE IMPROVED LAYOUT AND SPECIFIED THE LOCATION OF COMPOSITE MATERIALS. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED REVISED ILLUSTRATION TO SHOW THE GROUND CLEARANCE FOR ”RAT” AND ”SHARKLETS”. ILLUSTRATION ADDED IMPROVED LAYOUT. ILLUSTRATION ADDED HIGHLIGHTS Page 29 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING LIST OF EFFECTIVE CONTENT Revision No. 12 - May 01/14 CONTENT CHG CODE LAST REVISION DATE R May 01/14 N May 01/14 R May 01/14 General Aircraft Dimensions R May 01/14 FIGURE General Aircraft Dimensions - Wing Tip Fence R May 01/14 FIGURE General Aircraft Dimensions N May 01/14 Ground Clearances R May 01/14 FIGURE Ground Clearances R May 01/14 FIGURE Ground Clearances - Ground Clearances with Sharklets R May 01/14 FIGURE Ground Clearances N May 01/14 FIGURE Ground Clearances - Flaps and Flap Track Fairings When Flaps Fully Extended R May 01/14 FIGURE Ground Clearances - Flap Track Fairings Up R May 01/14 FIGURE Ground Clearances - Aileron Down R May 01/14 FIGURE Ground Clearances - Aileron Up and Spoilers 1 to 5 Extended R May 01/14 FIGURE Ground Clearances - Slats Extended R May 01/14 Interior Arrangements - Plan View R May 01/14 FIGURE Interior Arrangements - Plan View - Typical Configuration Single-Class, High Density R May 01/14 CHAPTER 1 Subject 1-1-0 Purpose Subject 1-2-0 Glossary CHAPTER 2 Subject 2-1-1 General Aircraft Characteristics Data Subject 2-2-0 Subject 2-3-0 Subject 2-4-1 L.E.C. Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 Interior Arrangements - Cross Section R May 01/14 FIGURE Interior Arrangements - Cross Section - Typical Configuration R May 01/14 FIGURE Interior Arrangements - Cross Section - Economy Class, 6 Abreast - Wider Aisle FIGURE Interior Arrangements - Cross Section - First-Class R May 01/14 R May 01/14 R May 01/14 R May 01/14 Door Clearances R May 01/14 FIGURE Door Identification and Location - Door Identification N May 01/14 Forward Passenger / Crew Doors R May 01/14 FIGURE Doors Clearances - Forward Passenger / Crew Doors R May 01/14 Emergency Exits R May 01/14 FIGURE Doors Clearances - Emergency Exits R May 01/14 Aft Passenger / Crew Doors R May 01/14 FIGURE Doors Clearances - Aft Passenger / Crew Doors R May 01/14 Forward Cargo Compartment Door R May 01/14 FIGURE Door Clearances - Forward Cargo Compartment Door R May 01/14 FIGURE Door Clearances - Forward Cargo Compartment Door N May 01/14 R May 01/14 FIGURE Interior Arrangements - Plan View - Typical Configuration Two-Class Subject 2-5-0 Subject 2-6-0 Cargo Compartments FIGURE Cargo Compartments - Locations, Dimensions and Loading Combinations Subject 2-7-0 Subject 2-7-1 Subject 2-7-2 Subject 2-7-3 Subject 2-7-4 Subject 2-7-5 Aft Cargo Compartment Door L.E.C. Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 Main Landing Gear Doors R May 01/14 FIGURE Doors Clearances - Main Landing Gear Doors R May 01/14 Radome R May 01/14 FIGURE Doors Clearances - Radome R May 01/14 APU and Nose Landing Gear Doors R May 01/14 FIGURE Doors Clearances - APU and Nose Landing Gear Doors R May 01/14 Escape Slides R May 01/14 FIGURE Escape Slides - Location R May 01/14 FIGURE Escape Slides - Dimensions R May 01/14 Landing Gear R May 01/14 FIGURE Landing Gear - Main Landing Gear - Twin-Wheel R May 01/14 FIGURE Landing Gear - Main Landing Gear Dimensions - Twin-Wheel R May 01/14 FIGURE Landing Gear - Nose Landing Gear R May 01/14 FIGURE Landing Gear - Nose Landing Gear Dimensions R May 01/14 Landing Gear Maintenance Pits R May 01/14 FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes R May 01/14 FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes R May 01/14 Exterior Lighting R May 01/14 FIGURE Exterior Lighting R May 01/14 FIGURE Exterior Lighting R May 01/14 FIGURE Exterior Lighting R May 01/14 FIGURE Exterior Lighting R May 01/14 FIGURE Doors Clearances - Aft Cargo Compartment Door Subject 2-7-7 Subject 2-7-8 Subject 2-7-9 Subject 2-8-0 Subject 2-9-0 Subject 2-10-0 L.E.C. Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE LAST REVISION DATE Antennas and Probes Location R May 01/14 FIGURE Antennas and Probes - Location R May 01/14 Auxiliary Power Unit R May 01/14 FIGURE Auxiliary Power Unit - Access Doors R May 01/14 FIGURE Auxiliary Power Unit - General Layout R May 01/14 Engine and Nacelle R May 01/14 FIGURE Power Plant Handling - Major Dimensions - CFM56 Series Engine R May 01/14 FIGURE Power Plant Handling - Major Dimensions - CFM56 Series Engine R May 01/14 FIGURE Power Plant Handling - Fan Cowls - CFM56 Series Engine R May 01/14 FIGURE Power Plant Handling - Thrust Reverser Cowls - CFM56 Series Engine R May 01/14 FIGURE Power Plant Handling - Major Dimensions - IAE V2500 Series Engine R May 01/14 FIGURE Power Plant Handling - Major Dimensions - IAE V2500 Series Engine R May 01/14 FIGURE Power Plant Handling - Fan Cowls - IAE V2500 Series Engine R May 01/14 FIGURE Power Plant Handling - Thrust Reverser Halves - IAE V2500 Series Engine R May 01/14 FIGURE Power Plant Handling - Major Dimensions - PW 1100G Engine N May 01/14 FIGURE Power Plant Handling - Fan Cowls - PW 1100G Engine N May 01/14 FIGURE Power Plant Handling - Thrust Reverser Halves - PW 1100G Engine N May 01/14 Leveling, Symmetry and Alignment R May 01/14 FIGURE Location of the Leveling Points R May 01/14 Subject 2-11-0 Subject 2-12-0 Subject 2-13-0 Subject 2-14-0 L.E.C. Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 FIGURE Jacking for Maintenance - Jacking Point Locations R May 01/14 FIGURE Jacking for Maintenance - Forward Jacking Point R May 01/14 FIGURE Jacking for Maintenance - Wing Jacking Points R May 01/14 FIGURE Jacking for Maintenance - Safety Stay R May 01/14 FIGURE Jacking for Maintenance - Jacking Design R May 01/14 FIGURE Loads at the Aircraft Jacking Points - Wing Jacking Point and Forward Fuselage Jacking Point R May 01/14 FIGURE Jacking for Maintenance - Location of Shoring Cradles R May 01/14 Jacking of the Landing Gear R May 01/14 FIGURE Jacking of the Twin Wheels FIGURE Jacking of the Jack - Twin Wheels FIGURE Jacking of the - Twin Wheels FIGURE Jacking of the - 75 500 kg Landing Gear - MLG Jacking Point Location - R May 01/14 Landing Gear - MLG Jacking with Cantilever R May 01/14 Landing Gear - Loads at MLG Jacking Points R May 01/14 Landing Gear - Loads at MLG Jacking Points R May 01/14 FIGURE Jacking of the Landing Gear - NLG Jacking - Point Location R May 01/14 FIGURE Jacking of the Landing Gear - Loads at NLG Jacking Points R May 01/14 FIGURE Jacking of the Landing Gear - Loads at NLG Jacking Points - 75 500 kg R May 01/14 N May 01/14 ISA Conditions R May 01/14 FIGURE Payload/Range N May 01/14 FIGURE Payload/Range - Sharklet N May 01/14 FIGURE Payload/Range N May 01/14 Jacking for Maintenance CHAPTER 3 Subject 3-1-0 General Information Subject 3-2-1 Subject 3-3-1 L.E.C. Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 FIGURE Take-Off Weight Limitation - ISA Conditions - CFM56 Series Engine R May 01/14 FIGURE Take-Off Weight Limitation - ISA Conditions - IAE V2500 Series Engine R May 01/14 Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions R May 01/14 FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions - CFM56 Series Engine R May 01/14 FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions - IAE V2500 Series Engine R May 01/14 Landing Field Length - ISA Conditions R May 01/14 FIGURE Landing Field Length - ISA Conditions - CFM56-5A Series Engine R May 01/14 FIGURE Landing Field Length - ISA Conditions - IAE V2500 Series Engine R May 01/14 R May 01/14 N May 01/14 Turning Radii R May 01/14 FIGURE Turning Radii, No Slip Angle R May 01/14 FIGURE Turning Radii, No Slip Angle R May 01/14 Minimum Turning Radii R May 01/14 FIGURE Minimum Turning Radii R May 01/14 R May 01/14 Take-Off Weight Limitation - ISA Conditions Subject 3-3-2 Subject 3-4-1 Subject 3-5-0 Final Approach Speed CHAPTER 4 Subject 4-1-0 General Information Subject 4-2-0 Subject 4-3-0 Subject 4-4-0 Visibility from Cockpit in Static Position L.E.C. Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 R May 01/14 R May 01/14 R May 01/14 R May 01/14 R May 01/14 R May 01/14 R May 01/14 R May 01/14 180˚ Turn on a Runway R May 01/14 FIGURE 180˚ Turn on a Runway - Edge of Runway Method R May 01/14 R May 01/14 R May 01/14 R May 01/14 R May 01/14 Runway Holding Bay (Apron) R May 01/14 FIGURE Runway Holding Bay (Apron) R May 01/14 FIGURE Visibility from Cockpit in Static Position FIGURE Binocular Visibility Through Windows from Captain Eye Position Subject 4-5-0 Runway and Taxiway Turn Paths Subject 4-5-1 135˚ Turn - Runway to Taxiway FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over Centerline Method FIGURE 135˚ Turn - Runway to Taxiway - Judgemental Oversteering Method Subject 4-5-2 90˚ Turn - Runway to Taxiway FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over Centerline Method FIGURE 90˚ Turn - Runway to Taxiway - Judgemental Oversteering Method Subject 4-5-3 Subject 4-5-4 135˚ Turn - Taxiway to Taxiway FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline Method Subject 4-5-5 90˚ Turn - Taxiway to Taxiway FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline Method Subject 4-6-0 Subject 4-7-0 L.E.C. Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 FIGURE Minimum Line-Up Distance Corrections - 90˚ Turn on Runway Entry N May 01/14 FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn on Runway Turn Pad N May 01/14 FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn on Runway Width N May 01/14 Aircraft Mooring N May 01/14 FIGURE Aircraft Mooring N May 01/14 R May 01/14 Typical Ramp Layout -- Open Apron R May 01/14 FIGURE Typical Ramp Layout - Open Apron - Bulk Loading R May 01/14 FIGURE Typical Ramp Layout - Open Apron - ULD Loading R May 01/14 Typical Ramp Layout - Gate R May 01/14 FIGURE Typical Ramp Layout - Gate R May 01/14 Terminal Operations - Full Servicing Turn Round Time R May 01/14 FIGURE Full Servicing Turn Round Time Chart R May 01/14 Terminal Operations - Outstation Turn Round Time R May 01/14 FIGURE Outstation Turn Round Time Chart R May 01/14 Ground Service Connections Layout R May 01/14 FIGURE Ground Service Connections Layout R May 01/14 Minimum Line-Up Distance Corrections Subject 4-8-0 CHAPTER 5 Subject 5-1-1 Aircraft Servicing Arrangements Subject 5-1-2 Subject 5-1-3 Subject 5-2-0 Subject 5-3-0 Subject 5-4-1 Subject 5-4-2 L.E.C. Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 FIGURE Ground Service Connections - Grounding (Earthing) Points Landing Gear R May 01/14 FIGURE Ground Service Connections - Grounding (Earthing) Points Wing (If Installed) R May 01/14 FIGURE Ground Service Connections - Grounding (Earthing) Point Avionics Compartment Door-Frame N May 01/14 FIGURE Ground Service Connections - Grounding (Earthing) Point Engine Air Intake (If Installed) N May 01/14 Hydraulic System R May 01/14 FIGURE Hydraulic System - Green System Ground Service Panel R May 01/14 FIGURE Hydraulic System - Blue System Ground Service Panel R May 01/14 FIGURE Hydraulic System - Yellow System Ground Service Panel R May 01/14 Electrical System R May 01/14 FIGURE Ground Service Connections - External Power Receptacles R May 01/14 Oxygen System R May 01/14 FIGURE Ground Service Connections - Oxygen System N May 01/14 Fuel System R May 01/14 FIGURE Ground Service Connections - Refuel/Defuel Control Panel R May 01/14 FIGURE Ground Service Connections - Refuel/Defuel Couplings R May 01/14 FIGURE Ground Service Connections - Overwing Gravity-Refuel Cap (If Installed) R May 01/14 R May 01/14 N May 01/14 Grounding (Earthing) Points Subject 5-4-3 Subject 5-4-4 Subject 5-4-5 Subject 5-4-6 FIGURE Ground Service Connections - Overpressure Protectors and NACA Vent Intake Subject 5-4-7 Pneumatic System L.E.C. Page 9 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE N LAST REVISION DATE May 01/14 Oil System R May 01/14 FIGURE Ground Service Connections - Engine Oil Tank -- CFM56 Series Engine N May 01/14 FIGURE Ground Service Connections - IDG Oil Tank -- CFM56 Series Engine N May 01/14 FIGURE Ground Service Connections - Starter Oil Tank -- CFM56 Series Engine N May 01/14 FIGURE Ground Service Connections - Engine Oil Tank -- IAE V2500 Series Engine N May 01/14 FIGURE Ground Service Connections - IDG Oil Tank -- IAE V2500 Series Engine N May 01/14 FIGURE Ground Service Connections - Starter Oil Tank -- IAE V2500 Series Engine N May 01/14 FIGURE Ground Service Connections - APU Oil Tank N May 01/14 Potable Water System R May 01/14 FIGURE Ground Service Connections - Potable Water Ground Service Panels FIGURE Ground Service Connections - Potable Water Tank Location N May 01/14 N May 01/14 Vacuum Toilet System R May 01/14 FIGURE Ground Service Connections - Waste Water Ground Service Panel FIGURE Ground Service Connections - Waste Tank Location R May 01/14 N May 01/14 Engine Starting Pneumatic Requirements R May 01/14 FIGURE Example for Use of the Charts N May 01/14 FIGURE Engine Starting Pneumatic Requirements - IAE V2500 Series Engine N May 01/14 FIGURE Ground Service Connections - LP and HP Ground Connectors Subject 5-4-8 Subject 5-4-9 Subject 5-4-10 Subject 5-5-0 L.E.C. Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE N LAST REVISION DATE May 01/14 N May 01/14 Ground Pneumatic Power Requirements N May 01/14 FIGURE Ground Pneumatic Power Requirements - Heating N May 01/14 FIGURE Ground Pneumatic Power Requirements - Cooling N May 01/14 Preconditioned Airflow Requirements N May 01/14 FIGURE Preconditioned Airflow Requirements N May 01/14 Ground Towing Requirements R May 01/14 FIGURE Ground Towing Requirements R May 01/14 R May 01/14 R May 01/14 Engine Exhaust Velocities Contours - Ground Idle Power R May 01/14 FIGURE Engine Exhaust Velocities - Ground Idle Power -- CFM56 series engine R May 01/14 FIGURE Engine Exhaust Velocities - Ground Idle Power -- IAE V2500 series engine R May 01/14 Engine Exhaust Temperatures Contours - Ground Idle Power R May 01/14 FIGURE Engine Exhaust Temperatures - Ground Idle Power -- CFM56 series engine R May 01/14 FIGURE Engine Exhaust Temperatures - Ground Idle Power -- IAE V2500 series engine R May 01/14 FIGURE Engine Starting Pneumatic Requirements - CFM56 Series and CFM LEAP-1A NEO Engine FIGURE Engine Starting Pneumatic Requirements - PW 1100G NEO Engine Subject 5-6-0 Subject 5-7-0 Subject 5-8-0 Subject 5-9-0 De-Icing and External Cleaning CHAPTER 6 Subject 6-1-0 Engine Exhaust Velocities and Temperatures Subject 6-1-1 Subject 6-1-2 L.E.C. Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE LAST REVISION DATE Engine Exhaust Velocities Contours - Takeoff Power R May 01/14 FIGURE Engine Exhaust Velocities - Takeoff Power -- CFM56 series engine R May 01/14 FIGURE Engine Exhaust Velocities - Takeoff Power -- IAE V2500 series engine R May 01/14 Engine Exhaust Temperatures Contours - Takeoff Power R May 01/14 FIGURE Engine Exhaust Temperatures - Takeoff Power -- CFM56 series engine R May 01/14 FIGURE Engine Exhaust Temperatures - Takeoff Power -- IAE V2500 series engine R May 01/14 R May 01/14 Noise Data R May 01/14 FIGURE Airport and Community Noise - CFM56-5A Series Engine R May 01/14 FIGURE Airport and Community Noise - CFM56-5B Series Engine R May 01/14 FIGURE Airport and Community Noise - IAE V2500 Series Engine R May 01/14 R May 01/14 Ground Idle Power R May 01/14 FIGURE Danger Areas of the Engines - CFM56 series engine R May 01/14 FIGURE Danger Areas of the Engines - IAE V2500 series engine R May 01/14 Takeoff Power R May 01/14 FIGURE Danger Areas of the Engines - CFM56 series engine R May 01/14 FIGURE Danger Areas of the Engines - IAE V2500 series engine R May 01/14 Subject 6-1-5 Subject 6-1-6 Subject 6-2-0 Airport and Community Noise Subject 6-2-1 Subject 6-3-0 Danger Areas of Engines Subject 6-3-1 Subject 6-3-2 Subject 6-4-1 L.E.C. Page 12 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE R LAST REVISION DATE May 01/14 R May 01/14 R May 01/14 Landing Gear Footprint R May 01/14 FIGURE Landing Gear Footprint R May 01/14 FIGURE Landing Gear Footprint N May 01/14 Maximum Pavement Loads R May 01/14 FIGURE Maximum Pavement Loads R May 01/14 FIGURE Maximum Pavement Loads N May 01/14 Landing Gear Loading on Pavement R May 01/14 FIGURE Landing Gear Loading on Pavement - WV012, MRW 62 400 kg, CG 36% N May 01/14 FIGURE Landing Gear Loading on Pavement - WV010, MRW 76 900 kg, CG 36% N May 01/14 FIGURE Landing Gear Loading on Pavement - WV050, MRW 64 400 kg, CG 39% N May 01/14 FIGURE Landing Gear Loading on Pavement - WV054, MRW 75 900 kg, CG 36% N May 01/14 Flexible Pavement Requirements - US Army Corps of Engineers Design Method R May 01/14 FIGURE Flexible Pavement Requirements - WV012, MRW 62 400 kg, CG 36 % FIGURE Flexible Pavement Requirements - WV010, MRW 76 900 kg, CG 36 % N May 01/14 N May 01/14 APU - APIC & GARRETT FIGURE Exhaust Velocities and Temperatures - APU -- APIC & GARRETT CHAPTER 7 Subject 7-1-0 General Information Subject 7-2-0 Subject 7-3-0 Subject 7-4-0 Subject 7-5-0 L.E.C. Page 13 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE N LAST REVISION DATE May 01/14 N May 01/14 Flexible Pavement Requirements - LCN Conversion R May 01/14 FIGURE Flexible Pavement Requirements - LCN Table N May 01/14 FIGURE Flexible Pavement Requirements - LCN - WV012, MRW 62 400 kg, CG 36 % N May 01/14 FIGURE Flexible Pavement Requirements - LCN - WV010, MRW 76 900 kg, CG 36 % N May 01/14 FIGURE Flexible Pavement Requirements - LCN Table N May 01/14 FIGURE Flexible Pavement Requirements - LCN - WV050, MRW 64 400 kg, CG 39 % N May 01/14 FIGURE Flexible Pavement Requirements - LCN - WV054, MRW 75 900 kg, CG 36 % N May 01/14 R May 01/14 N May 01/14 N May 01/14 N May 01/14 N May 01/14 Rigid Pavement Requirements - LCN Conversion N May 01/14 FIGURE Rigid Pavement Requirements - LCN Table N May 01/14 FIGURE Rigid Pavement Requirements - LCN Table N May 01/14 FIGURE Radius of Relative Stiffness (L) N May 01/14 FIGURE Flexible Pavement Requirements - WV050, MRW 64 400 kg, CG 39 % FIGURE Flexible Pavement Requirements - WV054, MRW 75 900 kg, CG 36 % Subject 7-6-0 Subject 7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method FIGURE Rigid Pavement Requirements - WV012, MRW 62 400 kg, CG 36 % FIGURE Rigid Pavement Requirements - WV010, MRW 76 900 kg, CG 36 % FIGURE Rigid Pavement Requirements - WV050, MRW 64 400 kg, CG 39 % FIGURE Rigid Pavement Requirements - WV054, MRW 75 900 kg, CG 36 % Subject 7-8-0 L.E.C. Page 14 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE N LAST REVISION DATE May 01/14 FIGURE Rigid Pavement Requirements - LCN - WV010, MRW 76 900 kg, CG 36 % N May 01/14 FIGURE Rigid Pavement Requirements - LCN - WV050, MRW 64 400 kg, CG 39 % N May 01/14 FIGURE Rigid Pavement Requirements - LCN - WV054, MRW 75 900 kg, CG 36 % N May 01/14 FIGURE Radius of Relative Stiffness (Effect of E and µ on ”L” Values) N May 01/14 Aircraft Classification Number - Flexible and Rigid Pavements R May 01/14 FIGURE Aircraft Classification Number - ACN Table N May 01/14 FIGURE Aircraft Classification Number - Flexible Pavement - WV012, MRW 62 400 kg, CG 36 % N May 01/14 FIGURE Aircraft Classification Number - Flexible Pavement - WV010, MRW 76 900 kg, CG 36 % N May 01/14 FIGURE Aircraft Classification Number - ACN Table N May 01/14 FIGURE Aircraft Classification Number - Flexible Pavement - WV050, MRW 64 400 kg, CG 39 % N May 01/14 FIGURE Aircraft Classification Number - Flexible Pavement - WV054, MRW 75 900 kg, CG 36 % N May 01/14 Scaled Drawings R May 01/14 FIGURE Scaled Drawing R May 01/14 Aircraft Rescue and Fire Fighting N May 01/14 FIGURE Front Page N May 01/14 FIGURE Highly Flammable and Hazardous Materials and Components N May 01/14 FIGURE Rigid Pavement Requirements - LCN - WV012, MRW 62 400 kg, CG 36 % Subject 7-9-0 CHAPTER 8 Subject 8-0-0 CHAPTER 10 Subject 10-0-0 L.E.C. Page 15 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE N LAST REVISION DATE May 01/14 FIGURE Wheel/Brake Overheat - Wheel Safety Area N May 01/14 FIGURE Composite Materials N May 01/14 FIGURE L/G Ground Lock Safety Devices N May 01/14 FIGURE Emergency Evacuation Devices N May 01/14 FIGURE Pax/Crew Doors N May 01/14 FIGURE Emergency Exit Hatch N May 01/14 FIGURE FWD and AFT Lower Deck Cargo Doors N May 01/14 FIGURE Control Panels N May 01/14 FIGURE APU Access Door N May 01/14 FIGURE Aircraft Ground Clearances N May 01/14 FIGURE Structural Break-in Points N May 01/14 FIGURE Batteries Location and Access L.E.C. Page 16 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING TABLE OF CONTENTS 1 1-1-0 1-2-0 SCOPE Introduction Glossary 2 AIRCRAFT DESCRIPTION 2-1-1 General Aircraft Characteristics Data 2-2-0 General Aircraft Dimensions 2-3-0 Ground Clearances 2-4-1 Interior Arrangements - Plan View 2-5-0 Interior Arrangements - Cross Section 2-6-0 Cargo Compartments 2-7-0 Door Clearances and Location 2-7-1 Forward Passenger / Crew Doors 2-7-2 Emergency Exits 2-7-3 Aft Passenger / Crew Doors 2-7-4 Forward Cargo Compartment Door 2-7-5 Aft Cargo Compartment Door 2-7-7 Main Landing Gear Doors 2-7-8 Radome 2-7-9 APU and Nose Landing Gear Doors 2-8-0 Escape Slides 2-9-0 Landing Gear 2-10-0 Exterior Lighting 2-11-0 Antennas and Probes Location 2-12-0 Power Plant 2-13-0 Leveling, Symmetry and Alignment 2-14-0 Jacking 3 3-1-0 3-2-1 3-3-1 3-3-2 3-4-1 3-5-0 AIRCRAFT PERFORMANCE General Information Payload / Range - ISA Conditions Take-off Weight Limitation - ISA Conditions Take-off Weight Limitation - ISA +15¿C (+59¿F) Conditions Landing Field Length - ISA Conditions Final Approach Speed T.O.C. Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4 4-1-0 4-2-0 4-3-0 4-4-0 4-5-0 4-5-1 4-5-2 4-5-3 4-5-4 4-5-5 4-6-0 4-7-0 4-8-0 GROUND MANEUVERING General Information Turning Radii Minimum Turning Radii Visibility from Cockpit in Static Position Runway and Taxiway Turn Paths 135˚ Turn - Runway to Taxiway 90˚ Turn - Runway to Taxiway 180˚ Turn on a Runway 135˚ Turn - Taxiway to Taxiway 90˚ Turn - Taxiway to Taxiway Runway Holding Bay (Apron) Minimum Line-Up Distance Corrections Aircraft Mooring 5 TERMINAL SERVICING 5-1-1 Aircraft Servicing Arrangements 5-1-2 Typical Ramp Layout - Open Apron 5-1-3 Typical Ramp Layout - Gate 5-2-0 Terminal Operations - Full Servicing Turn Round Time Chart 5-3-0 Terminal Operation - Outstation Turn Round Time Chart 5-4-1 Ground Service Connections 5-4-2 Grounding Points 5-4-3 Hydraulic System 5-4-4 Electrical System 5-4-5 Oxygen System 5-4-6 Fuel System 5-4-7 Pneumatic System 5-4-8 Oil System 5-4-9 Potable Water System 5-4-10 Waste Water System 5-5-0 Engine Starting Pneumatic Requirements 5-6-0 Ground Pneumatic Power Requirements 5-7-0 Preconditioned Airflow Requirements 5-8-0 Ground Towing Requirements 5-9-0 De-Icing and External Cleaning T.O.C. Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6 6-1-0 6-1-1 6-1-2 6-1-5 6-1-6 6-2-0 6-2-1 6-3-0 6-3-1 6-3-2 6-4-1 OPERATING CONDITIONS Engine Exhaust Velocities and Temperatures Engine Exhaust Velocities Contours - Ground Idle Power Engine Exhaust Temperatures Contours - Ground Idle Power Engine Exhaust Velocities Contours - Takeoff Power Engine Exhaust Temperatures Contours - Takeoff Power Airport and Community Noise Noise Data Danger Areas of Engines Ground Idle Power Takeoff Power APU 7 7-1-0 7-2-0 7-3-0 7-4-0 7-5-0 7-6-0 7-7-0 7-8-0 7-9-0 PAVEMENT DATA General Information Landing Gear Footprint Maximum Pavement Loads Landing Gear Loading on Pavement Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method Flexible Pavement Requirements - LCN Conversion Rigid Pavement Requirements - Portland Cement Association Design Method Rigid Pavement Requirements - LCN Conversion ACN/PCN Reporting System - Flexible and Rigid Pavements 8 8-0-0 SCALED DRAWINGS SCALED DRAWINGS 10 AIRCRAFT RESCUE AND FIRE FIGHTING 10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING T.O.C. Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING SCOPE 1-1-0 Introduction **ON A/C A319-100 A319neo Purpose 1. General The A319 AIRCRAFT CHARACTERISTICS -- AIRPORT AND MAINTENANCE PLANNING (AC) manual is issued for the A319-100 series aircraft equipped with wing-tip fences or sharklets, to provide necessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO) for airport and maintenance facilities planning. Preliminary information on neo (New Engine Option) given in this document can be subject to change, pending completion of the flight test phase. This document is not customized and must not be used for training purposes. No information within may constitute a contractual commitment. The A320 Family is the world’s best-selling single-aisle aircraft. An A320 takes off or lands somewhere in the world every 2.5 seconds of every day, the family has logged more than 50 million cycles since entry-into-service and records a best-in-class dispatch reliability of 99.7%. To ensure this true market leadership, Airbus continues to invest in improvements in the A320 Family: enhancements to aerodynamics such as the sharklet wingtip devices, upgrades to the widest passenger cabin in its class, the A320 Family neo. The latter combines top-of-class engine efficiency offered by two new engine options: the PW1100G PurePower from Pratt&Whitney and the LEAP-1A from CFM International with superior aerodynamics offered by the new sharklet devices. The neo will offer a minimum of 15% fuel savings and an additional flight range of about 500 nm (926 km). For the environment, the neo fuel savings will translate into some 3 600 t (7 936 639 lb) less CO2 per aircraft per year, together with a double-digit reduction in NOx emissions and reduced engine noise. Correspondence concerning this publication should be directed to: AIRBUS S.A.S. Customer Services Technical Data Support and Services 1, Rond Point Maurice BELLONTE 31707 BLAGNAC CEDEX FRANCE 1-1-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 1-2-0 Glossary **ON A/C A319-100 A319neo Glossary 1. List of Abbreviations A/C ACN AMM APU B/C CBR CC CG CKPT E ELEC ESWL FAA F/C FDL FR FSTE FWD GPU GSE HYD ICAO IDG ISA L L LCN LD L/G LH LPS MAC MAX Aircraft Aircraft Classification Number Aircraft Maintenance Manual Auxiliary Power Unit Business Class California Bearing Ratio Cargo Compartment Center of Gravity Cockpit Young’s Modulus Electric, Electrical, Electricity Equivalent Single Wheel Load Federal Aviation Administration First Class Fuselage Datum Line Frame Full Size Trolley Equivalent Forward Ground Power Unit Ground Support Equipment Hydraulic International Civil Aviation Organisation Integrated Drive Generator International Standard Atmosphere Left Radius of relative stiffness Load Classification Number Lower Deck Landing Gear Left Hand Last Pax Seating Mean Aerodynamic Chord Maximum 1-2-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING MIN MLG NLG OAT PAX PBB PCA PCN PRM R RH ULD US WV Y/C 2. Minimum Main Landing Gear Nose Landing Gear Outside Air Temperature Passenger Passenger Boarding Bridge Portland Cement Association Pavement Classification Number Passenger with Reduced Mobility Right Right Hand Unit Load Device United States Weight Variant Tourist Class Design Weight Terminology - Maximum Design Ramp Weight (MRW): Maximum weight for ground maneuver (including weight of taxi and run-up fuel) as limited by aircraft strength and airworthiness requirements. It is also called Maximum Design Taxi Weight (MTW). - Maximum Design Landing Weight (MLW): Maximum weight for landing as limited by aircraft strength and airworthiness requirements. - Maximum Design Takeoff Weight (MTOW): Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (This is the maximum weight at start of the take-off run). - Maximum Design Zero Fuel Weight (MZFW): Maximum permissible weight of the aircraft without usable fuel. - Maximum Seating Capacity: Maximum number of passengers specifically certified or anticipated for certification. - Usable Volume: Usable volume available for cargo, pressurized fuselage, passenger compartment and cockpit. - Water Volume: Maximum volume of cargo compartment. - Usable Fuel: Fuel available for aircraft propulsion. 1-2-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-1-1 General Aircraft Characteristics Data **ON A/C A319-100 A319neo General Aircraft Characteristics Data **ON A/C A319-100 1. The following table provides characteristics of A319-100 Models, these data are specific to each Weight Variant: Aircraft Characteristics WV000 WV001 WV002 Maximum (MRW) Maximum Maximum (MTOW) Maximum (MLW) Maximum (MZFW) Ramp Weight Taxi Weight (MTW) Take-Off Weight Landing Weight Zero Fuel Weight WV003 64 400 kg (141 978 lb) 70 400 kg 75 900 kg 68 400 kg (155 205 lb) (167 331 lb) (150 796 lb) 68 400 kg (150 796 lb) 64 000 kg (141 096 lb) 61 000 kg (134 482 lb) 57 000 kg (125 663 lb) 70 000 kg 75 500 kg 68 000 kg (154 324 lb) (166 449 lb) (149 914 lb) 61 000 kg 62 500 kg 61 000 kg (134 482 lb) (137 789 lb) (134 482 lb) 57 000 kg 58 500 kg 57 000 kg (125 663 lb) (128 970 lb) (125 663 lb) 68 000 kg (149 914 lb) 62 500 kg (137 789 lb) 58 500 kg (128 970 lb) Aircraft Characteristics WV005 WV006 WV007 Maximum (MRW) Maximum Maximum (MTOW) Maximum (MLW) Maximum (MZFW) Ramp Weight Taxi Weight (MTW) Take-Off Weight Landing Weight Zero Fuel Weight Maximum Ramp Weight (MRW) Maximum Taxi Weight (MTW) Maximum Take-Off Weight (MTOW) WV004 WV008 WV009 70 400 kg (155 205 lb) 73 900 kg 75 900 kg 64 400 kg 66 400 kg (162 922 lb) (167 331 lb) (141 978 lb) (146 387 lb) 70 000 kg (154 324 lb) 62 500 kg (137 789 lb) 58 500 kg (128 970 lb) 73 500 kg 75 500 kg 64 000 kg 66 000 kg (162 040 lb) (166 449 lb) (141 096 lb) (145 505 lb) 62 500 kg 61 000 kg 62 500 kg 62 500 kg (137 789 lb) (134 482 lb) (137 789 lb) (137 789 lb) 58 500 kg 57 000 kg 58 500 kg 58 500 kg (128 970 lb) (125 663 lb) (128 970 lb) (128 970 lb) Aircraft Characteristics WV010 WV011 76 900 kg 66 400 kg (169 535 lb) (146 387 lb) 76 500 kg 66 000 kg (168 653 lb) (145 505 lb) WV012 62 400 kg (137 568 lb) 62 000 kg (136 686 lb) 2-1-1 WV013 75 900 kg (167 331 lb) 75 500 kg (166 449 lb) Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING Maximum Landing Weight (MLW) Maximum Zero Fuel Weight (MZFW) Aircraft Characteristics WV010 WV011 62 500 kg 61 000 kg (137 789 lb) (134 482 lb) 58 500 kg 57 000 kg (128 970 lb) (125 663 lb) WV012 61 000 kg (134 482 lb) 57 000 kg (125 663 lb) WV013 62 500 kg (137 789 lb) 52 000 kg (114 640 lb) **ON A/C A319neo 2. The following table provides characteristics of A319neo Models, these data are specific to each Weight Variant: Maximum Ramp Weight (MRW) Maximum Taxi Weight (MTW) Maximum Take-Off Weight (MTOW) Maximum Landing Weight (MLW) Maximum Zero Fuel Weight (MZFW) Maximum Ramp Weight (MRW) Maximum Taxi Weight (MTW) Maximum Take-Off Weight (MTOW) Maximum Landing Weight (MLW) Maximum Zero Fuel Weight (MZFW) Aircraft Characteristics WV050 64 400 kg (141 978 lb) 64 000 kg (141 096 lb) 62 800 kg (138 450 lb) 58 800 kg (129 632 lb) Aircraft Characteristics WV053 70 400 kg (155 205 lb) 70 000 kg (154 323 lb) 63 900 kg (140 875 lb) 60 300 kg (132 939 lb) WV051 64 400 kg (141 978 lb) 64 000 kg (141 096 lb) 63 900 kg (140 875 lb) 60 300 kg (132 939 lb) WV054 75 900 kg (167 331 lb) 75 500 kg (166 449 lb) 62 800 kg (138 450 lb) 58 800 kg (129 632 lb) WV052 70 400 kg (155 205 lb) 70 000 kg (154 323 lb) 62 800 kg (138 450 lb) 58 800 kg (129 632 lb) WV055 75 900 kg (167 331 lb) 75 500 kg (166 449 lb) 63 900 kg (140 875 lb) 60 300 kg (132 939 lb) **ON A/C A319-100 A319neo 3. The following table provides characteristics of A319-100 and A319neo Models, these data are common to each Weight Variant: Standard Seating Capacity Aircraft Characteristics 156 (Single-Class) 2-1-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING Aircraft Characteristics Usable Fuel Capacity (density = 0.785 kg/l) Pressurized Fuselage Volume (A/C non equipped) Passenger Compartment Volume Cockpit Volume Usable Volume, FWD CC Usable Volume, AFT CC Usable Volume, Bulk CC Water Volume, FWD CC Water Volume, AFT CC Water Volume, Bulk CC 23 859 l (6 303 US gal) 18 729 kg (41 290 lb) 285 m3 (10 065 ft3) 120 m3 (4 238 ft3) 9 m3 (318 ft3) 8.52 m3 (301 ft3) 11.92 m3 (421 ft3) 7.22 m3 (255 ft3) 10.63 m3 (375 ft3) 13.91 m3 (491 ft3) 7.51 m3 (265 ft3) 2-1-1 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-2-0 General Aircraft Dimensions **ON A/C A319-100 A319neo General Aircraft Dimensions 1. This section provides general aircraft dimensions. 2-2-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5.07 m (16.63 ft) 5.87 m (19.26 ft) 4.14 m (13.58 ft) **ON A/C A319-100 OPTIONAL 11.04 m (36.22 ft) 34.10 m (111.88 ft) 12.45 m (40.85 ft) 0.50 m (1.64 ft) 0.93 m (3.05 ft) 7.59 m (24.90 ft) 8.95 m (29.36 ft) RELATED TO AIRCRAFT ATTITUDE AND WEIGHT N_AC_020200_1_0020101_01_03 General Aircraft Dimensions Wing Tip Fence (Sheet 1 of 4) FIGURE-2-2-0-991-002-A01 2-2-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 33.84 m (111.02 ft) 6.07 m (19.91 ft) 5.75 m (18.86 ft) 1.24 m 3.95 m (4.07 ft) (12.96 ft) 3.31 m (10.86 ft) 8.30 m (27.23 ft) CFM56 9.60 m (31.50 ft) V2500 9.52 m (31.23 ft) 11.91 m (39.07 ft) 4.87 m (15.98 ft) 1.50 m (4.92 ft) 1.82 m (5.97 ft) 0.76 m (2.49 ft) 20.86 m (68.44 ft) NOTE: RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. N_AC_020200_1_0020103_01_01 General Aircraft Dimensions Wing Tip Fence (Sheet 2 of 4) FIGURE-2-2-0-991-002-A01 2-2-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5.07 m (16.63 ft) 5.87 m (19.26 ft) 4.14 m (13.58 ft) **ON A/C A319-100 OPTIONAL 11.04 m (36.23 ft) 35.80 m (117.45 ft) 12.45 m (40.85 ft) 3.79 m (12.43 ft) 2.43 m (7.97 ft) 0.50 m (1.64 ft) 0.93 m (3.05 ft) 7.59 m (24.90 ft) 8.95 m (29.36 ft) RELATED TO AIRCRAFT ATTITUDE AND WEIGHT N_AC_020200_1_0020102_01_01 General Aircraft Dimensions Sharklet (Sheet 3 of 4) FIGURE-2-2-0-991-002-A01 2-2-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 33.84 m (111.02 ft) 6.07 m (19.91 ft) 5.75 m (18.86 ft) 1.24 m 3.95 m (4.07 ft) (12.96 ft) 3.31 m (10.86 ft) 8.30 m (27.23 ft) CFM56 9.60 m (31.50 ft) V2500 9.52 m (31.23 ft) 11.91 m (39.07 ft) 4.87 m (15.98 ft) 1.64 m (5.38 ft) 3.22 m (10.56 ft) 16.29 m (53.44 ft) 1.61 m (5.28 ft) 21.85 m (71.69 ft) NOTE: RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. N_AC_020200_1_0020104_01_01 General Aircraft Dimensions Sharklet (Sheet 4 of 4) FIGURE-2-2-0-991-002-A01 2-2-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo 5.87 m (19.26 ft) 4.14 m (13.58 ft) OPTIONAL 11.04 m (36.23 ft) 5.07 m (16.63 ft) 35.80 m (117.45 ft) 12.45 m (40.85 ft) 2.43 m (7.97 ft) 3.79 m (12.43 ft) 0.50 m (1.64 ft) NOTE: RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. 0.93 m (3.05 ft) 7.59 m (24.90 ft) 8.95 m (29.36 ft) N_AC_020200_1_0080101_01_00 General Aircraft Dimensions (Sheet 1 of 2) FIGURE-2-2-0-991-008-A01 2-2-0 Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo 33.84 m (111.02 ft) 6.07 m (19.91 ft) 5.75 m (18.86 ft) 1.24 m 3.95 m (4.07 ft) (12.96 ft) 3.31 m (10.86 ft) 8.30 m (27.23 ft) CFM LEAP−1A/ PW 1100G 9.54 m (31.30 ft) 11.91 m (39.07 ft) 4.87 m (15.98 ft) 1.64 m (5.38 ft) 3.22 m (10.56 ft) 16.29 m (53.44 ft) 1.61 m (5.28 ft) 21.85 m (71.69 ft) NOTE: RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. N_AC_020200_1_0080102_01_00 General Aircraft Dimensions (Sheet 2 of 2) FIGURE-2-2-0-991-008-A01 2-2-0 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-3-0 Ground Clearances **ON A/C A319-100 A319neo Ground Clearances 1. This section provides the height of various points of the aircraft, above the ground, for different aircraft configurations. Dimensions in the tables are approximate and will vary with tire type, weight and balance and other special conditions. The dimensions are given for: - A light weight, for an A/C in maintenance configuration with a mid CG, - An aircraft at Maximum Ramp Weight with a FWD CG and an AFT CG, - Aircraft on jacks, FDL at 4.60 m (15.09 ft). NOTE : Passenger and cargo door ground clearances are measured from the center of the door sill and from floor level. 2-3-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING F1 F N G C2 D2 H L J Q NOTE: FOR DIMENSIONS, SEE SHEET 2. PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL. E F2 D1 B F3 C1 A P K1 K2 **ON A/C A319-100 N_AC_020300_1_0020101_01_05 Ground Clearances (Sheet 1 of 2) FIGURE-2-3-0-991-002-A01 2-3-0 Page 2 May 01/14 A B C1 C2 D1 D2 E (CFM) E (IAE) F F1 F2 F3 G H J K1 K2 L N P Q A/C CONFIGURATION CG 28% m ft 3.47 11.38 2.09 6.86 6.00 1.83 6.36 1.94 19.59 5.97 19.98 6.09 2.20 0.67 2.79 0.85 5.68 1.73 8.96 2.73 10.37 3.16 11.48 3.50 7.28 2.22 3.71 12.17 12.11 39.73 12.80 3.90 4.87 15.98 18.31 5.58 13.02 3.97 13.98 4.26 15.98 4.87 40 000 kg (88 185 lb) FWD CG 21% m ft 11.09 3.38 6.53 1.99 5.68 1.73 6.04 1.84 19.29 5.88 19.65 5.99 1.87 0.57 2.49 0.76 5.35 1.63 8.63 2.63 10.04 3.06 3.41 11.19 6.96 2.12 3.61 11.84 12.01 39.40 3.81 12.50 15.68 4.78 17.98 5.48 12.73 3.88 13.65 4.16 15.68 4.78 AFT CG 36% m ft 11.25 3.43 2.03 6.66 5.77 1.76 5.94 1.81 19.36 5.90 19.52 5.95 1.90 0.58 2.49 0.76 5.31 1.62 8.56 2.61 9.97 3.04 11.09 3.38 6.86 2.09 11.61 3.54 11.89 39.01 3.77 12.37 15.55 4.74 17.62 5.37 12.73 3.88 13.91 4.24 15.26 4.65 MRW m 4.13 2.71 2.43 2.43 6.58 6.58 1.24 1.42 2.26 3.25 3.68 4.01 2.71 4.13 12.45 4.38 5.35 5.93 4.54 4.96 5.20 ft 13.55 8.89 7.97 7.97 21.59 21.59 4.07 4.66 7.41 10.66 12.07 13.16 8.89 13.55 40.85 14.37 17.55 19.46 14.89 16.27 17.06 A/C JACKED FDL = 4.60 m (15.09 ft) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_020300_1_0020102_01_00 Ground Clearances (Sheet 2 of 2) FIGURE-2-3-0-991-002-A01 2-3-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING F1 F N G C2 D2 H L J Q NOTE: FOR DIMENSIONS, SEE SHEET 2. PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL. E F2 D1 B F3 C1 A P K1 K2 **ON A/C A319-100 N_AC_020300_1_0280101_01_01 Ground Clearances Ground Clearances with Sharklets (Sheet 1 of 2) FIGURE-2-3-0-991-028-A01 2-3-0 Page 4 May 01/14 A B C1 C2 D1 D2 E (CFM) E (IAE) F F1 F2 F3 G H J K1 K2 L N P Q A/C CONFIGURATION CG 28% m ft 3.47 11.38 2.09 6.86 6.00 1.83 6.36 1.94 19.59 5.97 19.98 6.09 2.20 0.67 2.79 0.85 5.68 1.73 8.96 2.73 10.37 3.16 11.48 3.50 7.28 2.22 3.71 12.17 12.11 39.73 13.68 4.17 6.81 22.34 18.31 5.58 13.02 3.97 13.98 4.26 15.98 4.87 40 000 kg (88 185 lb) FWD CG 21% m ft 11.09 3.38 6.53 1.99 1.73 5.68 1.84 6.04 19.29 5.88 19.65 5.99 1.87 0.57 2.49 0.76 5.35 1.63 8.63 2.63 10.04 3.06 3.41 11.19 6.96 2.12 3.61 11.84 12.01 39.40 13.39 4.08 22.05 6.72 17.98 5.48 12.73 3.88 13.65 4.16 15.68 4.78 AFT CG 36% m ft 11.25 3.43 2.03 6.66 5.77 1.76 5.94 1.81 19.36 5.90 19.52 5.95 1.90 0.58 2.49 0.76 5.31 1.62 8.56 2.61 9.97 3.04 11.09 3.38 6.86 2.09 11.61 3.54 11.89 39.01 13.25 4.04 21.92 6.68 17.62 5.37 12.73 3.88 13.91 4.24 15.26 4.65 MRW m 4.13 2.71 2.43 2.43 6.58 6.58 1.24 1.42 2.26 3.25 3.68 4.01 2.71 4.13 12.45 4.65 7.29 5.93 4.54 4.96 5.20 ft 13.55 8.89 7.97 7.97 21.59 21.59 4.07 4.66 7.41 10.66 12.07 13.16 8.89 13.55 40.85 15.26 23.92 19.46 14.89 16.27 17.06 A/C JACKED FDL = 4.60 m (15.09 ft) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_020300_1_0280102_01_00 Ground Clearances Ground Clearances with Sharklets (Sheet 2 of 2) FIGURE-2-3-0-991-028-A01 2-3-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING F1 F N G C2 D2 H L J Q NOTE: FOR DIMENSIONS, SEE SHEET 2. PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL. E F2 D1 B F3 C1 A P K1 K2 **ON A/C A319neo N_AC_020300_1_0310101_01_00 Ground Clearances (Sheet 1 of 2) FIGURE-2-3-0-991-031-A01 2-3-0 Page 6 May 01/14 A B C1 C2 D1 D2 E (CFM LEAP−1A) E (PW 1100G) F F1 F2 F3 G H J K1 K2 L N P Q A/C CONFIGURATION CG 28% m ft 3.47 11.38 2.09 6.86 6.00 1.83 6.36 1.94 19.59 5.97 19.98 6.09 1.84 0.56 1.84 0.56 5.68 1.73 8.96 2.73 10.37 3.16 11.48 3.50 7.28 2.22 3.71 12.17 12.11 39.73 13.68 4.17 6.81 22.34 18.31 5.58 13.02 3.97 13.98 4.26 15.98 4.87 40 000 kg (88 185 lb) FWD CG 21% m ft 11.09 3.38 6.53 1.99 1.73 5.68 1.84 6.04 19.29 5.88 19.65 5.99 0.46 1.51 0.46 1.51 5.35 1.63 8.63 2.63 10.04 3.06 3.41 11.19 6.96 2.12 3.61 11.84 12.01 39.40 13.39 4.08 22.05 6.72 17.98 5.48 12.73 3.88 13.65 4.16 15.68 4.78 AFT CG 36% m ft 11.25 3.43 2.03 6.66 5.77 1.76 5.94 1.81 19.36 5.90 19.52 5.95 0.47 1.54 0.47 1.54 5.31 1.62 8.56 2.61 9.97 3.04 11.09 3.38 6.86 2.09 11.61 3.54 11.89 39.01 13.25 4.04 21.92 6.68 17.62 5.37 12.73 3.88 13.91 4.24 15.26 4.65 MRW m 4.13 2.71 2.43 2.43 6.58 6.58 1.13 1.13 2.26 3.25 3.68 4.01 2.71 4.13 12.45 4.65 7.29 5.93 4.54 4.96 5.20 ft 13.55 8.89 7.97 7.97 21.59 21.59 3.71 3.71 7.41 10.66 12.07 13.16 8.89 13.55 40.85 15.26 23.92 19.46 14.89 16.27 17.06 A/C JACKED FDL = 4.60 m (15.09 ft) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo N_AC_020300_1_0310102_01_00 Ground Clearances (Sheet 2 of 2) FIGURE-2-3-0-991-031-A01 2-3-0 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo E A B G C F D HEIGHT FROM GROUND A/C IN MAINTENANCE CONFIGURATION MID CG MAXIMUM RAMP WEIGHT FWD CG MAXIMUM RAMP WEIGHT AFT CG m ft m ft m ft A 2.07 6.79 1.94 6.36 1.93 6.33 B 2.79 9.15 2.67 8.76 2.65 8.69 C 2.83 9.28 2.70 8.86 2.69 8.83 D 3.67 12.04 3.54 11.61 3.51 11.52 E 2.11 6.92 1.99 6.53 1.97 6.46 F 2.61 8.56 2.48 8.14 2.46 8.07 G 3.06 10.06 2.93 9.61 2.91 9.55 N_AC_020300_1_0110101_01_01 Ground Clearances Flaps and Flap Track Fairings When Flaps Fully Extended FIGURE-2-3-0-991-011-A01 2-3-0 Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo K J H HEIGHT FROM GROUND A/C IN MAINTENANCE CONFIGURATION MID CG MAXIMUM RAMP WEIGHT FWD CG MAXIMUM RAMP WEIGHT AFT CG m ft m ft m ft H 2.70 8.86 2.58 8.46 2.57 8.43 J 3.10 10.17 2.98 9.78 2.97 9.74 K 3.50 11.48 3.37 11.06 3.36 11.02 N_AC_020300_1_0120101_01_01 Ground Clearances Flap Track Fairings Up FIGURE-2-3-0-991-012-A01 2-3-0 Page 9 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo L M HEIGHT FROM GROUND A/C IN MAINTENANCE CONFIGURATION MID CG MAXIMUM RAMP WEIGHT FWD CG MAXIMUM RAMP WEIGHT AFT CG m ft m ft m ft L 4.20 13.78 4.06 13.32 4.04 13.25 M 3.86 12.66 3.73 12.24 3.71 12.17 N_AC_020300_1_0130101_01_01 Ground Clearances Aileron Down FIGURE-2-3-0-991-013-A01 2-3-0 Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N P Q R S T U V W HEIGHT FROM GROUND A/C IN MAINTENANCE CONFIGURATION MID CG MAXIMUM RAMP WEIGHT FWD CG MAXIMUM RAMP WEIGHT AFT CG m ft m ft m ft N 4.58 15.03 4.44 14.57 4.42 14.50 P 4.38 14.37 4.25 13.94 4.23 13.88 Q 4.62 15.16 4.49 14.73 4.47 14.67 R 4.49 14.73 4.37 14.34 4.35 14.27 S 4.37 14.34 4.24 13.91 4.23 13.88 T 4.23 13.88 4.11 13.48 4.10 13.10 U 4.09 13.42 3.97 13.02 3.96 12.99 V 4.02 13.19 3.91 12.83 3.90 12.80 W 3.77 12.37 3.65 11.98 3.64 11.94 N_AC_020300_1_0140101_01_01 Ground Clearances Aileron Up and Spoilers 1 to 5 Extended (Sheet 1 of 2) FIGURE-2-3-0-991-014-A01 2-3-0 Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo Y X Z B’ A’ C’ D’ E’ F’ G’ HEIGHT FROM GROUND A/C IN MAINTENANCE CONFIGURATION MID CG MAXIMUM RAMP WEIGHT FWD CG MAXIMUM RAMP WEIGHT AFT CG m ft m ft m ft X 2.57 8.43 2.47 8.10 2.49 8.17 Y 2.98 9.78 2.88 9.45 2.89 9.48 Z 3.07 10.07 2.97 9.74 2.97 9.74 3.37 11.06 3.26 10.70 3.26 10.70 3.63 11.91 3.51 11.52 3.51 11.52 3.88 12.73 3.76 12.34 3.75 12.30 4.12 13.52 3.99 13.09 3.97 13.02 A’ B’ C’ D’ E’ F’ G’ N_AC_020300_1_0150101_01_01 Ground Clearances Slats Extended (Sheet 1 of 2) FIGURE-2-3-0-991-015-A01 2-3-0 Page 12 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-4-1 Interior Arrangements - Plan View **ON A/C A319-100 A319neo Interior Arrangements - Plan View 1. This section gives the typical interior configuration. 2-4-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING L G FWD PASSENGER /CREW DOOR 156 SEATS ALL TOURIST CLASS 28/30 in PITCH. 6 ABREAST. 3.3 ITEM G L A EMERGENCY EXIT DESIGNATION (2) GALLEY (2) LAVATORY ATTENDANT SEAT (5) AFT PASSENGER /CREW DOOR FWD PASSENGER /CREW DOOR L A A A G A A EMERGENCY EXIT AFT PASSENGER /CREW DOOR **ON A/C A319-100 A319neo N_AC_020401_1_0020101_01_02 Interior Arrangements - Plan View Typical Configuration - Single-Class, High Density FIGURE-2-4-1-991-002-A01 2-4-1 Page 2 May 01/14 ITEM G L A FWD PASSENGER /CREW DOOR L A A G FWD PASSENGER /CREW DOOR DESIGNATION (2) GALLEY (3) LAVATORY ATTENDANT SEAT (3) 2-4-1 SEAT PITCHES: FIRST 36 in ECONOMY 32 in 8 SUPER FIRST CLASS 116 ECONOMY CLASS PASSENGER SEATS (124 TOTAL) EMERGENCY EXIT EMERGENCY EXIT L G AFT PASSENGER /CREW DOOR L A AFT PASSENGER /CREW DOOR @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_020401_1_0080101_01_00 Interior Arrangements - Plan View Typical Configuration - Two-Class FIGURE-2-4-1-991-008-A01 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-5-0 Interior Arrangements - Cross Section **ON A/C A319-100 A319neo Interior Arrangements - Cross Section 1. This section gives the typical configuration. 2-5-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 3.95 (155.51) 1.60 (62.99) 2.13 (83.86) Wind ows 0.52 (20.47) Aircraft Datum 0.49 (19.29) CABIN FLOOR Top of cargo Compartment 2.64 (103.94) 1.24 (48.82) Cargo Compartment Floor 1.42 (55.91) 3.45 (135.83) 3.68 (144.88) NOTE: DIMENSIONS m (in) N_AC_020500_1_0010101_01_01 Interior Arrangements - Cross Section Typical Configuration FIGURE-2-5-0-991-001-A01 2-5-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 2.21 (87) 6 ABREAST−WIDER AISLE 1.24 (48.9) 4.14 (163) 0.432 (17) 1.50 (59) 0.64 (25) 1.50 (59) 3.64 (143) 3.95 (155.5) NOTE: DIMENSIONS m (in) N_AC_020500_1_0050101_01_00 Interior Arrangements - Cross Section Economy Class, 6 Abreast - Wider Aisle (Sheet 1 of 2) FIGURE-2-5-0-991-005-A01 2-5-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 2.21 (87) 6 ABREAST−WIDER SEAT 1.24 (48.9) 4.14 (163) 0.457 (18) 1.58 (62) 0.48 (19) 1.58 (62) 3.64 (143) 3.95 (155.5) NOTE: DIMENSIONS m (in) N_AC_020500_1_0050102_01_02 Interior Arrangements - Cross Section Economy Class, 6 Abreast - Wider Seat (Sheet 2 of 2) FIGURE-2-5-0-991-005-A01 2-5-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 2.21 (87) 4 ABREAST−FIRST CLASS 1.24 (48.9) 4.14 (163) 0.57 (22.6) 1.45 (57) 0.69 (27) 1.45 (57) 3.59 (141) 3.95 (155.5) NOTE: DIMENSIONS m (in) N_AC_020500_1_0060101_01_00 Interior Arrangements - Cross Section First-Class FIGURE-2-5-0-991-006-A01 2-5-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-6-0 Cargo Compartments **ON A/C A319-100 A319neo Cargo Compartments 1. This section gives the cargo compartments locations, dimensions and loading combinations. 2-6-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 1.81 m (71.26 in) 3.35 m (131.89 in) 7.67 m (301.97 in) 1.81 m (71.26 in) BULK CARGO COMPARTMENT AFT CARGO COMPARTMENT (2 CONTAINERS) FWD CARGO COMPARTMENT (2 CONTAINERS) FR24A FR34 FR47 / FR51 FR59 FR65 **ON A/C A319-100 A319neo N_AC_020600_1_0020101_01_00 Cargo Compartments Locations, Dimensions and Loading Combinations FIGURE-2-6-0-991-002-A01 2-6-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-0 Door Clearances and Location **ON A/C A319-100 A319neo Door Clearances 1. This section provides door identification and location. NOTE : Dimensions of the ground clearances are approximate and will vary with tire type, weight and balance and other special conditions. 2-7-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo OVERWING FWD EMERGENCY PASSENGER/CREW EXIT DOOR (LH) DOOR (LH) (OPTIONAL) OVERWING EMERGENCY AFT PASSENGER/CREW EXIT DOOR (LH) DOOR (LH) OVERWING FWD EMERGENCY EXIT DOOR (RH) PASSENGER/CREW AFT PASSENGER/CREW OVERWING EMERGENCY DOOR (RH) EXIT DOOR (RH) DOOR (RH) (OPTIONAL) AFT CARGO COMPARTMENT FWD CARGO COMPARTMENT DOOR DOOR N_AC_020700_1_0020101_01_00 Door Identification and Location Door Identification (Sheet 1 of 2) FIGURE-2-7-0-991-002-A01 2-7-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 25.81 m (84.68 ft) 13.68 m (44.88 ft) 12.83 m (42.09 ft) 5.04 m (16.54 ft) 8.16 m (26.77 ft) 20.56 m (67.45 ft) N_AC_020700_1_0020102_01_00 Door Identification and Location Door Location (Sheet 2 of 2) FIGURE-2-7-0-991-002-A01 2-7-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-1 Forward Passenger / Crew Doors **ON A/C A319-100 A319neo Forward Passenger / Crew Doors 1. This section gives forward passenger / crew doors clearances. 2-7-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 1.8 m (5 ft 10.8 in) 0.48 m (1 ft 6.88 in) 0.81 m (2 ft 7.8 in) 0.61 m (2 ft) 2.54 m (8 ft 3.99 in) CRITICAL CLEARANCE LIMIT 5.02 m (16 ft 5.62 in) 2.375 m (7 ft 9.48 in) 1.85 m (6 ft 0.82 in) 0.03 m (1.18 in) SEE CHAPTER 2−3 N_AC_020701_1_0020101_01_00 Doors Clearances Forward Passenger / Crew Doors FIGURE-2-7-1-991-002-A01 2-7-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-2 Emergency Exits **ON A/C A319-100 A319neo Emergency Exits 1. This section gives emergency exits doors clearances. 2-7-2 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo CL OPTIONAL FWD (FROM NOSE) 12.83 m (42 ft 1.11 in) 0.5 m (1ft 7.68 in) 0.85 m (2 ft 9.45 in) B A 0.47 m (1ft 6.49 in) SEE SECTION 2−3 0.2 m (7.87 in) B A 1.23 m (4 ft 0.42 in) 0.9 m (2 ft 11.4 in) 0.12 m (4.72 in) 0.495 m (1ft 7.48 in) (TOP OF FLOOR) B B A A (FRAME 47) NOTE: ESCAPE SLIDE COMPARTMENT DOOR OPENS ON WING UPPER SURFACE. N_AC_020702_1_0030101_01_00 Doors Clearances Emergency Exits FIGURE-2-7-2-991-003-A01 2-7-2 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-3 Aft Passenger / Crew Doors **ON A/C A319-100 A319neo Aft Passenger / Crew Doors 1. This section gives Aft passenger / crew doors clearances. 2-7-3 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 1.79 m (5 ft 10.46 in) 0.81 m (2 ft 7.88 in) FWD A CRITICAL CLEARANCE LIMIT 0.58 m (1 ft 10.8 in) A 2.44 m (8 ft) (FROM NOSE) 25.91 m (85 ft) 1.85 m (6 ft 0.82 in) 0.03 m (1.18 in) SEE CHAPTER 2−3 0.6 m (1 ft 11.6 in) A A N_AC_020703_1_0020101_01_00 Doors Clearances Aft Passenger / Crew Doors FIGURE-2-7-3-991-002-A01 2-7-3 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-4 Forward Cargo Compartment Door **ON A/C A319-100 A319neo Forward Cargo Compartment Door 1. This section gives forward cargo compartment door clearances. 2-7-4 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A 8.160 m (FROM NOSE) (26.772 ft) 1.240 m (4.068 ft) 1.495 m (4.905 ft) FWD SEE CHAPTER 2−3 3.945 m (12.943 ft) A 1.820 m (5.971 ft) A A 2.710 m (8.891 ft) 0.500 m (1.640 ft) N_AC_020704_1_0020101_01_01 Door Clearances Forward Cargo Compartment Door FIGURE-2-7-4-991-002-A01 2-7-4 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo A 8.160 m (FROM NOSE) (26.772 ft) 1.240 m (4.068 ft) 1.495 m (4.905 ft) FWD SEE CHAPTER 2−3 3.945 m (12.943 ft) A 1.820 m (5.971 ft) A A CFM ENGINE = 2.470 m (8.104 ft) PW ENGINE = 2.430 m (7.972 ft) CFM ENGINE = 0.450 m (1.476 ft) PW ENGINE = 0.453 m (1.486 ft) N_AC_020704_1_0050101_01_00 Door Clearances Forward Cargo Compartment Door FIGURE-2-7-4-991-005-A01 2-7-4 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-5 Aft Cargo Compartment Door **ON A/C A319-100 A319neo Aft Cargo Compartment Door 1. This section gives Aft cargo compartment door clearances. 2-7-5 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A 20.58 m (FROM NOSE) (67ft 6.22 in) 1.43 m (4 ft 8.29 in) FWD 1.23 m (4 ft 0.42 in) A SEE CHAPTER 2−3 3.945 m 1.82 m (5 ft 11.65 in) (12 ft 11.3 in) A A FWD 1.6 m 5 ft 2.93 in) N_AC_020705_1_0020101_01_01 Doors Clearances Aft Cargo Compartment Door FIGURE-2-7-5-991-002-A01 2-7-5 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-7 Main Landing Gear Doors **ON A/C A319-100 A319neo Main Landing Gear Doors 1. This section gives the main landing gear doors clearances. 2-7-7 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A 1.826 m (5 ft 11.88 in) 14.758 m (48 ft 5 in) NOTE: VALUE OF CG: 25% RC. AIRCRAFT 1.942 m 0.485 m (6 ft 4.45 in) (1 ft 7.09 in) 0.207 m (8.14 in) 84° (5 1.7 6 ft 9 1 m .32 in) 0.14 m (5.51 in) 1.23 m (4 ft 0.42 in) GROUND LINE A N_AC_020707_1_0020101_01_02 Doors Clearances Main Landing Gear Doors FIGURE-2-7-7-991-002-A01 2-7-7 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-8 Radome **ON A/C A319-100 A319neo Radome 1. This section gives the radome clearances. 2-7-8 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 0.63 m (2 ft 0.79 in) STA 3500 FR1 1.54 m (5 ft 0.62 in) 65° N_AC_020708_1_0020101_01_00 Doors Clearances Radome FIGURE-2-7-8-991-002-A01 2-7-8 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-7-9 APU and Nose Landing Gear Doors **ON A/C A319-100 A319neo APU and Nose Landing Gear Doors 1. This section gives APU and Nose Landing Gear doors clearances. 2-7-9 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo NOTE: VALUE OF CG : 25% RC. FR80 3.86 m (12 ft 7.96 in) 1.4 m (4 ft 7.11 in) 1.5 m (4 ft 11 in) 3.23 m (10 ft 7.16 in) FR84 N_AC_020709_1_0020101_01_00 Doors Clearances APU and Nose Landing Gear Doors FIGURE-2-7-9-991-002-A01 2-7-9 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-8-0 Escape Slides **ON A/C A319-100 A319neo Escape Slides 1. General This section gives location of cabin escape facilities and related clearances. 2. Location Escape facilities are provided at the following locations: - one slide-raft at each passenger/crew door (total four) - one slide for each emergency exit door (total two). Dual lane offwing escape slides are installed above the wings in the left and right wing-to-fuselage fairings for off-the-wing evacuation. 2-8-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo AFT CABIN ESCAPE SLIDE OFF WING ESCAPE SLIDE FWD CABIN ESCAPE SLIDE N_AC_020800_1_0030101_01_00 Escape Slides Location FIGURE-2-8-0-991-003-A01 2-8-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo EMERGENCY DESCENT DEVICE THROUGH WINDOW OPENING GRID EQUALS 1 m (3.28 ft) IN REALITY N_AC_020800_1_0040101_01_00 Escape Slides Dimensions FIGURE-2-8-0-991-004-A01 2-8-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-9-0 Landing Gear **ON A/C A319-100 A319neo Landing Gear 1. General The landing gear is of the conventional retractable tricycle type comprising: - Two main gears with twin-wheel, - A twin-wheel nose gear. The main landing gears are located under the wing and retract sideways towards the fuselage centerline. The nose landing gear retracts forward into a fuselage compartment located between FR9 and FR20. The landing gears and landing gear doors are operated and controlled electrically and hydraulically. In abnormal operation, the landing gear can be extended by gravity. For landing gear footprint and tire size, refer to 07-02-00. 2. Main Landing Gear A. Twin-Wheel Each of the two main landing gear assemblies consists of a conventional two-wheel direct type with an integral shock absorber supported in the fore and aft directions by a fixed drag strut and laterally by a folding strut mechanically locked when in the DOWN position. 3. Nose Landing Gear The nose landing gear consists of a leg with a built-in shock absorber strut, carrying twin wheels with adequate shimmy damping and a folding strut mechanically locked when in the DOWN position. 4. Nose Wheel Steering Steering is controlled by two hand wheels in the cockpit. For steering angle controlled by the hand wheels, refer to AMM 32-51-00. For steering angle limitation, refer to AMM 09-10-00. A steering disconnection box is installed on the nose landing gear to allow steering deactivation for towing purposes. 5. Landing Gear Servicing Points A. General Filling of the landing-gear shock absorbers is done through MIL-PRF-6164 standard valves. 2-9-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING Charging of the landing-gear shock absorbers is accomplished with nitrogen through MILPRF-6164 standard valves. B. Charging Pressure For charging of the landing-gear shock absorbers, refer to AMM 12-14-32. 6. Braking A. General The four main wheels are equipped with carbon multidisc brakes. The braking system is electrically controlled and hydraulically operated. The braking system has four braking modes plus autobrake and anti-skid systems: - Normal braking with anti-skid capability, - Alternative braking with anti-skid capability, - Alternative braking without anti-skid capability, - Parking brake with full pressure application capability only. B. In-Flight Wheel Braking The main gear wheels are braked automatically before the wheels enter the wheel bay. The nose gear wheels are stopped by the wheels contacting a rubbing strip (the brake band) when the gear is in the retracted position. 2-9-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo HINGED FAIRING (MECHANICALLY OPERATED) HINGED FAIRING FIXED FAIRING DOOR ACTUATING CYLINDER B A C ADJUSTABLE RAMP STEPS UPLOCK ROLLER PROXIMITY SENSORS ACTUATING CYLINDER FIXED RAMPS MAIN DOOR (HYDRAULICALLY OPERATED) LOCK STAY E UNLOCK ACTUATOR MAIN FITTING SIDE STAY SHOCK ABSORBER TORQUE LINK D A NOTE: MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION. N_AC_020900_1_0060101_01_00 Landing Gear Main Landing Gear - Twin-Wheel (Sheet 1 of 2) FIGURE-2-9-0-991-006-A01 2-9-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo LOCKSTAY ACTUATING CYLINDER LOCKING PIN GROUND LOCK SLEEVE DOOR ACTUATING CYLINDER LOCKING PIN FLAG FLAG B C BOTTOM FILLING AND CHARGING CONNECTION TOP FILLING AND CHARGING CONNECTION E D EXAMPLE N_AC_020900_1_0060102_01_01 Landing Gear Main Landing Gear - Twin-Wheel (Sheet 2 of 2) FIGURE-2-9-0-991-006-A01 2-9-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 2 265 mm (89.17 in) 2 868.70 mm (112.94 in) Y= COMPRESSED 3 795 mm (149.41 in) EXTENDED 20 252.50 mm X= (797.34 in) 58.40 % AMC 469.90 mm (18.50 in) 3 453 mm (135.94 in) 80°30 RETRACTION ANGLE 927.10 mm (36.50 in) N_AC_020900_1_0070101_01_00 Landing Gear Main Landing Gear Dimensions - Twin-Wheel FIGURE-2-9-0-991-007-A01 2-9-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo BELL CRANK DOOR ACTUATING CYLINDER DOOR UPLOCK ASSEMBLY FR9 DRAG STRUT ASSEMBLY GEAR UPLOCK ASSEMBLY FR20 CONTROL ROD C B ROTATING ROD ASSEMBLY FITTING AFT DOORS FWD DOORS LEG DOOR A ACTUATING CYLINDER D DOWNLOCK PROXIMITY DETECTORS NOSE WHEEL STEERING SERVO CONTROL STEERING ACTUATING CYLINDER E SHOCK ABSORBER TORQUE LINK TOWING FITTING A N_AC_020900_1_0080101_01_00 Landing Gear Nose Landing Gear (Sheet 1 of 2) FIGURE-2-9-0-991-008-A01 2-9-0 Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo LOCKSTAY NLG DOOR SAFETY PIN DOWNLOCK SAFETY PIN DOOR HINGE NLG DOOR FLAG FLAG B C RH SHOWN LH SYMMETRICAL TOWING LEVER FILLING AND CHARGING CONNECTION NORMAL POSITION (NOSE WHEEL STEERING OPERATIONAL) TOWING POSITION (NOSE WHEEL STEERING DEACTIVATED) D E SAFETY PIN (TOWING POSITION) N_AC_020900_1_0080102_01_01 Landing Gear Nose Landing Gear (Sheet 2 of 2) FIGURE-2-9-0-991-008-A01 2-9-0 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 92° 1 957.03 mm (77.05 in) 2 338 mm (92.05 in) COMPRE SSED EXTEND ED 430 mm (16.93 in) 9° X= 7 561 mm (297.68 in) 500 mm (19.69 in) N_AC_020900_1_0090101_01_00 Landing Gear Nose Landing Gear Dimensions FIGURE-2-9-0-991-009-A01 2-9-0 Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo Landing Gear Maintenance Pits 1. Description The minimum maintenance pit envelopes for the landing-gear shock absorber removal are shown in FIGURE 2-9-0-991-022-A and FIGURE 2-9-0-991-023-A. All dimensions shown are minimum dimensions with zero clearances. The dimensions for the pits have been determined as follows: - The length and width of the pits allow the gear to rotate as the weight is taken off the landing gear. - The depth of the pits allows the shock absorber to be removed when all the weight is taken off the landing gear. Dimensions for elevators and associated mechanisms must be added to those in FIGURE 2-9-0-991-022-Aand FIGURE 2-9-0-991-023-A. 2-9-0 Page 9 May 01/14 FROM X0 5.28 m (17.32 ft) 7.61 m (24.97 ft) FWD JACKING POINT 1.5 m (4.92 ft) = = 2.5 m (8.20 ft) 1m (3.28 ft) 18.65 m (61.19 ft) 18.5 m (60.70 ft) 3.76 m (12.34 ft) 2.95 m (9.68 ft) MAIN JACKING POINT 3.79 m (12.43 ft) 6.49 m (21.29 ft) = MAIN JACKING POINT 1.92 m (6.30 ft) = 7.59 m (24.90 ft) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_020900_1_0220101_01_00 Landing Gear Maintenance Pits Maintenance Pit Envelopes FIGURE-2-9-0-991-022-A01 2-9-0 Page 10 May 01/14 2-9-0 2 1.71 0.52 B 0.40 m (1.31 ft) 1.17 m 1.60 m (5.25 ft) 18.65 m (61.19 ft) 3.84 ft STATIC GROUND LINE 2 REPRESENTS TOP OF MECHANICAL OR HYDRAULIC ELEVATOR, SHOWN WITH ZERO CLEARANCE LOWERED FOR SHOCK ABSORBER REMOVAL. NOTE: 1 REPRESENTS TOP OF MECHANICAL OR HYDRAULIC ELEVATOR, WITH AIRCRAFT WEIGHT SUPPORTED AND LANDING GEAR SHOCK ABSORBERS EXTENDED. 1 7.61 m (24.97 ft) DIM QUOTED IS WITH WHEELS REMOVED AND 153 mm (6.02 in) CLEARANCE AT JACKING DOME ft A m 2 1 A B @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FROM X0 N_AC_020900_1_0230101_01_00 Landing Gear Maintenance Pits Maintenance Pit Envelopes FIGURE-2-9-0-991-023-A01 Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-10-0 Exterior Lighting **ON A/C A319-100 A319neo Exterior Lighting 1. General This section gives the location of the aircraft exterior lighting. ITEM 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 EXTERIOR LIGHTING DESCRIPTION RIGHT NAVIGATION LIGHT (GREEN) TAIL NAVIGATION LIGHT (WHITE) LEFT NAVIGATION LIGHT (RED) RETRACTABLE LANDING LIGHT RUNWAY TURN OFF LIGHT TAXI LIGHT TAKE-OFF LIGHT LOGO LIGHT UPPER ANTI-COLLISION LIGHT/BEACON (RED) LOWER ANTI-COLLISION LIGHT/BEACON (RED) WING STROBE LIGHT (HIGH INTENSITY, WHITE) TAIL STROBE LIGHT (HIGH INTENSITY, WHITE) WING/ENGINE SCAN LIGHT WHEEL WELL LIGHT (DOME) CARGO COMPARTMENT FLOOD LIGHT 2-10-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 2 8 12 9 8 11 1 RH 3 LH 10 13 11 RH 1 LH 3 6 5 7 4 N_AC_021000_1_0050101_01_00 Exterior Lighting FIGURE-2-10-0-991-005-A01 2-10-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 2 1 3 5 5 7 N_AC_021000_1_0060101_01_00 Exterior Lighting FIGURE-2-10-0-991-006-A01 2-10-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 12 9 10 11 11 13 13 4 6 N_AC_021000_1_0070101_01_00 Exterior Lighting FIGURE-2-10-0-991-007-A01 2-10-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 8 8 15 15 14 EXAMPLE FOR LIGHT N° 15 CEILING LIGHT SPOT LIGHT GROUND N_AC_021000_1_0180101_01_00 Exterior Lighting FIGURE-2-10-0-991-018-A01 2-10-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-11-0 Antennas and Probes Location **ON A/C A319-100 A319neo Antennas and Probes Location 1. This section gives the location of antennas and probes. 2-11-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo WEATHER RADAR EMERGENCY STATIC PROBE AOA SENSOR(3) STBY VHF(1) GPS(2) ATC(4) VHF(3) HF AOA SENSOR(1) GPS(1) ELT TCAS TOP LOC GLIDE RADIO ALTIMETER(2) DME(1) TAT PROBE RADIO ALTIMETER(1) TCAS BOTTOM PITOT PROBE(3) VHF(2) MARKER PITOT PROBE(1) DME(2) ATC(1) STATIC PROBE(1) STATIC PROBE(2) VOR EMERGENCY STATIC PROBE ATC(3) ADF(1) AOA SENSOR(2) TAT PROBE PITOT PROBE(2) ATC(2) STATIC PROBE(1) STATIC PROBE(2) NOTE: DEPENDING ON AIRCRAFT CONFIGURATION N_AC_021100_1_0020101_01_00 Antennas and Probes Location FIGURE-2-11-0-991-002-A01 2-11-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-12-0 Power Plant **ON A/C A319-100 Auxiliary Power Unit 1. General The APU is installed at the rear part of the fuselage in the tail cone. An air intake system with a flap-type door is installed in front of the APU compartment. The exhaust gases pass overboard at the end of the fuselage cone. 2. Controls and Indication The primary APU controls and indications are installed on the overhead panel, on the center pedestal and on the center instrument panel. Additionally, an external APU panel is installed on the nose landing gear to initiate an APU emergency shutdown. 2-12-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 Z310 A UPPER FIREWALL FRONT FIREWALL STA33561 / FR80 FIREWALL RH LOUVER LH CUT OUT SEALED WITH LABYRINTH GASKET B REAR FIREWALL CUT OUT SEALED WITH LABYRINTH GASKET RH ACCESS DOOR 316AR AIR INTAKE FIXED ON ACCESS DOOR STA35211 / FR84 A NOTE: LH ACCESS DOOR 315AL NOT SHOWN FOR CLARITY N_AC_021200_1_0030101_01_00 Auxiliary Power Unit Access Doors FIGURE-2-12-0-991-003-A01 2-12-0 Page 2 May 01/14 FRONT FIRE WALL BLEED AIR LINE DIVERTER 2-12-0 B OIL COOLER OUTLET STA35211/FR84 APU−FUEL−LINE AIR INTAKE HOUSING STA36379 / FR87 EXHAUST MUFFLER APU SUSPENSION (7 RODS) AIR INTAKE DUCT STA33561 /FR80 STA32923 / FR78 APU STA32811 /FR77 APU SUSPENSION (7 RODS) GENERATOR FIRE EXTINGUISHING BOTTLE FIRE OVERHEAT DETECTOR @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_021200_1_0040101_01_00 Auxiliary Power Unit General Layout FIGURE-2-12-0-991-004-A01 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo Engine and Nacelle **ON A/C A319-100 1. Engine and Nacelle - CFM Engine A. Engine The engine is a dual-rotor, variable stator, high bypass ratio turbo fan power plant for subsonic services. The principal modules of the engine are: - low pressure compressor (fan stator and fan rotor) - high pressure compressor - turbine frame - combustion chamber - high pressure turbine - low pressure turbine - accessory drives (gear box). The 9 stage high pressure compressor is driven by 1 stage high pressure turbine, and the integrated front fan and booster is driven by 4 stage low pressure turbine. An annular combustor converts fuel and compressor discharge air into energy to provide engine thrust part through primary exhaust and to drive the turbines. The accessory drive system extracts energy from the high pressure rotor to drive the engine accessories and the engine mounted aircraft accessories. Reverse thrust for braking the aircraft after landing is supplied by an integrated system which acts on the fan discharge airflow. B. Nacelle The cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine is housed in a nacelle suspended from a pylon attached to the wing lower surface. The nacelle consists of the demountable powerplant, the fan cowls and the thrust reverser cowls. The nacelle installation is designed to provide cooling and ventilation air for engine accessories mounted along the fan and core casing. The nacelle provides: - protection for the engine and the accessories - airflow around the engine during its operation - lighting protection - HIRF and EMI attenuation. 2. Engine and Nacelle - IAE Engine A. Engine The engine is a two spool, axial flow, high bypass ratio turbofan powerplant for subsonic sevice. The main modules of the engine are: 2-12-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING - low pressure compressor (fan and booster) assembly LP compressor/intermediate case No. 4 bearing and combustion section high pressure compressor HP turbine section LP turbine section accessory drives (gear box). The four stage Low Pressure Compressor (LPC) is driven by a five stage Low Pressure Turbine (LPT) and the ten stage High Pressure Compressor (HPC) by a two stage High Pressure Turbine (HPT). The HPT also drives a gearbox which, in turn drives the engines and aircraft mounted accessories. The two shafts are supported by five main bearings. The V2500 incorporates a Full Authority Digital Engine Control (FADEC) which governs all engine functions, including power management. Reverse thrust for braking the aircraft after landing is supplied by an integrated system which acts on the fan discharge airflow. B. Nacelle The cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine is housed in a nacelle suspended from a pylon attached below the wing. The nacelle installation is designed to provide cooling and ventilation air for engine accessories mounted along the fan and core casing. The nacelle provides: - protection for the engine and the accessories - airflow around the engine during its operation - lighting protection - HIRF and EMI attenuation. 2-12-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A 1 125 mm (44.28 in) FAN AND BOOSTER FWD HANDLING POINT FWD HOISTING POINT 2 943 mm (115.87 in) 2 600 mm (102.36 in) COMPRESSOR COMBUSTOR TURBINE FRAME DIA 986 mm (38.82 in) B 1 820 mm (71.65 in) AGB TGB HP TURBINE LP TURBINE AFT HOISTING AND ACCESSORY HANDLING POINT DRIVE A 2 145 mm (84.45 in) 1 130 mm (44.49 in) 989 mm (38.94 in) 1 978 mm (77.87 in) B N_AC_021200_1_0190101_01_00 Power Plant Handling Major Dimensions - CFM56 Series Engine FIGURE-2-12-0-991-019-A01 2-12-0 Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 DISTANCE FROM THE NOSE 9.6 m (31.5 m) 0.93 m (3.1 ft) A 1.3 m (4.3 ft) B 1.2 m (3.9 ft) 0.33 m (1.1 ft) 1.2 m (3.9 ft) D C PRIMARY NOZZLE 6° 2.3 m (7.5 ft) 1.6 m (5.2 ft) CENTERBODY A ENGINE AIR INLET COWL 0.57 m (1.9 ft) B FAN COWL 2.1 m (6.9 ft) C FAN D REVERSER A A BLOCKER DOOR EXTENDED 2.07 m (6.8 ft) 1.9 m (6.2 ft) 1.8 m (5.9 ft) 1.2 m (3.9 ft) B B C C D D N_AC_021200_1_0200101_01_00 Power Plant Handling Major Dimensions - CFM56 Series Engine FIGURE-2-12-0-991-020-A01 2-12-0 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A B C 0.55 m (1.8 ft) m (ft) A B C VIEW COWLING AFT 42°27 1.8 (5.9) 1.5 (4.9) 1.3 (4.3) 55°15 2.0 (6.6) 1.8 (5.9) 1.7 (5.6) VIEW COWLING FWD 40°40 1.8 (5.9) 1.4 (4.6) 1.3 (4.3) 52°56 2.0 (6.6) 1.7 (5.6) 1.6 (5.2) NOTE: APPROXIMATE DIMENSIONS N_AC_021200_1_0210101_01_00 Power Plant Handling Fan Cowls - CFM56 Series Engine FIGURE-2-12-0-991-021-A01 2-12-0 Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 3.7 m (12.1 ft) 3.3 m (10.8 ft) 1m (3.3 ft) 0.9 m (3 ft) 35° 45° 0.5 m (1.6 ft) 1m (3.3 ft) 0.7 m (2.3 ft) GROUND NOTE: APPROXIMATE DIMENSIONS CAUTION DO NOT ACTUATE SLATS: − WITH THRUST REVERSER COWLS 45° OPEN POSITION − WITH BLOCKER DOORS OPEN AND THRUST REVERSER COWLS AT 35° AND 45° OPEN POSITION N_AC_021200_1_0220101_01_00 Power Plant Handling Thrust Reverser Cowls - CFM56 Series Engine FIGURE-2-12-0-991-022-A01 2-12-0 Page 9 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A 3 101 mm (122.1 in) FAN AND BOOSTER HP LP TURBINE TURBINE TURBINE FRAME COMPRESSOR COMBUSTOR 1 715 mm (67.5 in) 1 067 mm (42.0 in) ACCESSORY DRIVE A FWD N_AC_021200_1_0230101_01_00 Power Plant Handling Major Dimensions - IAE V2500 Series Engine FIGURE-2-12-0-991-023-A01 2-12-0 Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 DISTANCE FROM THE NOSE 9.52 m (31.23 ft) 5.25 m (17.23 ft) D A C F B W E 0.5° 6° U V 1.50 m (4.95 ft) A E B F C D 5.26 m (17.27 ft) W U V PPS AT COMPONENT m ft m ft m ft m ft A−A 2.01 6.58 0.99 3.25 1.10 3.63 1.41 4.62 INLET ATTACH FLG B−B 2.01 6.58 1.00 3.29 1.11 3.64 2.59 8.50 TORQUE BOX "V" BLADE C−C 1.98 6.50 0.97 3.19 1.07 3.52 3.26 10.70 COMB. CHAMBER ENTRY FLG D−D 1.93 6.32 0.93 3.06 1.03 3.39 3.63 11.90 COMB. CHAMBER EXIT FLG E−E 1.64 5.38 0.78 2.57 0.86 2.83 4.60 15.10 TEC FLG TURB. EXIT CASE F−F 1.24 4.07 0.60 1.96 0.64 2.11 −−−− −−−− AFT END CNA NOTE: ALL SIZES GIVEN ON THIS ILLUSTRATION ARE APPROXIMATE N_AC_021200_1_0240101_01_00 Power Plant Handling Major Dimensions - IAE V2500 Series Engine FIGURE-2-12-0-991-024-A01 2-12-0 Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 FWD VIEW 2m (6.6 ft) WL100 CLOSED 3.9 m (12.8 ft) WL100 FAN COWL OPEN 50° 1.6 m (5.2 ft) 1.2 m (3.9 ft) 0.67 m (2.2 ft) GROUND NOTE: APPROXIMATE DIMENSIONS N_AC_021200_1_0250101_01_00 Power Plant Handling Fan Cowls - IAE V2500 Series Engine FIGURE-2-12-0-991-025-A01 2-12-0 Page 12 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 AFT VIEW 2m (6.6 ft) WL100 CLOSED 3.6 m (11.8 ft) WL100 THRUST REVERSER OPEN 45° 0.9 m (3 ft) 1.1 m (3.6 ft) 1m (3.3 ft) 0.67 m (2.2 ft) NOTE: APPROXIMATE DIMENSIONS N_AC_021200_1_0260101_01_00 Power Plant Handling Thrust Reverser Halves - IAE V2500 Series Engine FIGURE-2-12-0-991-026-A01 2-12-0 Page 13 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo FAN COWL THRUST REVERSER NOSE COWL PRIMARY NOZZLE A PLUG 0.46 m (1.51 ft) 0.66 m (2.17 ft) 1.46 m (4.79 ft) 1.53 m (5.02 ft) 1.44 m (4.72 ft) FWD 2.60 m (8.53 ft) 2.67 m (8.76 ft) 0.46 m (1.51 ft) A N_AC_021200_1_0430101_01_00 Power Plant Handling Major Dimensions - PW 1100G Engine FIGURE-2-12-0-991-043-A01 2-12-0 Page 14 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo A A 4.70 m (15.42 ft) 1 OPEN POSITION: FULL: 50° 1 1.22 m (4.00 ft) 50° 1: FAN COWL 0.46 m (1.51 ft) A N_AC_021200_1_0440101_01_00 Power Plant Handling Fan Cowls - PW 1100G Engine FIGURE-2-12-0-991-044-A01 2-12-0 Page 15 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo A A A A 1 1 1 1 B B 45° 43° 1 : THRUST REVERSER C C A OPEN POSITION A 43° 45° B MIN. MAX. 4.26 m (13.98 ft) 0.80 m (2.62 ft) 0.90 m (2.95 ft) 4.33 m (14.21 ft) 0.84 m (2.76 ft) 0.95 m (3.12 ft) C SEE AC SECTION 2−3−0 NOTE: B AND C DEPENDING ON AIRCRAFT CONFIGURATION. N_AC_021200_1_0450101_01_00 Power Plant Handling Thrust Reverser Halves - PW 1100G Engine FIGURE-2-12-0-991-045-A01 2-12-0 Page 16 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-13-0 Leveling, Symmetry and Alignment **ON A/C A319-100 A319neo Leveling, Symmetry and Alignment 1. Quick Leveling There are three alternative procedures to level the aircraft: - Quick leveling procedure with Air Data/Inertial Reference Unit (ADIRU). - Quick leveling procedure with a spirit level in the passenger compartment. - Quick leveling procedure with a spirit level in the FWD cargo compartment. 2. Precise Leveling For precise leveling, it is necessary to install sighting rods in the receptacles located under the fuselage (points 11 and 12 for longitudinal leveling) and under the wings (points 2LH and 2RH for lateral leveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until the reference marks on the sighting rods are aligned in the sighting plane (aircraft level). 3. Symmetry and Alignment Check Possible deformation of the aircraft is measured by photogrammetry. 2-13-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo RIB10 FR57 FR54 2LH 12 2RH 11 FR28 FR34 RIB10 N_AC_021300_1_0020101_01_00 Location of the Leveling Points FIGURE-2-13-0-991-002-A01 2-13-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 2-14-0 Jacking **ON A/C A319-100 A319neo Jacking for Maintenance 1. Aircraft Jacking Points for Maintenance A. General (1) The A319 can be jacked: - At not more than 57 000 kg (125 663 lb), - Within the limits of the permissible wind speed when the aircraft is not in a closed environment. B. Primary Jacking Points (1) The aircraft is provided with three primary jacking points: - One located under the forward fuselage (FR8), - Two located under the wings (one under each wing, located at the intersection of RIB9 and the datum of the rear spar). (2) Three jack adapters are used as intermediary parts between the aircraft and the jacks: - One male spherical jack adapter of 19 mm (0.75 in) radius, forming part of the aircraft structure (FR8), - Two wing jack pads (one attached to each wing at RIB9 with 2 bolts) for the location of the jack adaptor. Wing jack pads are ground equipment. C. Auxiliary Jacking Points (Safety Stay) (1) When the aircraft is on jacks, it is recommended that a safety stay be placed under the fuselage, between FR73 and FR74, to prevent tail tipping caused by accidental displacement of the center of gravity. (2) The safety stay must not be used to lift the aircraft. (3) A male spherical ball pad with a 19 mm (0.75 in) radius, forming part of the aircraft structure, is provided for using the safety stay. 2. Jacks and Safety Stay A. Jack Design (1) The maximum permitted loads given in the table in FIGURE 2-14-0-991-005-A are the maximum loads applicable on jack fittings. (2) In the fully retracted position (jack stroke at minimum), the height of the jack is such that the jack may be placed beneath the aircraft in the most adverse conditions, namely, tires deflated and shock absorbers depressurized. In addition, there must be a clearance of approximately 50 mm (1.97 in) between the aircraft jacking point and the jack upper end. 2-14-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING (3) The lifting jack stroke enables the aircraft to be jacked up so that the fuselage longitudinal datum line (aircraft center line) is parallel to the ground, with a clearance of 100 mm (3.94 in) between the main landing gear wheels and the ground. This enables the landing gear extension/retraction tests to be performed. 3. Shoring Cradles When it is necessary to support the aircraft in order to relieve the loads on the structure to do modifications or major work, shoring cradles shall be placed under each wing and the fuselage as necessary. NOTE : The aircraft must not be lifted or supported by the wings or fuselage alone without adequate support of the other. 2-14-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo WING JACKING POINT B X C A Y SAFETY STAY FWD JACKING POINT B’ WING JACKING POINT X MAXIMUM LOAD ELIGIBLE Y m ft m ft daN FORWARD FUSELAGE JACKING POINT A 2.74 8.99 0 0 6 800 WING JACKING POINT B 15.97 52.40 6.50 21.33 28 500 B’ 15.97 52.40 −6.50 −21.33 28 500 SAFETY STAY C 28.83 94.59 0 0 2 000 NOTE: SAFETY STAY IS NOT USED FOR JACKING. N_AC_021400_1_0050101_01_01 Jacking for Maintenance Jacking Point Locations FIGURE-2-14-0-991-005-A01 2-14-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A FR8 POINT A DETAIL Z−1 979.8 Z−1 987 B A SPHERICAL RADIUS 19 mm (0.75 in) B N_AC_021400_1_0060101_01_00 Jacking for Maintenance Forward Jacking Point FIGURE-2-14-0-991-006-A01 2-14-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A WING JACK PAD A LOWER SURFACE B POINT BB’ DETAIL RIB9 INTERSECTION WITH REAR SPAR DATUM Z−828.35 A SPHERICAL RADIUS 32 mm (1.26 in) B EXAMPLE REAR SPAR DATUM Z−895 N_AC_021400_1_0070101_01_00 Jacking for Maintenance Wing Jacking Points FIGURE-2-14-0-991-007-A01 2-14-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A Z−748.44 SPHERICAL RADIUS 19 mm (0.75 in) (19 D535−71 595) 126.15 mm X = 31 372 (4.97 in) A N_AC_021400_1_0080101_01_00 Jacking for Maintenance Safety Stay FIGURE-2-14-0-991-008-A01 2-14-0 Page 6 May 01/14 B B’ M CONFIGURATION DESCRIPTION A B’ C N M N 2-14-0 2.55 m 3.66 m 3.81 m (8.37 ft) (12.01 ft) (12.50 ft) 3.20 m 4.31 m 4.46 m (10.50 ft) (14.14 ft) (14.63 ft) 2.39 m 3.12 m 2.91 m (7.84 ft) (10.24 ft) (9.55 ft) AIRCRAFT ON JACKS, STANDARD TIRES AND STANDARD SHOCK ABSORBERS EXTENDED, FUSELAGE DATUM LINE PARALLEL TO GROUND (AT 4.56 m (14.96 ft) FROM THE GROUND), MLG WHEELS CLEARANCE 0.12 m (0.39 ft) AIRCRAFT ON JACKS, STANDARD TIRES AND STANDARD SHOCK ABSORBERS EXTENDED, FUSELAGE DATUM LINE PARALLEL TO GROUND (AT 5.21 m (17.09 ft) FROM THE GROUND), MLG WHEELS CLEARANCE 0.77 m (2.52 ft) AIRCRAFT ON JACK ’A’ WITH MLG WHEELS ON GROUND, SAFETY STAY ’C’ IN POSITION, STANDARD TIRES, NLG SHOCK ABSORBERS EXTENDED, NLG WHEELS CLEARANCE 0.06 m (0.20 ft) EXTENSION AND RETRACTION OF MLG REPLACEMENT OF MLG EXTENSION AND RETRACTION TEST OF NLG 1.86 m 3.12 m 3.43 m (6.10 ft) (10.24 ft) (11.25 ft) AIRCRAFT ON WHEELS WITH FLAT TIRES AND SHOCK ABSORBERS 1.66 m 2.74 m 2.86 m (5.45 ft) (8.99 ft) (9.38 ft) DEFLATED 1.58 m 3.12 m 3.70 m (5.18 ft) (10.24 ft) (12.14 ft) L CHECK OF DISTANCE BETWEEN AIRCRAFT ON WHEELS WITH STANDARD TIRES AND STANDARD JACKING POINTS AND GROUND (STANDARD AIRCRAFT POSITION) SHOCK ABSORBERS CHECK OF DISTANCE BETWEEN JACKING POINTS AND GROUND (LOWEST POSITION FOR POINTS B AND B’) CHECK OF DISTANCE BETWEEN AIRCRAFT ON WHEELS WITH NLG SHOCK ABSORBER DEFLATED JACKING POINTS AND GROUND AND FLAT TIRES, MLG WITH STANDARD SHOCK ABSORBERS AND (LOWEST POSITION FOR POINT A) STANDARD TIRES CONFIGURATION CASE L A FUSELAGE DATUM LINE @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_021400_1_0090101_01_01 Jacking for Maintenance Jacking Design FIGURE-2-14-0-991-009-A01 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 20 40 60 30 50 70 50 90 45 PERMISSIBLE WIND SPEED (km/h) 40 AIRCRAFT CG (%RC) 35 30 70 25 20 15 70 60 B 65 60 50 55 C 40 50 A D 45 40 30 TIP UP SECURITY MARGIN AIRCRAFT WEIGHT (kg x 1 000) LOAD ON WING JACKING POINTS (kg x 1 000) 55 80 35 30 20 0 1 2 3 4 5 6 7 8 9 10 LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1000) EXAMPLE: ASSUME AIRCRAFT WITH GROSS WEIGHT OF 47 000 kg A AND CENTER OF GRAVITY AT 18 % RC B . THE REACTION AT THE WING JACKING POINTS IS 41 500 kg (20 750 kg PER SIDE) C AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINT IS 5 500 kg D . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE THE WIND SPEED MUST NOT BE IN EXCESS OF 84 km/h. N_AC_021400_1_0100101_01_00 Loads at the Aircraft Jacking Points Wing Jacking Point and Forward Fuselage Jacking Point FIGURE-2-14-0-991-010-A01 2-14-0 Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FR73 / FR74 (SAFETY STAY) FR60 RIB4 RIB4 RIB22 RIB22 RIB13 RIB13 FR28 FR9 NOTE: THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME. N_AC_021400_1_0110101_01_00 Jacking for Maintenance Location of Shoring Cradles FIGURE-2-14-0-991-011-A01 2-14-0 Page 9 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo Jacking of the Landing Gear 1. General Landing gear jacking will be required to lift the landing gear wheels off the ground. NOTE : You can lift the aircraft at Maximum Ramp Weight (MRW). NOTE : The load at each jacking position is the load required to give a 25.4 mm (1 in) clearance between the ground and the tire. 2. Main Gear Jacking The main gears are normally jacked up by placing a jack directly under the ball pad. The ball spherical radius is 19 mm (0.75 in). It is also possible to jack the main gear using a cantilever jack. 3. Nose Gear Jacking For nose gear jacking, a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shockabsorber sliding tube. Jacking can be accomplished either by placing a jack directly under the ball pad, or using an adapter fitting provided with an identical ball pad. 2-14-0 Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 49 x 19 R20 600 mm (23.62 in) FULLY EXTENDED 200 mm (7.87 in) FULLY RETRACTED 45 x 16 R20 218 mm (8.58 in) 25 mm (1 in) 180 mm (7.09 in) ON THE RIM FLAT TIRES 38 mm (1.5 in) DIA. BALL 552 mm (21.73 in) INFLATED TIRES NOTE: TWIN WHEEL TRACK IS 927 mm (36.5 in). THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES. THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in) CLEARANCE BETWEEN THE TIRE AND GROUND. N_AC_021400_1_0170101_01_00 Jacking of the Landing Gear MLG Jacking Point Location - Twin Wheels FIGURE-2-14-0-991-017-A01 2-14-0 Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 643 mm (25.32 in) MLG TIRE 49 x 19 R20 CANTILEVER ARM 552 mm (21.73 in) 25 mm (1 in) FWD TWIN WHEEL TRACK 927 mm (36.5 in) DOUBLE FLAT MLG TIRES 218 mm (8.58 in) (180 mm (7.09 in) ON RIM) FORK 409 mm (16.1 in) 25 mm (1 in) MIN 1 620 mm (63.78 in) 25 mm (1 in) MIN APPROX CONTOUR OF TIRES ON GROUND N_AC_021400_1_0180101_01_00 Jacking of the Landing Gear MLG Jacking with Cantilever Jack - Twin Wheels FIGURE-2-14-0-991-018-A01 2-14-0 Page 12 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo LOAD AT MLG JACKING POINT 1 000 kg 40 CG POSITION 40% 30% 25% 20% 14% 35 30 25 20 15 10 5 30 70 40 80 90 50 100 110 60 120 130 70 140 150 80 160 170 180 x1 000 kg x1 000 lb AIRCRAFT WEIGHT MODEL 100 N_AC_021400_1_0190101_01_00 Jacking of the Landing Gear Loads at MLG Jacking Points - Twin Wheels FIGURE-2-14-0-991-019-A01 2-14-0 Page 13 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo LOAD AT MLG JACKING POINT 1 000 kg CG POSITION 36 36.0% CG 34 26.0% CG 32 21.0% CG 30 28 14.0% CG 26 24 22 20 18 45 50 100 110 55 120 60 130 65 140 75 70 150 160 x1 000 kg 80 170 180 x1 000 lb AIRCRAFT WEIGHT N_AC_021400_1_0200101_01_00 Jacking of the Landing Gear Loads at MLG Jacking Points - 75 500 kg FIGURE-2-14-0-991-020-A01 2-14-0 Page 14 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A 40 mm (1.57 in) APPROX 128 mm (5.04 in) 25 mm (1 in) 38 mm (1.5 in) DIA. BALL SAE AS 33559 326 mm (12.83 in) FWD 500 mm (19.69 in) 264 mm MIN (10.39 in) 289 mm MAX (11.38 in) 198 mm (7.8 in) FLAT TIRES INFLATED TIRES A NOTE: THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES. THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in) CLEARANCE BETWEEN THE TIRE AND GROUND. N_AC_021400_1_0210101_01_00 Jacking of the Landing Gear NLG Jacking - Point Location FIGURE-2-14-0-991-021-A01 2-14-0 Page 15 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo LOAD AT NLG JACKING POINT 1 000 kg CG POSITION 15 14 14% 13 12 20% 11 25% 10 9 30% 8 7 6 40% 5 4 3 2 1 x1 000 kg 30 40 50 60 70 80 x1 000 lb 70 80 90 100 110 120 130 140 150 160 170 180 AIRCRAFT WEIGHT MODEL 100 N_AC_021400_1_0220101_01_00 Jacking of the Landing Gear Loads at NLG Jacking Points FIGURE-2-14-0-991-022-A01 2-14-0 Page 16 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo LOAD AT NLG JACKING POINT 1 000 kg CG POSITION 12 14.0% CG 11 21.0% CG 10 26.0% CG 9 8 7 36.0% CG 6 5 4 3 45 50 100 110 55 120 60 130 65 140 75 70 150 160 x1 000 kg 80 170 AIRCRAFT WEIGHT 180 x1 000 lb N_AC_021400_1_0230101_01_00 Jacking of the Landing Gear Loads at NLG Jacking Points - 75 500 kg FIGURE-2-14-0-991-023-A01 2-14-0 Page 17 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING AIRCRAFT PERFORMANCE 3-1-0 General Information **ON A/C A319-100 A319neo General Information 1. Standard day temperatures for the altitudes shown are tabulated below: FEET 0 2 4 6 8 000 000 000 000 Standard Day Temperatures for the Altitudes Standard Day Temperature Altitude METERS ˚F ˚C 0 59.0 15.0 610 51.9 11.1 44.7 1 220 7.1 1 830 37.6 3.1 2 440 30.5 -0.8 3-1-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 3-2-1 Payload / Range - ISA Conditions **ON A/C A319-100 A319neo ISA Conditions 1. This section provides the payload/range at ISA conditions. 3-2-1 Page 1 May 01/14 3-2-1 1 000 0 500 2 4 6 8 10 12 14 16 18 20 2 000 1 000 3 000 1 500 4 000 2 000 5 000 2 500 3 500 7 000 4 000 8 000 4 500 9 000 5 000 MTOW − 64 000 kg (141 096 lb) MTOW − 75 500 kg (166 449 lb) MTOW − 75 500 kg (166 449 lb); 2 ACT 6 000 3 000 NOTE : THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. 0 4 8 12 16 20 24 28 32 36 40 44 PAYLOAD PAYLOAD (1 000 lb) (1 000 kg) RANGE (km) RANGE (nm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_030201_1_0130101_01_00 Payload/Range FIGURE-3-2-1-991-013-A01 Page 2 May 01/14 3-2-1 1 000 0 500 2 4 6 8 10 12 14 16 18 20 2 000 1 000 3 000 1 500 4 000 2 000 5 000 2 500 3 500 7 000 4 000 8 000 4 500 9 000 5 000 MTOW − 64 000 kg (141 096 lb) MTOW − 75 500 kg (166 449 lb) MTOW − 75 500 kg (166 449 lb); 2 ACT 6 000 3 000 NOTE : THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. 0 4 8 12 16 20 24 28 32 36 40 44 PAYLOAD PAYLOAD (1 000 lb) (1 000 kg) RANGE (km) RANGE (nm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_030201_1_0140101_01_00 Payload/Range Sharklet FIGURE-3-2-1-991-014-A01 Page 3 May 01/14 3-2-1 1 000 0 500 2 4 6 8 10 12 14 16 18 20 2 000 1 000 3 000 1 500 4 000 2 000 5 000 2 500 3 500 7 000 4 000 8 000 4 500 9 000 5 000 MTOW − 64 000 kg (141 096 lb) MTOW − 75 500 kg (166 449 lb) MTOW − 75 500 kg (166 449 lb); 1 ACT 6 000 3 000 NOTE : THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. 0 4 8 12 16 20 24 28 32 36 40 44 PAYLOAD PAYLOAD (1 000 lb) (1 000 kg) RANGE (km) RANGE (nm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo N_AC_030201_1_0150101_01_00 Payload/Range FIGURE-3-2-1-991-015-A01 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 3-3-1 Take-off Weight Limitation - ISA Conditions **ON A/C A319-100 Take-Off Weight Limitation - ISA Conditions 1. This section gives the take-off weight limitation at ISA conditions. 3-3-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. 1000 kg 1000 lb AIRPORT PRESSURE ALTITUDE (1000 ft) 110 230 100 80 TAKE−OFF WEIGHT 90 220 210 200 190 180 0 2 4 6 8 170 160 70 150 140 60 130 120 50 110 1000 ft 4 6 8 10 12 14 16 40 RUNWAY LENGTH 1000 m 1 2 3 4 5 N_AC_030301_1_0030101_01_00 Take-Off Weight Limitation - ISA Conditions CFM56 Series Engine FIGURE-3-3-1-991-003-A01 3-3-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. 1000 kg 1000 lb AIRPORT PRESSURE ALTITUDE (1000 ft) 110 230 100 80 TAKE−OFF WEIGHT 90 220 210 200 190 180 0 2 4 6 8 170 160 70 150 140 60 130 120 50 110 1000 ft 4 6 8 10 12 14 16 40 RUNWAY LENGTH 1000 m 1 2 3 4 5 N_AC_030301_1_0040101_01_00 Take-Off Weight Limitation - ISA Conditions IAE V2500 Series Engine FIGURE-3-3-1-991-004-A01 3-3-1 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 3-3-2 Take-off Weight Limitation - ISA +15¿C (+59¿F) Conditions **ON A/C A319-100 Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions 1. This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions. 3-3-2 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. 1000 kg 1000 lb 110 80 220 TAKE−OFF WEIGHT 90 210 200 190 180 0 2 4 6 8 170 160 70 AIRPORT PRESSURE ALTITUDE (1000 ft) 230 100 150 140 60 130 120 50 110 1000 ft 4 6 8 10 12 14 16 40 RUNWAY LENGTH 1000 m 1 2 3 4 5 N_AC_030302_1_0030101_01_00 Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions CFM56 Series Engine FIGURE-3-3-2-991-003-A01 3-3-2 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. 1000 kg 1000 lb AIRPORT PRESSURE ALTITUDE (1000 ft) 110 230 100 80 TAKE−OFF WEIGHT 90 220 210 200 190 180 0 2 4 6 8 170 160 70 150 140 60 130 120 50 110 1000 ft 4 6 8 10 12 14 16 40 RUNWAY LENGTH 1000 m 1 2 3 4 5 N_AC_030302_1_0040101_01_00 Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions IAE V2500 Series Engine FIGURE-3-3-2-991-004-A01 3-3-2 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 3-4-1 Landing Field Length - ISA Conditions **ON A/C A319-100 Landing Field Length - ISA Conditions 1. This section provides the landing field length. 3-4-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 6.0 ISA CONDITIONS SLATS 27 DEG. FLAPS 35 DEG. PRESSURE ALTITUDE (x 1 000 ft) 10 5.5 8 6 4 2 LANDING LENGTH (x 1 000 ft) SEA LEVEL 5.0 4.5 4.0 3.5 3.0 40 60 80 100 120 140 160 GROSS WEIGHT (x 1 000 lb) NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. N_AC_030401_1_0030101_01_01 Landing Field Length - ISA Conditions CFM56-5A Series Engine FIGURE-3-4-1-991-003-A01 3-4-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 5.5 ISA CONDITIONS SLATS 27 DEG. FLAPS 35 DEG. PRESSURE ALTITUDE (x 1 000 ft) 10 LANDING LENGTH (x 1 000 ft) 5.0 8 6 4 2 SEA LEVEL 4.5 4.0 3.5 3.0 40 60 80 100 120 140 160 GROSS WEIGHT (x 1 000 lb) NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. N_AC_030401_1_0040101_01_01 Landing Field Length - ISA Conditions IAE V2500 Series Engine FIGURE-3-4-1-991-004-A01 3-4-1 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 3-5-0 Final Approach Speed **ON A/C A319-100 Final Approach Speed 1. This section provides the final approach speed. It is defined as the indicated airspeed at threshold in the landing configuration, at the certificated maximum flap setting and Maximum Landing Weight (MLW), in standard atmospheric conditions. The approach speed is used to classify the aircraft into an Aircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold. 2. The final approach speed is 126 kt at a MLW of 62 500 kg (137 789 lb) and classifies the aircraft into the Aircraft Approach Category C. NOTE : This value is given for information only. 3-5-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING GROUND MANEUVERING 4-1-0 General Information **ON A/C A319-100 A319neo General Information 1. This section provides aircraft turning capability and maneuvering characteristics. For ease of presentation, this data has been determined from the theoretical limits imposed by the geometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such, it reflects the turning capability of the aircraft in favorable operating circumstances. This data should only be used as a guideline for the method of determination of such parameters and for the maneuvering characteristics of this aircraft type. In ground operating mode, varying airline practices may demand that more conservative turning procedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airline operating techniques will vary in the level of performance, over a wide range of operating circumstances throughout the world. Variations from standard aircraft operating patterns may be necessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limited area or a high risk of jet blast damage. For these reasons, ground maneuvering requirements should be coordinated with the airlines in question prior to layout planning. 4-1-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-2-0 Turning Radii **ON A/C A319-100 A319neo Turning Radii 1. This section gives the turning radii. 4-2-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo R3 R1 R5 50° 60° 70° 7.59 m (24.9 ft) R2 R6 11.04 m (36.22 ft) R4 NOTE: FOR STEERING DIMENSION TABLE SEE SHEET 2. TURN TYPE: 1. ASYMMETRIC THRUST DIFFERENTIAL BRAKING (PIVOTTING ON ONE MAIN GEAR). 2. SYMMETRIC THRUST NO BRAKING. N_AC_040200_1_0030101_01_02 Turning Radii, No Slip Angle FIGURE-4-2-0-991-003-A01 4-2-0 Page 2 May 01/14 24.3 20.9 55 44 35 28 22 16.7 13.3 10.6 8.5 6.7 29.1 33.9 38.8 43.6 48.4 30 35 40 45 50 2 2 2 2 2 4-2-0 2 0.5 8 2.5 5 12 1.4 17 5.1 3.7 8.1 27 30 33 9.0 10.1 41 37 11.3 12.6 11.7 12.1 12.5 13.2 14.0 14.9 11.8 12.2 12.6 38 40 41 43 46 49 39 40 41 43 46 49 53 59 21.1 69 72 76 23.1 22.0 80 84 24.3 25.6 70 89 27.1 21.4 73 76 23.2 22.2 80 84 25.7 24.4 89 95 27.2 102 31.1 29.0 92 87 28.0 26.5 75 72 22.8 22.0 78 82 23.9 87 92 22.3 28.0 25.1 73 23.0 26.4 79 76 24.0 83 98 25.2 105 113 34.6 29.8 125 38.0 31.9 162 140 42.6 ft 49.4 m SHARKLET 16.5 16.7 17.1 17.5 18.1 18.8 16.6 16.8 17.1 17.5 18.1 18.9 19.8 21.2 23.0 25.6 29.3 35.2 m 54 55 56 57 59 62 54 55 56 58 59 62 65 69 75 84 96 116 ft R5 NOSE 19.6 20.0 20.6 21.3 22.2 23.2 19.7 20.1 20.7 21.4 22.3 23.3 24.6 26.2 28.3 31.1 35.1 41.2 m ft 64 66 68 70 73 76 65 66 68 70 73 76 81 86 93 102 115 135 R6 THS NOTE: ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION. TYPE 1 TURNS USE: ASYMMETRIC THRUST DURING THE WHOLE TURN; AND DIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY. TYPE 2 TURNS USE: SYMMETRIC THRUST DURING THE WHOLE TURN; AND NO DIFFERENTIAL BRAKING AT ALL. IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN. 71.9 75 (MAX) 1 63.1 67.7 65 1 70 58.3 1 1 53.5 55 60 1 28 47 8.4 14.2 3 22 0.8 50 1 6.6 70.3 48.6 75 (MAX) 2 30 9.2 5 1.6 34 10.2 9 2.6 62.5 66.9 13.2 65 14.0 42 37 70 15.0 47 2 16.3 111 33.7 66 20.1 69 17.9 122 37.1 76 23.0 80 53 137 41.8 89 27.2 60 159 48.6 110 33.5 ft 95 m 117 WINGTIP FENCE R4 − WING ft R3 NLG m ft 2 13 2 12.7 11.4 17 5.2 3.8 53.2 57.9 55 60 2 14.3 16.1 18.2 35.8 29.0 92 70 24.3 25 28.2 21.4 19.4 20 2 m ft R2 LMLG m R1 RMLG 2 TYPE OF STEERING EFFECTIVE TURN ANGLE STEERING ANGLE (deg) (deg) MAXIMUM RAMP WEIGHT @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_040200_1_0040101_01_01 Turning Radii, No Slip Angle FIGURE-4-2-0-991-004-A01 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-3-0 Minimum Turning Radii **ON A/C A319-100 A319neo Minimum Turning Radii 1. This section gives the minimum turning radii. 4-3-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo R4 11.0 m (36 ft) R6 OUTSIDE FACE OF TIRE Y EFFECTIVE TURN A STEERING ANGLE 75° MINIMUM PAVEMENT WIDTH FOR 180° TURN R3 R5 NOTE: NOSE GEAR RADII TRACK R3, MEASURED FROM OUTSIDE FACE OF TIRE. MODEL 100 TURN DIMENSION SHOWN. THEORETICAL CENTER OF TURN FOR MINIMUM TURNING RADIUS. SLOW CONTINUOUS TURNING. APPROXIMATELY IDLE THRUST ON ALL ENGINES. NO DIFFERENTIAL BRAKING. DRY SURFACE. TYPE STEERING OF ANGLE TURN (DEG) EFFECTIVE STEERING ANGLE 1 75 (MAX) 71.9° 2 75 (MAX) 70.3° R4 WING WING TIP SHARKLET FENCE 21.1 22.0 R5 NOSE R6 THS 16.5 19.6 54 64 22.3 16.6 19.7 73 54 65 Y A R3 NLG m 3.6 20.1 11.7 ft 12 66 38 69 72 m 3.9 20.5 11.8 21.4 ft 13 67 39 70 NOTE: IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN. N_AC_040300_1_0020101_01_02 Minimum Turning Radii FIGURE-4-3-0-991-002-A01 4-3-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-4-0 Visibility from Cockpit in Static Position **ON A/C A319-100 A319neo Visibility from Cockpit in Static Position 1. This section gives the visibility from cockpit in static position. 4-4-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo NOT TO BE USED FOR LANDING APPROACH VISIBILITY DIMENSIONS ARE APPROXIMATE 30° VISUAL ANGLES IN VERTICAL PLANE THROUGH PILOT EYE POSITION. 20° 2.41 m (7 ft 10.92 in) 4.56 m (14 ft 11.52 in) 10.14 m (33 ft 3.24 in) 111° 133° FIRST OFFICER FIELD OF VIEW 5.07 m (16 ft 7.56 in) MAX AFT VISION WITH HEAD TURNED AROUND SPINAL COLUMN. WING TIP CAN BE SEEN WHEN HEAD IS MOVED TO THE SIDE. VISUAL ANGLES IN HORIZONTAL PLANE THROUGH PILOT EYE POSITION. CAPTAIN FIELD OF VIEW 111° 133° WITH HEAD MOVED 125 mm (5 in) OUTBOARD VISUAL ANGLES IN PLANE PERPENDICULAR TO LONGITUDINAL AXIS. 0.53 m (1 ft 8.88 in) 46° 46° 33° 33° 25° 25° 32° 32° ZONE THAT CANNOT BE SEEN NOTE: PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS. N_AC_040400_1_0010101_01_03 Visibility from Cockpit in Static Position FIGURE-4-4-0-991-001-A01 4-4-0 Page 2 May 01/14 20° 25° 10° 0° 10° 20° 35° 30° CAPTAIN SLIDING WINDOW CAPTAIN WINDSHIELD FIRST OFFICER WINDSHIELD FIRST OFFICER SLIDING WINDOW FIRST OFFICER FIXED WINDOW 4-4-0 PILOT EYE POSITION (CAPTAIN POSITION) EXAMPLE: WHEN CAPTAIN TURNS HIS HEAD BY 80° LEFT, VISIBILITY WILL BE 35° UP AND 25° DOWN THROUGH THE SLIDING WINDOW FRAME. CAPTAIN FIELD OF VIEW SHOWN. FIRST OFFICER FIELD OF VIEW SYMMETRICAL. A320 AS 580 B 130°120° 110°100° 90° 80° 70° 60° 50° 40° 30° 20° 10° 0° 10° 20° 30° 40° 50° 60° 70° 80° 90° 100° 110° CAPTAIN FIXED WINDOW @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_040400_1_0050101_01_00 Binocular Visibility Through Windows from Captain Eye Position FIGURE-4-4-0-991-005-A01 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-5-0 Runway and Taxiway Turn Paths **ON A/C A319-100 A319neo Runway and Taxiway Turn Paths 1. Runway and Taxiway Turn Paths. 4-5-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-5-1 135˚ Turn - Runway to Taxiway **ON A/C A319-100 A319neo 135˚ Turn - Runway to Taxiway 1. This section gives the 135˚ turn - runway to taxiway. 4-5-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FA L A LE = AD 45 − m IN (1 FIL 50 L ft) ET APPROX 5.1 m (17 ft) TAXIWAY CENTERLINE FILLET R = 16.5 m (55 ft) TURN R = 30 m (100 ft) RUNWAY CENTERLINE 15 m (50 ft) NLG PATH 30 m (100 ft) MLG PATH NOTE: FAA GROUP III FACILITIES. N_AC_040501_1_0020101_01_02 135˚ Turn - Runway to Taxiway Cockpit Over Centerline Method FIGURE-4-5-1-991-002-A01 4-5-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo APPROX 3.2 m (10 ft) FA A LE A 45 D− m IN F (1 IL 50 LE FILLET R = 16.5 m ft) T (55 ft) L = TAXIWAY CENTERLINE TURN R = 30 m (100 ft) RUNWAY CENTERLINE 15 m (50 ft) NLG PATH 30 m (100 ft) MLG PATH NOTE: FAA GROUP III FACILITIES. N_AC_040501_1_0030101_01_02 135˚ Turn - Runway to Taxiway Judgemental Oversteering Method FIGURE-4-5-1-991-003-A01 4-5-1 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-5-2 90˚ Turn - Runway to Taxiway **ON A/C A319-100 A319neo 90˚ Turn - Runway to Taxiway 1. This section gives the 90˚ turn - runway to taxiway. 4-5-2 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FAA LEAD−IN FILLET L = 45 m (150 ft) 15 m (50 ft) APPROX 6.4 m (21 ft) TAXIWAY CENTERLINE FILLET R = 16.5 m (55 ft) TURN R = 30 m (100 ft) NLG PATH RUNWAY CENTERLINE MLG PATH 30 m (100 ft) NOTE: FAA GROUP III FACILITIES. N_AC_040502_1_0020101_01_01 90˚ Turn - Runway to Taxiway Cockpit Over Centerline Method FIGURE-4-5-2-991-002-A01 4-5-2 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FAA LEAD−IN FILLET L = 45 m (150 ft) 15 m (50 ft) APPROX 9 m (29 ft) TAXIWAY CENTERLINE FILLET R = 16.5 m (55 ft) TURN R = 30 m (100 ft) NLG PATH RUNWAY CENTERLINE MLG PATH 30 m (100 ft) NOTE: FAA GROUP III FACILITIES. N_AC_040502_1_0030101_01_01 90˚ Turn - Runway to Taxiway Judgemental Oversteering Method FIGURE-4-5-2-991-003-A01 4-5-2 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-5-3 180˚ Turn on a Runway **ON A/C A319-100 A319neo 180˚ Turn on a Runway 1. This section gives the 180˚ turn on a runway. 4-5-3 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo RUNWAY CENTERLINE 6.6 m (22 ft) 3m (10 ft) R3 = 11.7 m (39 ft) R5 = 16.5 m (55 ft) R4 NLG PATH WINGTIP PATH: WINGTIP FENCES: R4 = 21.1 m (70 ft) SHARKLETS: R4 = 22 m (72 ft) NOSE PATH 30 m (100 ft) MLG PATH NOTE: TYPE 1 VALUES. N_AC_040503_1_0010101_01_02 180˚ Turn on a Runway Edge of Runway Method (Sheet 1 of 2) FIGURE-4-5-3-991-001-A01 4-5-3 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo RUNWAY CENTERLINE R5 = 16.5 m (55 ft) R4 R3 = 11.7 m (38 ft) 4.75 m (16 ft) 5.22 m (17 ft) 25° NLG PATH 30 m (100 ft) WINGTIP PATH: WINGTIP FENCES: R4 = 21.1 m (70 ft) SHARKLETS: R4 = 22 m (72 ft) NOSE PATH MLG PATH NOTE: TYPE 1 VALUES. N_AC_040503_1_0010102_01_00 180˚ Turn on a Runway Center of Runway Method (Sheet 2 of 2) FIGURE-4-5-3-991-001-A01 4-5-3 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-5-4 135˚ Turn - Taxiway to Taxiway **ON A/C A319-100 A319neo 135˚ Turn - Taxiway to Taxiway 1. This section gives the 135˚ turn - taxiway to taxiway. 4-5-4 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FA A L = LEA 45 D m −IN (1 F 50 IL ft) LET APPROX 5.8 m (19 ft) FILLET R = 16.5 m (55 ft) TURN R = 30 m (100 ft) TAXIWAY CENTERLINE 15 m (50 ft) TAXIWAY CENTERLINE 15 m (50 ft) NLG PATH MLG PATH NOTE: FAA GROUP III FACILITIES N_AC_040504_1_0050101_01_00 135˚ Turn - Taxiway to Taxiway Cockpit Over Centerline Method (Sheet 1 of 2) FIGURE-4-5-4-991-005-A01 4-5-4 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo APPROX 3.3 m (11ft) FA A L = LEA 45 D m −IN (1 F 50 IL ft) LET FILLET R = 16.5 m (55 ft) TURN R = 30 m (100 ft) TAXIWAY CENTERLINE 15 m (50 ft) TAXIWAY CENTERLINE 15 m (50 ft) NLG PATH MLG PATH NOTE: FAA GROUP III FACILITIES N_AC_040504_1_0050102_01_00 135˚ Turn - Taxiway to Taxiway Judgemental Oversteering Method (Sheet 2 of 2) FIGURE-4-5-4-991-005-A01 4-5-4 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-5-5 90˚ Turn - Taxiway to Taxiway **ON A/C A319-100 A319neo 90˚ Turn - Taxiway to Taxiway 1. This section gives the 90˚ turn - taxiway to taxiway. 4-5-5 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FAA LEAD−IN FILLET L = 45 m (150 ft) 15 m (50 ft) APPROX 6.1 m (20 ft) TAXIWAY CENTERLINE FILLET R = 16.5 m (55 ft) TURN R = 30 m (100 ft) NLG PATH TAXIWAY CENTERLINE MLG PATH 15 m (50 ft) NOTE: FAA GROUP III FACILITIES. N_AC_040505_1_0030101_01_00 90˚ Turn - Taxiway to Taxiway Cockpit Over Centerline Method (Sheet 1 of 2) FIGURE-4-5-5-991-003-A01 4-5-5 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FAA LEAD−IN FILLET L = 45 m (150 ft) 15 m (50 ft) APPROX 9 m (29 ft) TAXIWAY CENTERLINE FILLET R = 16.5 m (55 ft) TURN R = 30 m (100 ft) NLG PATH TAXIWAY CENTERLINE MLG PATH 15 m (50 ft) NOTE: FAA GROUP III FACILITIES. N_AC_040505_1_0030102_01_00 90˚ Turn - Taxiway to Taxiway Judgemental Oversteering Method (Sheet 2 of 2) FIGURE-4-5-5-991-003-A01 4-5-5 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-6-0 Runway Holding Bay (Apron) **ON A/C A319-100 A319neo Runway Holding Bay (Apron) 1. This section gives the runway holding bay (Apron). 4-6-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 6.1 m (20 ft) 90 m (300 ft) 61 m (200 ft) 12.2 m (40 ft) HOLDING POINT 6.1 m (20 ft) 190 m (625 ft) TAXIWAY CENTERLINE RUNWAY CENTERLINE 45 m (150 ft) 23 m (75 ft) NOTE: LAYOUT IN ACCORDANCE WITH THE REQUIREMENTS OF NAS 3601, CHAPTER 4, AND AN/865, CHAPTER 3. OUTER PARKED AIRCRAFT TURNED THRU MIN. TURN RADIUS TO PARKED POSITION. N_AC_040600_1_0020101_01_02 Runway Holding Bay (Apron) FIGURE-4-6-0-991-002-A01 4-6-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-7-0 Minimum Line-Up Distance Corrections **ON A/C A319-100 A319neo Minimum Line-Up Distance Corrections 1. The ground maneuvers were performed using asymmetric thrust and differential braking only to initiate the turn. TODA: Take-Off Distance Available ASDA: Acceleration-Stop Distance Available 2. 90˚ Turn on Runway Entry This section gives the minimum line-up distance correction for a 90˚ turn on runway entry. This maneuver consists in a 90˚ turn at minimum turn radius. It starts with the edge of the MLG at a distance of 3 m (10 ft) from the taxiway edge, and finishes with the aircraft aligned on the centerline of the runway, see FIGURE 4-7-0-991-017-A. During the turn, all the clearances must meet the minimum value of 3 m (10 ft) for this category of aircraft as recommended in ICAO Annex 14. 3. 180˚ Turn on Runway Turn Pad This section gives the minimum line-up distance correction for a 180˚ turn on the runway turn pad. This maneuver consists in a 180˚ turn at minimum turn radius on a runway turn pad with standard ICAO geometry. It starts with the edge of the MLG at a distance of 3 m (10 ft) from the pavement edge, and it finishes with the aircraft aligned on the centerline of the runway, see FIGURE 4-7-0-991-018-A. During the turn, all the clearances must meet the minimum value of 3 m (10 ft) for this category of aircraft as recommended in ICAO Annex 14. 4. 180˚ Turn on Runway Width This section gives the minimum line-up distance correction for a 180˚ turn on the runway width. For this maneuver, the pavement width is considered to be the runway width, which is a frozen parameter (30 m (100 ft), 45 m (150 ft) and 60 m (200 ft)). As per the standard operating procedures for the ”180˚ turn on runway” (described in the Flight Crew Operating Manual), the aircraft is initially angled with respect to the runway centerline when starting the 180˚ turn, see FIGURE 4-7-0-991-019-A. The value of this angle depends on the aircraft type and is mentioned in the FCOM. During the turn, all the clearances must meet the minimum value of 3 m (10 ft) for this category of aircraft as recommended in ICAO Annex 14. 4-7-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 3m (10 ft) TODA ASDA TAXIWAY CENTERLINE >3m (10 ft) RUNWAY CENTERLINE ASDA: ACCELERATION−STOP DISTANCE AVAILABLE TODA: TAKE−OFF DISTANCE AVAILABLE 90° TURN ON RUNWAY ENTRY 30 m (100 ft)/45 m (150 ft)/60 m (200 ft) WIDE RUNWAY AIRCRAFT TYPE MAX STEERING ANGLE A319 75° MINIMUM LINE−UP DISTANCE CORRECTION ON TODA 11.1 m 36 ft ON ASDA 22.1 m 73 ft N_AC_040700_1_0170101_01_00 Minimum Line-Up Distance Corrections 90˚ Turn on Runway Entry FIGURE-4-7-0-991-017-A01 4-7-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo MINIMUM PAVEMENT WIDTH 3m (10 ft) TODA >3m (10 ft) 3m (10 ft) ASDA RUNWAY CENTERLINE ASDA: ACCELERATION−STOP DISTANCE AVAILABLE TODA: TAKE−OFF DISTANCE AVAILABLE 180° TURN ON RUNWAY TURN PAD 30 m (100 ft)/45 m (150 ft)/60 m (200 ft) WIDE RUNWAY MAX AIRCRAFT STEERING TYPE ANGLE A319 75° MINIMUM LINE−UP DISTANCE CORRECTION ON TODA ON ASDA 15.0 m 49 ft 26.0 m 85 ft REQUIRED MINIMUM PAVEMENT WIDTH 29.7 m 97 ft N_AC_040700_1_0180101_01_00 Minimum Line-Up Distance Corrections 180˚ Turn on Runway Turn Pad FIGURE-4-7-0-991-018-A01 4-7-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 3m (10 ft) TODA 3m (10 ft) ASDA >3m (10 ft) RUNWAY CENTERLINE 25° ASDA: ACCELERATION−STOP DISTANCE AVAILABLE TODA: TAKE−OFF DISTANCE AVAILABLE 180° TURN ON RUNWAY WIDTH 30 m (100 ft)/45 m (150 ft)/60 m (200 ft) WIDE RUNWAY AIRCRAFT TYPE MAX STEERING ANGLE A319 75° MINIMUM LINE−UP DISTANCE CORRECTION ON TODA 15.0 m 49 ft ON ASDA 26.0 m 85 ft N_AC_040700_1_0190101_01_00 Minimum Line-Up Distance Corrections 180˚ Turn on Runway Width FIGURE-4-7-0-991-019-A01 4-7-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 4-8-0 Aircraft Mooring **ON A/C A319-100 A319neo Aircraft Mooring 1. This section provides information on aircraft mooring. 4-8-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo TOWING FITTING TOWING FITTING A B GROUND ANCHOR FWD A B N_AC_040800_1_0010101_01_00 Aircraft Mooring FIGURE-4-8-0-991-001-A01 4-8-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-1-1 Aircraft Servicing Arrangements **ON A/C A319-100 A319neo Aircraft Servicing Arrangements 1. This section provides typical ramp layouts, showing the various GSE items in position during typical turn-round scenarios. These ramp layouts show typical arrangements only. Each operator will have its own specific requirements/regulations for positioning and operation on the ramp. This table gives the symbols used on servicing diagrams. AC AS BULK CAT CB CLEAN FUEL GPU LDCL LV PBB PS TOW ULD WV Ground Support Equipment AIR CONDITIONING UNIT AIR START UNIT BULK TRAIN CATERING TRUCK CONVEYOR BELT CLEANING TRUCK FUEL HYDRANT DISPENSER or TANKER GROUND POWER UNIT LOWER DECK CARGO LOADER LAVATORY VEHICLE PASSENGER BOARDING BRIDGE PASSENGER STAIRS TOW TRACTOR ULD TRAIN POTABLE WATER VEHICLE 5-1-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-1-2 Typical Ramp Layout - Open Apron **ON A/C A319-100 A319neo Typical Ramp Layout -- Open Apron 1. This section gives the typical servicing arrangement for pax version (Open Apron). The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m from the aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks in position on landing gears). 5-1-2 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 0 0 FEET 5 10 15 20 2 4 6 METERS 8 AS TOW G PS BULK PU CAT CB AC FUEL BULK CB WV CAT PS LV STAND SAFETY LINE NOTE: TYPICAL RAMP LAYOUT APPLICABLE TO AIRCRAFT WITH OR WITHOUT SHARKLETS. N_AC_050102_1_0020101_01_03 Typical Ramp Layout Open Apron - Bulk Loading FIGURE-5-1-2-991-002-A01 5-1-2 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 0 0 FEET 5 10 15 20 2 4 6 METERS 8 AS TOW G PS ULD PU CAT AC LD CL FUEL ULD WV LD CL CAT PS LV STAND SAFETY LINE NOTE: TYPICAL RAMP LAYOUT APPLICABLE TO AIRCRAFT WITH OR WITHOUT SHARKLETS. N_AC_050102_1_0080101_01_00 Typical Ramp Layout Open Apron - ULD Loading FIGURE-5-1-2-991-008-A01 5-1-2 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-1-3 Typical Ramp Layout - Gate **ON A/C A319-100 A319neo Typical Ramp Layout - Gate 1. This section gives the typical servicing arrangement for pax version (Passenger Bridge). The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m from the aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks in position on landing gears). 5-1-3 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 0 0 FEET 5 10 15 20 2 4 6 METERS 8 AS TOW G PU ULD PBB CAT AC LD CL FUEL ULD WV LD CL CAT LV STAND SAFETY LINE NOTE: TYPICAL RAMP LAYOUT APPLICABLE TO AIRCRAFT WITH OR WITHOUT SHARKLETS. N_AC_050103_1_0010101_01_03 Typical Ramp Layout Gate FIGURE-5-1-3-991-001-A01 5-1-3 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-2-0 Terminal Operations - Full Servicing Turn Round Time Chart **ON A/C A319-100 A319neo Terminal Operations - Full Servicing Turn Round Time 1. This section provides a typical turn round time chart showing the typical time for ramp activities during aircraft turn round. Actual times may vary due to each operator’s specific practices, resources, equipment and operating conditions. 2. Assumptions used for full servicing turn round time chart A. PASSENGER HANDLING 124 pax: 8 F/C + 116 Y/C. All passengers deplane and board the aircraft. 1 Passenger Boarding Bridge (PBB) used at door L1. Equipment positioning + opening door = +2 min. Closing door + equipment removal = +1.5 min. No Passenger with Reduced Mobility (PRM) on board. Deplaning: - 124 pax at door L1 - Deplaning rate = 20 pax/min per door - Priority deplaning for premium passengers. Boarding: - 124 pax at door L1 - Boarding rate = 12 pax/min per door - Last Pax Seating allowance (LPS) + headcounting = +2 min. B. CARGO 2 cargo loaders. Opening door + equipment positioning = +2 min. Equipment removal + closing door = +1.5 min. 100% cargo exchange: - FWD cargo compartment: 2 containers - AFT cargo compartment: 2 containers - Bulk compartment: 500 kg (1 102 lb). Container unloading/loading times: - Unloading = 1.5 min/container - Loading = 1.5 min/container. Bulk unloading/loading times: 5-2-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING - Unloading = 120 kg/min (265 lb/min) Loading = 100 kg/min (220 lb/min). C. REFUELING 20 000 l (5 283 US gal) at 50 psig (3.45 bars-rel), one hose (right wing). Dispenser positioning/removal + connection/disconnection times = +2.5 min. D. CLEANING Cleaning is performed in available time. E. CATERING 1 catering truck for servicing galleys sequentially at doors R1 and R2. Equipment positioning + opening door = +2 min. Closing door + equipment removal = +1.5 min. Time to drive from one door to the other = +2 min. Full Size Trolley Equivalent (FSTE) to unload and load: 8 FSTE - 4 FSTE at door R1 - 4 FSTE at door R2. Time for trolley exchange = 1.2 min per FSTE. F. GROUND HANDLING/GENERAL SERVICING Start of operations: - Bridges/stairs: t0 = 0 - Other equipment: t = t0 + 1 min. Ground Power Unit (GPU): up to 90 kVA. Air conditioning: one hose. Potable water servicing: 100% uplift, 200 l (53 US gal). Toilet servicing: draining + rinsing. 5-2-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo TRT: 37 min 0 5 10 15 20 25 30 35 40 DEPLANING/BOARDING AT L1 HEADCOUNTING CATERING AT R1 CATERING AT R2 CLEANING AVAILABLE TIME CARGO FWD CC CARGO AFT CC BULK REFUELING POTABLE WATER SERVICING TOILET SERVICING GSE POSITIONING/REMOVAL ACTIVITY CRITICAL PATH N_AC_050200_1_0050101_01_02 Full Servicing Turn Round Time Chart FIGURE-5-2-0-991-005-A01 5-2-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-3-0 Terminal Operation - Outstation Turn Round Time Chart **ON A/C A319-100 A319neo Terminal Operations - Outstation Turn Round Time 1. This section provides a typical turn round time chart showing the typical time for ramp activities during aircraft turn round. Actual times may vary due to each operator’s specific practices, resources, equipment and operating conditions. 2. Assumptions used for outstation turn round time chart A. PASSENGER HANDLING 156 pax (all Y/C). All passengers deplane and board the aircraft. 2 stairways used at doors L1 & L2. Equipment positioning + opening door = +2 min. Closing door + equipment removal = +1.5 min. No Passenger with Reduced Mobility (PRM) on board. Deplaning: - 78 pax at door L1 - 78 pax at door L2 - Deplaning rate = 18 pax/min per door. Boarding: - 78 pax at door L1 - 78 pax at door L2 - Boarding rate = 12 pax/min per door - Last Pax Seating allowance (LPS) + headcounting = +2 min. B. CARGO 2 cargo loaders. Opening door + equipment positioning = +2 min. Equipment removal + closing door = +1.5 min. 100% cargo exchange: - FWD cargo compartment: 2 containers - AFT cargo compartment: 2 containers. Container unloading/loading times: - Unloading = 1.5 min/container - Loading = 1.5 min/container. C. REFUELING No refueling. 5-3-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING D. CLEANING Cleaning is performed in available time. E. CATERING One catering truck for servicing the galleys as required. F. GROUND HANDLING/GENERAL SERVICING Start of operations: - Bridges/stairs: t0 = 0 - Other equipment: t = t0 + 1 min. Ground Power Unit (GPU): up to 90 kVA. Air conditioning: one hose. No potable water servicing. No toilet servicing. 5-3-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo TRT: 21 min 0 5 10 15 20 25 DEPLANING/BOARDING AT L1 DEPLANING/BOARDING AT L2 HEADCOUNTING CATERING AVAILABLE TIME CLEANING AVAILABLE TIME CARGO FWD CC CARGO AFT CC REFUELING POTABLE WATER SERVICING TOILET SERVICING GSE POSITIONING/REMOVAL ACTIVITY CRITICAL PATH N_AC_050300_1_0020101_01_02 Outstation Turn Round Time Chart FIGURE-5-3-0-991-002-A01 5-3-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-1 Ground Service Connections **ON A/C A319-100 A319neo Ground Service Connections Layout 1. This section provides the ground service connections layout. 5-4-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 2 9 7 11 12 13 10 8 1 3 10 4 5 6 9 18 8 11 15 16 14 15 14 17 18 12 13 10 20 10 19 21 1 − GROUND ELECTRICAL POWER CONNECTOR 2 − OXYGEN SYSTEM 3 − NLG GROUNDING (EARTHING) POINT 4 − POTABLE WATER DRAIN PANEL 5 − LOW PRESSURE AIR PRE−CONDITIONING 6 − HIGH PRESSURE AIR PRE−CONDITIONING 7 − REFUEL/DEFUEL INTEGRATED PANEL 8 − IDG/STARTER OIL SERVICING 9 − ENGINE OIL SERVICING 10 − OVERPRESSURE PROTECTOR 11 − REFUEL/DEFUEL COUPLINGS (OPTIONAL−LH WING) 12 − OVERWING REFUEL (IF INSTALLED) 13 − NACA VENT INTAKE 14 − YELLOW HYDRAULIC−SYSTEM SERVICE PANEL 15 − BLUE HYDRAULIC−SYSTEM SERVICE PANEL 16 − ACCUMULATOR CHARGING (GREEN SYSTEM) AND RESERVOIR DRAIN (GREEN SYSTEM) 17 − GREEN HYDRAULIC−SYSTEM SERVICE PANEL 18 − MLG GROUNDING (EARTHING) POINT 19 − WASTE WATER SERVICE PANEL 20 − POTABLE WATER SERVICE PANEL 21 − APU OIL SERVICING N_AC_050401_1_0020101_01_02 Ground Service Connections Layout FIGURE-5-4-1-991-002-A01 5-4-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-2 Grounding Points **ON A/C A319-100 A319neo Grounding (Earthing) Points 1. Grounding (Earthing) Points DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE On Nose Landing Gear leg: On left Main Landing Gear leg: On right Main Landing Gear leg: 5.07 m (16.63 ft) 16.11 m (52.85 ft) 16.11 m (52.85 ft) LH SIDE RH SIDE On Centerline 3.79 m (12.43 ft) - - 3.79 m (12.43 ft) MEAN HEIGHT FROM GROUND 0.94 m (3.08 ft) 1.07 m (3.51 ft) 1.07 m (3.51 ft) A. The grounding (earthing) stud on each landing gear leg is designed for use with a clip-on connector (such as Appleton TGR). B. The grounding (earthing) studs are used to connect the aircraft to an approved ground (earth) connection on the ramp or in the hangar for: - Refuel/defuel operations, - Maintenance operations, - Bad weather conditions. NOTE : In all other conditions, the electrostatic discharge through the tire is sufficient. If the aircraft is on jacks for retraction and extension checks or for the removal/installation of the landing gear, the grounding (earthing) alternative points (if installed) are: - In the hole on the avionics-compartment lateral right door-frame (on FR14), - On the engine nacelles, - Adjacent to the high-pressure connector, - On the wing upper surfaces. 5-4-2 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A A NOSE LANDING GEAR MAIN LANDING GEAR LANDING GEAR GROUNDING (EARTHING) POINT GROUNDING (EARTHING) CABLE A TYPICAL N_AC_050402_1_0030101_01_01 Ground Service Connections Grounding (Earthing) Points - Landing Gear FIGURE-5-4-2-991-003-A01 5-4-2 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A A RIB20 RIB19 B A FOR SPECIFICATIONS REFER TO FLIGHT MANUAL NOTE: R SIDE SYMMETRICAL B F W D N_AC_050402_1_0040101_01_00 Ground Service Connections Grounding (Earthing) Points - Wing (If Installed) FIGURE-5-4-2-991-004-A01 5-4-2 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FR14 FR12 FR12 A FR14 Z822 PR ES S B C A A/C STRUCTURE GROUNDING (EARTHING) POINT GROUNDING (EARTHING) CABLE B FWD C N_AC_050402_1_0120101_01_00 Ground Service Connections Grounding (Earthing) Point - Avionics Compartment Door-Frame FIGURE-5-4-2-991-012-A01 5-4-2 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A PHONE JACK GROUNDING (EARTHING) POINT A N_AC_050402_1_0130101_01_00 Ground Service Connections Grounding (Earthing) Point - Engine Air Intake (If Installed) FIGURE-5-4-2-991-013-A01 5-4-2 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-3 Hydraulic System **ON A/C A319-100 A319neo Hydraulic System 1. Access DISTANCE FROM AIRCRAFT CENTERLINE ACCESS Green System: Access Door 197CB Yellow System: Access Door 198CB Blue System: Access Door 197EB 2. AFT OF NOSE 17.57 m (57.64 ft) 17.57 m (57.64 ft) 18.92 m (60.07 ft) RH SIDE 1.27 m (4.17 ft) - - 1.27 m (4.17 ft) 1.27 m (4.17 ft) - Reservoir Pressurization DISTANCE FROM AIRCRAFT CENTERLINE ACCESS AFT OF NOSE 14.05 m (46.10 ft) Access Door 195BB 3. LH SIDE MEAN HEIGHT FROM GROUND 1.76 m (5.77 ft) 1.76 m (5.77 ft) 1.76 m (5.77 ft) LH SIDE 0.25 m (0.82 ft) RH SIDE - MEAN HEIGHT FROM GROUND 1.74 m (5.71 ft) Accumulator Charging Four MIL-PRF-6164 connections: ACCESS Yellow System Accumulator: Access Door 196BB DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE 14.05 m (46.10 ft) LH SIDE - RH SIDE 0.25 m (0.82 ft) 5-4-3 MEAN HEIGHT FROM GROUND 1.74 m (5.71 ft) Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING ACCESS Green System Accumulator: Left MLG Door Blue System Accumulator: Access Door 195BB Yellow System Braking Accumulator: Access Door 196BB 4. DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE LH SIDE RH SIDE MEAN HEIGHT FROM GROUND 15.67 m (51.41 ft) 0.25 m (0.82 ft) - 3.20 m (10.50 ft) 14.05 m (46.10 ft) 0.25 m (0.82 ft) - 1.74 m (5.71 ft) 14.05 m (46.10 ft) - 0.25 m (0.82 ft) 1.74 m (5.71 ft) Reservoir Filling Centralized filling capability on the Green System ground service panel: ACCESS Access Door 197CB DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE 17.57 m (57.64 ft) LH SIDE 1.27 m (4.17 ft) RH SIDE - MEAN HEIGHT FROM GROUND 1.76 m (5.77 ft) Filling: Ground pressurized supply or hand pump. 5. Reservoir Drain Three 3/8 in. self-sealing connections: ACCESS Yellow System: Access Door 196BB Green System: Left MLG Door DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE 14.05 m (46.10 ft) 15.67 m (51.41 ft) LH SIDE RH SIDE - 0.25 m (0.82 ft) 0.25 m (0.82 ft) - 5-4-3 MEAN HEIGHT FROM GROUND 1.74 m (5.71 ft) 3.20 m (10.50 ft) Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING ACCESS Blue System: Access Door 197EB DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE 18.92 m (62.07 ft) LH SIDE 1.27 m (4.17 ft) RH SIDE - MEAN HEIGHT FROM GROUND 1.76 m (5.77 ft) NOTE : The drain valve is on the Blue System ground service panel for the reservoir of the Blue hydraulic system. The drain valve is on the reservoir for the Green and Yellow Hydraulic Systems. 6. Ground Test On each ground service panel: - One self-sealing connector (suction). - One self-sealing connector (delivery). 5-4-3 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A FR47 FR50 197CB RESERVOIR FILL SYSTEM HAND PUMP FILL CONNECTION RESERVOIR FILL SYSTEM SELECTOR VALVE QUANTITY INDICATOR RESERVOIR DEPRESSURIZATION CONNECTION GROUND DELIVERY CONNECTION GROUND SUPPLY RESERVOIR FILL CONNECTION A FWD GROUND SUCTION CONNECTION N_AC_050403_1_0040101_01_01 Hydraulic System Green System Ground Service Panel FIGURE-5-4-3-991-004-A01 5-4-3 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A FR47 FR50 RESERVOIR DEPRESSURIZATION VALVE 197EB GROUND DELIVERY CONNECTION GROUND SUCTION CONNECTION RESERVOIR DRAIN VALVE A FWD N_AC_050403_1_0050101_01_01 Hydraulic System Blue System Ground Service Panel FIGURE-5-4-3-991-005-A01 5-4-3 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FR47 198CB A FR50 GROUND DELIVERY CONNECTION RESERVOIR DEPRESSURIZATION VALVE GROUND SUCTION CONNECTION HAND PUMP LEVER A FWD N_AC_050403_1_0060101_01_01 Hydraulic System Yellow System Ground Service Panel FIGURE-5-4-3-991-006-A01 5-4-3 Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-4 Electrical System **ON A/C A319-100 A319neo Electrical System 1. Electrical System This chapter gives data related to the location of the ground service connections. ACCESS A/C External Power: Access Door 121AL AFT OF NOSE 2.55 m (8.37 ft) DISTANCE FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE MEAN HEIGHT FROM GROUND On centerline 2.00 m (6.56 ft) NOTE : Distances are approximate. 2. Technical Specifications A. External Power Receptacle: - One receptacle according to MS 90362-3 (without shield MS 17845-1) -- 90 kVA. NOTE : Make sure that for connectors featuring micro switches, the connector is chamfered to properly engage in the receptacle. B. Power Supply: - Three-phase, 115/200V, 400 Hz. C. Electrical Connectors for Servicing: - AC outlets: HUBBELL 5258 - DC outlets: HUBBELL 7472. D. Electrical Loads in Ground Configuration In ground configuration, in addition to the power necessary for maintenance, all the circuits, except those which are connected to the engines, are supplied as in flight. In these conditions, the maximum power on ground is approximately 75 kVA. This value does not take into account the supply of the galleys and IFE, which according to the aircraft interior layout, may reach 30 kVA. E. Electrical Power necessary for Maintenance at Line Stop and Workshops: - Hydraulic electric-pumps: 34 kVA - Air conditioning/ventilation: 20.8 kVA - Fuel pumps: 12 kVA - Lighting (commercial): 6.7 kVA - Lighting (technical): 3 kVA - Ice and rain protection: 3 kVA - Cargo loading: 3 kVA 5-4-4 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING - AFS, flight controls, ADS, recorders: 3.3 kVA Communications: 1.3 kVA Radio navigation: 1.2 kVA. 5-4-4 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A 121AL 108VU A N_AC_050404_1_0010101_01_01 Ground Service Connections External Power Receptacles FIGURE-5-4-4-991-001-A01 5-4-4 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-5 Oxygen System **ON A/C A319-100 A319neo Oxygen System 1. Oxygen System DISTANCE FROM AIRCRAFT CENTERLINE ACCESS Oxygen Replenishment: Access Door 812 2. AFT OF NOSE 3.45 m (11.32 ft) LH SIDE RH SIDE 1.15 m (3.77 ft) - MEAN HEIGHT FROM GROUND 2.60 m (8.53 ft) Technical Specifications - One 3/8 in. MIL-DTL 7891 standard service connection. NOTE : External charging in the avionics compartment. 5-4-5 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo OXYGEN STORAGE CYLINDER FR16 FR9 B Z125 812 A FR12 A FR9 C B OXYGEN FILLING PORT OXYGEN FILLING INDICATOR TEST PORT C N_AC_050405_1_0010101_01_00 Ground Service Connections Oxygen System FIGURE-5-4-5-991-001-A01 5-4-5 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-6 Fuel System **ON A/C A319-100 A319neo Fuel System 1. Refuel/Defuel Control Panel ACCESS Refuel/Defuel Integrated Panel: Access Door 192MB 2. AFT OF NOSE DISTANCE POSITION FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE 14.8 m (48.56 ft) - 1.8 m (5.91 ft) MEAN HEIGHT FROM GROUND 1.8 m (5.91 ft) Refuel/Defuel Connectors ACCESS Refuel/Defuel Coupling, Left: Access Panel 522HB (Optional) Refuel/Defuel Coupling, Right: Access Panel 622HB Overwing GravityRefuel Cap AFT OF NOSE DISTANCE POSITION FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE MEAN HEIGHT FROM GROUND 15.99 m (52.46 ft) 9.83 m (32.25 ft) - 3.65 m (11.98 ft) 15.99 m (52.46 ft) - 9.83 m (32.25 ft) 3.65 m (11.98 ft) 17.5 m (57.41 ft) 12.4 m (40.68 ft) 12.4 m (40.68 ft) 3.7 m (12.14 ft) A. Refuel/Defuel Couplings: - Right wing: one standard ISO 45, 2.5 in. - Left wing: one optional standard ISO 45, 2.5 in. B. Refuel Pressure: - Maximum pressure: 3.45 bar (50 psi). C. Average Flow Rate: - 1250 l/min (330 US gal/min). 5-4-6 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 3. Overpressure Protectors and NACA Vent Intake ACCESS Surge Tank OverpressureProtector: Access Panel 550CB (650CB) Inner Cell OverpressureProtector: Access Panel 540HB (640HB) NACA Vent Intake: Access Panel 550AB (650AB) AFT OF NOSE DISTANCE POSITION FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE MEAN HEIGHT FROM GROUND 18.76 m (61.55 ft) 14.9 m (48.88 ft) 14.9 m (48.88 ft) 4.32 m (14.17 ft) 17.5 m (57.41 ft) 9.19 m (30.15 ft) 9.19 m (30.15 ft) 4.1 m (13.45 ft) 18.2 m (59.71 ft) 13.7 m (44.95 ft) 13.7 m (44.95 ft) 4.02 m (13.19 ft) NOTE : Distances are approximate. 5-4-6 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A REFUEL/DEFUEL CONTROL PANEL FUEL QTY kg x 1000 LEFT RIGHT CTR LVL HI LEFT RIGHT CTR VALVES REFUEL OPEN OPEN OPEN NORM NORM NORM SHUT SHUT MODE SELECT SHUT TEST BATT POWER HI LVL ON REFUEL OFF DEFUEL / XFR OPEN LTS ACTUAL REFUEL PRESELECTED NORM kg x 1000 DEC CKPT INC END A NOTE: STANDARD CONFIGURATION OF REFUEL/DEFUEL PANEL. N_AC_050406_1_0010101_01_00 Ground Service Connections Refuel/Defuel Control Panel FIGURE-5-4-6-991-001-A01 5-4-6 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo RIB14 RIB15 A LEADING EDGE WING FRONT SPAR 40QM 41QM A N_AC_050406_1_0020101_01_00 Ground Service Connections Refuel/Defuel Couplings FIGURE-5-4-6-991-002-A01 5-4-6 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo RIB19 A RIB20 ADAPTER (REF ONLY) GROUND CONNECTION (REF ONLY) 44QM (45QM) F W D A N_AC_050406_1_0030101_01_00 Ground Service Connections Overwing Gravity-Refuel Cap (If Installed) FIGURE-5-4-6-991-003-A01 5-4-6 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo Z500 (Z600) C 540HB (640HB) A 550AB (650AB) 550CB (650CB) B RIB14 RIB13 RIB22 RIB23 RIB25 RIB24 NACA VENT PROTECTOR NACA VENT INTAKE A 01 OVERPRESSURE PROTECTOR NOTE: 01 LH SHOWN, RH SYMMETRICAL B C 01 N_AC_050406_1_0040101_01_01 Ground Service Connections Overpressure Protectors and NACA Vent Intake FIGURE-5-4-6-991-004-A01 5-4-6 Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-7 Pneumatic System **ON A/C A319-100 A319neo Pneumatic System 1. High Pressure Air Connector ACCESS HP Connector: Access Door 191DB A. 2. AFT OF NOSE 11.38 m (37.34 ft) DISTANCE FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE 0.84 m (2.76 ft) MEAN HEIGHT FROM GROUND 1.76 m (5.77 ft) Connector: - One standard 3 in. ISO 2026 connection. Low Pressure Air Connector ACCESS LP Connector: Access Door 191CB A. AFT OF NOSE 10.85 m (35.6 ft) DISTANCE FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE 1.11 m (3.64 ft) MEAN HEIGHT FROM GROUND 1.73 m (5.68 ft) Connector: - One standard 8 in. SAE AS4262 connection. 5-4-7 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FR34 FR36 B A 191CB 191DB HP CONNECTOR A LP CONNECTOR B N_AC_050407_1_0010101_01_00 Ground Service Connections LP and HP Ground Connectors FIGURE-5-4-7-991-001-A01 5-4-7 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-8 Oil System **ON A/C A319-100 A319neo Oil System **ON A/C A319-100 1. Engine Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-8-991-003-A): One gravity filling cap and one pressure filling connection per engine. ACCESS Engine Oil Gravity Filling Cap: Access door: 437BL (LH), 447BL (RH) Engine Oil Pressure Filling Port: DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE ENGINE 1 (LH) ENGINE 2 (RH) MEAN HEIGHT FROM GROUND 11.56 m (37.93 ft) 6.63 m (21.75 ft) 4.82 m (15.81 ft) 1.46 m (4.79 ft) 11.40 m (37.40 ft) 6.49 m (21.29 ft) 4.74 m (15.55 ft) 1.42 m (4.66 ft) NOTE : Distances are approximate. A. Tank capacity: - Full level: 19.6 l (5 US gal), - Usable: 9.46 l (3 US gal). B. Maximum delivery pressure required: 1.72 bar (25 psi). Maximum delivery flow required: 180 l/h (48 US gal/h). 2. IDG Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-8-991-004-A): One pressure filling connection per engine: OMP 2506-18 plus one connection overflow: OMP 2505-18. DISTANCE FROM AIRCRAFT CENTERLINE MEAN HEIGHT ACCESS AFT OF NOSE FROM ENGINE 1 (LH) ENGINE 2 (RH) GROUND IDG Oil Pressure Filling Connection: 10.60 m 6.90 m 5.52 m 0.68 m Access door: 438AR (34.78 ft) (22.64 ft) (18.11 ft) (2.23 ft) (LH), 448AR (RH) 5-4-8 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING NOTE : Distances are approximate. 3. A. Tank capacity: 5 l (1 US gal). B. Delivery pressure required: 0.34 bar (5 psi) to 2.76 bar (40 psi) at the IDG inlet. Starter Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-8-991-005-A): One gravity filling cap per engine. ACCESS Starter Oil Filling Connection: DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE 11.40 m (37.40 ft) ENGINE 1 (LH) 5.30 m (17.39 ft) ENGINE 2 (RH) 6.20 m (20.34 ft) MEAN HEIGHT FROM GROUND 0.76 m (2.49 ft) NOTE : Distances are approximate. A. 4. Tank capacity: 0.8 l (0.21 US gal). Engine Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-8-991-006-B): One gravity filling cap per engine. ACCESS DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE Engine Oil Gravity Filling Cap: 10.64 m Access door: 437BL (34.91 ft) (LH), 447BL (RH) ENGINE 1 (LH) 6.56 m (21.52 ft) ENGINE 2 (RH) 4.92 m (16.14 ft) MEAN HEIGHT FROM GROUND 1.22 m (4.00 ft) NOTE : Distances are approximate. A. 5. Tank capacity: - Full level: 28 l (7 US gal), - Usable: 23.50 l (6 US gal). IDG Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-8-991-007-B): One pressure filling connection per engine: OMP 2506-2 plus one overflow connection: OMP 2505-2. 5-4-8 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING DISTANCE FROM AIRCRAFT CENTERLINE ACCESS IDG Oil Pressure Filling Connection: AFT OF NOSE 11.04 m (36.22 ft) ENGINE 1 (LH) 5.30 m (17.39 ft) ENGINE 2 (RH) 6.14 m (20.14 ft) MEAN HEIGHT FROM GROUND 0.75 m (2.46 ft) NOTE : Distances are approximate. A. 6. Tank capacity: 4.10 l (1 US gal). Starter Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-8-991-008-B): One gravity filling cap per engine. DISTANCE FROM AIRCRAFT CENTERLINE ACCESS Starter Oil Filling Connection: AFT OF NOSE 11.04 m (36.22 ft) ENGINE 1 (LH) 5.30 m (17.39 ft) ENGINE 2 (RH) 6.14 m (20.14 ft) MEAN HEIGHT FROM GROUND 0.75 m (2.46 ft) NOTE : Distances are approximate. A. Tank capacity: 0.35 l (0.09 US gal). **ON A/C A319-100 A319neo 7. APU Oil System (See FIGURE 5-4-8-991-009-A): APU oil gravity filling cap. ACCESS GTCP 36-300 APS 3200 131-9 DISTANCE FROM AIRCRAFT CENTERLINE AFT OF NOSE 31.76 m (104.20 ft) 31.76 m (104.20 ft) 31.66 m (103.87 ft) ENGINE 1 (LH) 0.30 m (0.98 ft) 0.30 m (0.98 ft) 0.35 m (1.15 ft) ENGINE 2 (RH) - MEAN HEIGHT FROM GROUND 4.83 m (15.85 ft) 4.78 m (15.68 ft) 4.32 m (14.17 ft) NOTE : Distances are approximate. 5-4-8 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING A. Tank capacity (usable): - APU type GTCP 36-300: 6.20 l (2 US gal), - APU type APS 3200: 5.40 l (1 US gal), - APU type 131-9: 6.25 l (2 US gal). 5-4-8 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A B 437BL (ENGINE 1) 447BL (ENGINE 2) FWD A OIL IN VENT OIL LEVEL TRANSMITTER (OPTIONAL) ANTI−SIPHON DEVICE OIL CAP AIR PRESSURE SWITCH NIPPLE SIGHT WINDOW PRESSURE NIPPLE SELF−SEALING MAGNETIC DRAIN PLUG OIL OUT SERVO FUEL HEATER OIL/FUEL HEAT EXCHANGER B N_AC_050408_1_0030101_01_00 Ground Service Connections Engine Oil Tank -- CFM56 Series Engine FIGURE-5-4-8-991-003-A01 5-4-8 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 B A 1 − PRESSURE FILL VALVE 2 − CASE DRAIN PLUG 3 − DUST CAP 4 − DUST CAP 5 − OVERFLOW DRAIN VALVE 1 5 A OVER FULL 2 4 3 B ADD OIL ADD OIL CFM−56 SIGHT GLASS B C A NOTE: A IF THE OIL LEVEL IS ABOVE THE YELLOW BAND, OIL SERVICING IS REQUIRED. B IF THE OIL LEVEL IS WITHIN THE GREEN AND YELLOW BANDS, OIL SERVICING IS NOT REQUIRED. C IF THE OIL LEVEL IS BELOW THE GREEN BAND, OIL SERVICING IS REQUIRED. N_AC_050408_1_0040101_01_00 Ground Service Connections IDG Oil Tank -- CFM56 Series Engine FIGURE-5-4-8-991-004-A01 5-4-8 Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A STARTER DRAIN PORT AND MAGNETIC PLUG OVERFLOW PLUG OIL FILLER PLUG A N_AC_050408_1_0050101_01_00 Ground Service Connections Starter Oil Tank -- CFM56 Series Engine FIGURE-5-4-8-991-005-A01 5-4-8 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A 437BL (ENGINE 1) 447BL (ENGINE 2) FCOC GRAVITY FILLER CAP B PRISMALITE LEVEL INDICATOR OIL TANK FWD A ’FULL’ LEVEL NOTCH 27.3 LT 29.0 US QTS 6.0 IMP GAL (WITHIN 60 MIN FROM SHUTDOWN) NOTCH ’2’ 23 LT 24 US QTS 5.1 IMP GAL NOTCH ’1’ 26 LT 27 US QTS 5.7 IMP GAL NOTCH ’3’ 20 LT 22 US QTS 4.5 IMP GAL B N_AC_050408_1_0060201_01_00 Ground Service Connections Engine Oil Tank -- IAE V2500 Series Engine FIGURE-5-4-8-991-006-B01 5-4-8 Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 IDG B A PRESSURE FILL VALVE OVER FLOW DRAIN VALVE OIL LEVEL INDICATOR DUST CAP OVER FULL ADD OIL DUST CAP PRESSURE FILL HOSE OVER FLOW DRAIN HOSE ADD OIL OVER FULL ADD OIL CORRECTLY FILLED IDG ADD OIL V2500 V2500 A B B AFTER ENGINE SHUTDOWN (HOT OIL/IDG) AFTER SERVICING OR ENGINE SHUTDOWN (COLD OIL/IDG) OIL LEVEL CAN BE IN THE GREEN BAND OR THE YELLOW BAND OIL LEVEL MUST BE AT OR NEAR THE LINE BETWEEN THE YELLOW BAND AND THE GREEN BAND INCORRECTLY FILLED IDG ADD OIL OVER FULL OVER FULL OVER FULL ADD OIL ADD OIL ADD OIL ADD OIL V2500 V2500 V2500 ADD OIL B B AFTER SERVICING OR ENGINE SHUTDOWN (COLD OIL/IDG) AT ALL TIMES (HOT OR COLD OIL/IDG) THE OIL LEVEL MUST NOT BE IN THE YELLOW BAND BUT IT CAN BE IMMEDIATELY ABOVE THE LOWER LIMIT OF THE YELLOW BAND BECAUSE OF THE AIRCRAFT RAMP ANGLE DO THE IDG SERVICING TO GET THE CORRECT IDG OIL LEVEL. THE OIL LEVEL MUST NOT BE IN THE RED BAND PERFORM IDG OIL SERVICING TO GET THE CORRECT IDG OIL LEVEL. DO NOT USE THE OVERFLOW DRAIN HOSE TO GET THE CORRECT IDG OIL LEVEL. N_AC_050408_1_0070201_01_00 Ground Service Connections IDG Oil Tank -- IAE V2500 Series Engine FIGURE-5-4-8-991-007-B01 5-4-8 Page 9 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 * THE STARTER IS FULL WHEN THE OIL LEVEL SHOWS NOT LESS THAN 3/4 FULL ON THE SIGHT GLASS A * B EXTERNAL GEARBOX OIL FILLING POINT ADAPTER B SIGHT GLASS PNEUMATIC STARTER OIL OVERFLOW POINT A N_AC_050408_1_0080201_01_00 Ground Service Connections Starter Oil Tank -- IAE V2500 Series Engine FIGURE-5-4-8-991-008-B01 5-4-8 Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo FR84 A Z315 (Z316) FR80 GRAVITY OIL FILLER OIL LEVEL SIGHT GLASS PRESSURE FILL PORT OVERFLOW DRAIN VALVE A N_AC_050408_1_0090101_01_00 Ground Service Connections APU Oil Tank FIGURE-5-4-8-991-009-A01 5-4-8 Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-9 Potable Water System **ON A/C A319-100 A319neo Potable Water System 1. Potable Water Ground Service Panels ACCESS Potable-Water Service Panel: Access Door 171AL Potable-Water Drain Panel: Access Door 133AL AFT OF NOSE DISTANCE POSITION FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE MEAN HEIGHT FROM GROUND 27.5 m (90.22 ft) 0.3 m (0.98 ft) - 2.6 m (8.53 ft) 11.8 m (38.71 ft) 0.15 m (0.49 ft) - 1.75 m (5.74 ft) NOTE : Distances are approximate. 2. Technical Specifications A. Connectors: (1) On the potable-water service panel (Access Door 171AL) - Fill/Drain Nipple 3/4 in. (ISO 17775). - One ground air-pressure connector. (2) On the potable-water drain panel (Access Door 133AL) - Drain Nipple 3/4 in. (ISO 17775). B. Usable capacity: - Standard configuration - one tank: 200 l (53 US gal). C. Filling pressure: - 3.45 bar (50 psi). D. Typical flow rate: - 50 l/min (13 US gal/min). 5-4-9 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A FR29 DRAIN CONTROL HANDLE 133AL B 171AL FR28 DRAIN PORT FILL/DRAIN CONTROL HANDLE OVERFLOW PORT A POTABLE−WATER DRAIN PANEL FR66 FR65 FILL/DRAIN PORT GROUND AIR−PRESSURE CONNECTION B POTABLE−WATER SERVICE PANEL N_AC_050409_1_0290101_01_00 Ground Service Connections Potable Water Ground Service Panels FIGURE-5-4-9-991-029-A01 5-4-9 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A B FR68 Z170 FR65 A POTABLE WATER TANK FILL/DRAIN LINE OVERFLOW LINE POTABLE WATER DISTRIBUTION LINE B N_AC_050409_1_0300101_01_00 Ground Service Connections Potable Water Tank Location FIGURE-5-4-9-991-030-A01 5-4-9 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-4-10 Waste Water System **ON A/C A319-100 A319neo Vacuum Toilet System 1. Vacuum Toilet System ACCESS DISTANCE POSITION FROM AIRCRAFT CENTERLINE LH SIDE RH SIDE AFT OF NOSE Waste-Water 27.5 m Ground Service (90.22 ft) Panel: Access door 172AR - 0.8 m (2.62 ft) MEAN HEIGHT FROM GROUND 2.8 m (9.19 ft) NOTE : Distances are approximate. 2. Technical Specifications A. Connectors: - Draining: 4 in. (ISO 17775). - Flushing and filling: 1 in. (ISO 17775). B. Usable waste tank capacity: - Standard configuration - one tank: 177 l (47 US gal). C. Waste tank - Rinsing: - Operating pressure: 3.45 bar (50 psi). D. Waste tank - Precharge: - 10 l (3 US gal). 5-4-10 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A Z172 FR66 FR65 FILL AND RINSE CONNECTION TOILET DRAIN CONNECTION A N_AC_050410_1_0010101_01_00 Ground Service Connections Waste Water Ground Service Panel FIGURE-5-4-10-991-001-A01 5-4-10 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo A Z170 FR68 WASTE TANK FR65 FLUSH LINE DRAIN LINE A N_AC_050410_1_0040101_01_00 Ground Service Connections Waste Tank Location FIGURE-5-4-10-991-004-A01 5-4-10 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-5-0 Engine Starting Pneumatic Requirements **ON A/C A319-100 A319neo Engine Starting Pneumatic Requirements 1. The purpose of this section is to provide the minimum air data requirements at the aircraft connection, needed to start the engine within no more than 60 seconds, at sea level (0 feet), for a set of Outside Air Temperatures (OAT). ABBREVIATION A/C ASU HPGC OAT DEFINITION Aircraft Air Start Unit High Pressure Ground Connection Outside Air Temperature A. Air data (discharge temperature, absolute discharge pressure) are given at the HPGC. B. For a given OAT the following charts are used to determine an acceptable combination for air discharge temperature, absolute discharge pressure and mass flow rate. C. This section addresses requirements for the ASU only, and is not representative of the start performance of the aircraft using the APU or engine cross bleed procedure. D. To protect the A/C, the charts feature, if necessary: - The maximum discharge pressure at the HPGC - The maximum discharge temperature at the HPGC. 5-5-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo CFM56 SERIES/SEA LEVEL STARTING TIME: LESS THAN 60 s AIR DATA AT AIRCRAFT CONNECTION 70 65 140 60 130 55 120 50 110 AIRFLOW (lb/min) AIRFLOW (kg/min) 150 100 45 45 ABSOLUTE PRESSURE (psia) 40 50 ABSOLUTE PRESSURE (psia) 50 45 40 −45 −35 −40 −5 5 15 25 35 −25 −15 OUTSIDE AIR TEMPERATURE OAT (° C) −20 100 0 20 40 60 80 OUTSIDE AIR TEMPERATURE OAT (° F) 45 55 120 ASU DISCHARGE TEMPERATURE: 100° C (212° F) 150° C (302° F) 220° C (428° F) MAX. EXAMPLE: FOR AN OAT OF 20° C (68° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 150° C (302° F) AT HPGC: − THE REQUIRED PRESSURE AT HPGC IS 42 psia − THE REQUIRED AIRFLOW AT A/C CONNECTION IS 55 kg/min. NOTE: IN CASE THE ACTUAL DISCHARGE TEMPERATURE OF THE ASU DIFFERS SUBSTANTIALLY FROM THE ONES GIVEN IN THE CHARTS, A SIMPLE INTERPOLATION (LINEAR) IS SUFFICIENT TO DETERMINE THE REQUIRED AIR DATA. N_AC_050500_1_0080101_01_00 Example for Use of the Charts FIGURE-5-5-0-991-008-A01 5-5-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 IAE V2500 SERIES/SEA LEVEL STARTING TIME: LESS THAN 60 s AIR DATA AT AIRCRAFT CONNECTION 85 180 80 160 70 150 65 140 60 130 55 120 50 110 AIRFLOW (lb/min) AIRFLOW (kg/min) 170 75 100 45 35 45 40 50 55 60 65 ABSOLUTE PRESSURE (psia) ABSOLUTE PRESSURE (psia) 65 60 55 50 45 40 35 −50 −40 −30 −20 −10 0 10 20 30 40 50 60 120 140 OUTSIDE AIR TEMPERATURE OAT (° C) −40 −20 0 20 40 60 80 100 OUTSIDE AIR TEMPERATURE OAT (° F) ASU DISCHARGE TEMPERATURE: 100° C (212° F) 150° C (302° F) 220° C (428° F) MAX. N_AC_050500_1_0090101_01_00 Engine Starting Pneumatic Requirements IAE V2500 Series Engine FIGURE-5-5-0-991-009-A01 5-5-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo CFM56 SERIES AND CFM LEAP−1A NEO/SEA LEVEL STARTING TIME: LESS THAN 60 s AIR DATA AT AIRCRAFT CONNECTION 70 150 140 60 130 55 120 50 110 AIRFLOW (lb/min) AIRFLOW (kg/min) 65 100 45 45 40 50 ABSOLUTE PRESSURE (psia) ABSOLUTE PRESSURE (psia) 50 45 40 −45 −35 −25 −15 −5 5 15 25 45 35 55 OUTSIDE AIR TEMPERATURE OAT (° C) −40 −20 0 20 40 60 80 100 120 OUTSIDE AIR TEMPERATURE OAT (° F) ASU DISCHARGE TEMPERATURE: 100° C (212° F) 150° C (302° F) 220° C (428° F) MAX. N_AC_050500_1_0100101_01_00 Engine Starting Pneumatic Requirements CFM56 Series and CFM LEAP-1A NEO Engine FIGURE-5-5-0-991-010-A01 5-5-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo PW 1100G NEO/SEA LEVEL STARTING TIME: LESS THAN 60 s AIR DATA AT AIRCRAFT CONNECTION 80 170 160 70 150 65 140 60 AIRFLOW (lb/min) AIRFLOW (kg/min) 75 130 55 45 40 55 50 ABSOLUTE PRESSURE (psia) ABSOLUTE PRESSURE (psia) 55 50 45 40 −45 −35 −25 −15 −5 5 15 25 35 45 OUTSIDE AIR TEMPERATURE OAT (° C) −40 −20 0 20 40 60 80 100 OUTSIDE AIR TEMPERATURE OAT (° F) ASU DISCHARGE TEMPERATURE: 100° C (212° F) 150° C (302° F) 220° C (428° F) MAX. N_AC_050500_1_0110101_01_00 Engine Starting Pneumatic Requirements PW 1100G NEO Engine FIGURE-5-5-0-991-011-A01 5-5-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-6-0 Ground Pneumatic Power Requirements **ON A/C A319-100 A319neo Ground Pneumatic Power Requirements 1. General This section describes the required performance for the ground equipment to maintain the cabin temperature at 27 ˚C (80.6 ˚F) after boarding (Section 5.7 - steady state), and provides the time needed to cool down or heat up the aircraft cabin to the required temperature (Section 5.6 - dynamic cases with aircraft empty). ABBREVIATION A/C AHM AMM GC GSE IFE OAT PCA A. DEFINITION Aircraft Aircraft Handling Manual Aircraft Maintenance Manual Ground Connection Ground Service Equipment In-Flight Entertainment Outside Air Temperature Pre-Conditioned Air The air flow rates and temperature requirements for the GSE, provided in Sections 5.6 and 5.7, are given at A/C ground connection. NOTE : The cooling capacity of the equipment (kW) is only indicative and is not sufficient by itself to ensure the performance (outlet temperature and flow rate combinations are the requirements needed for ground power). An example of cooling capacity calculation is given in Section 5.7. NOTE : The maximum air flow is driven by pressure limitation at the ground connection. B. 2. For temperatures at ground connection below +2 ˚C (+35.6 ˚F) (Subfreezing), the ground equipment shall be compliant with the Airbus document ”Subfreezing PCA Carts - Compliance Document for Suppliers” (contact Airbus to obtain this document) defining all the requirements with which Subfreezing Pre-Conditioning Air equipment must comply to allow its use on Airbus aircraft. These requirements are in addition to the functional specifications included in the IATA AHM997. Ground Pneumatic Power Requirements This section provides the ground pneumatic power requirements for: - Heating (pull up) the cabin, initially at OAT, up to 21 ˚C (69.8 ˚F) (see FIGURE 5-6-0-991-001-A) - Cooling (pull down) the cabin, initially at OAT, down to 27 ˚C (80.6 ˚F) (see FIGURE 5-6-0-991-002-A). 5-6-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo PULL UP PERFORMANCE AIRFLOW AT GC (kg/s) 3.0 MAXIMUM AIRFLOW 1.3 1.2 2.5 1.1 1.0 2.0 0.9 0.8 0.7 1.5 0.6 0.5 AIRFLOW AT GC (lb/s) 1.4 1.0 0.4 15 30 45 60 75 90 TIME TO HEAT CABIN TO +21° C (+69.8° F) ON GROUND (min) OAT ISA −38° C (−36.4° F); GC INLET +70° C (+158° F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON N_AC_050600_1_0010101_01_00 Ground Pneumatic Power Requirements Heating FIGURE-5-6-0-991-001-A01 5-6-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo PULL DOWN PERFORMANCE 3.0 MAXIMUM AIRFLOW 1.3 AIRFLOW AT GC (lb/s) AIRFLOW AT GC (kg/s) 1.4 1.2 2.5 1.1 1.0 2.0 0.9 0.8 0.7 1.5 0.6 30 45 60 75 90 105 120 TIME TO COOL CABIN TO +27° C (+80.6° F) ON GROUND (min) OAT ISA +23° C (+73.4° F); GC INLET +2° C (+35.6° F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON OAT ISA +23° C (+73.4° F); GC INLET −10° C (+14° F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON N_AC_050600_1_0020101_01_00 Ground Pneumatic Power Requirements Cooling FIGURE-5-6-0-991-002-A01 5-6-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-7-0 Preconditioned Airflow Requirements **ON A/C A319-100 A319neo Preconditioned Airflow Requirements 1. This section provides the preconditioned airflow rate and temperature needed to maintain the cabin temperature at 27 ˚C (80.6 ˚F). These settings are not intended to be used for operation (they are not a substitute for the settings given in the AMM). They are based on theoretical simulations and give the picture of a real steady state. The purpose of the air conditioning operation (described in the AMM) is to maintain the cabin temperature below 27 ˚C (80.6 ˚F) during boarding (therefore it is not a steady state). 5-7-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo COOLING/HEATING PERFORMANCE 1.4 3.0 MAXIMUM AIRFLOW 1.2 MAXIMUM AIRFLOW 1.0 H SETTINGS NOT INTENDED TO BE USED FOR OPERATION C 2.0 0.8 AIRFLOW AT GC (lb/s) AIRFLOW AT GC (kg/s) 2.5 1.5 0.6 1.0 0.4 −10 −5 20 0 30 2 5 10 15 20 INLET TEMPERATURE AT GC (° C) 40 50 60 70 25 30 80 35 90 INLET TEMPERATURE AT GC (° F) OAT ISA +23° C (73.4° F); EMPTY CABIN; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON; GALLEYS ON OAT ISA −38° C (−36.4° F); EMPTY CABIN; IFE OFF; LIGHTS ON; NO SOLAR LOAD; RECIRCULATION FANS ON; GALLEYS OFF EXAMPLE: COOLING CAPACITY CALCULATION: FOR THE CONDITIONS "C", THE COOLING CAPACITY OF 1 kg/s x 1 kJ/(kg.° C) x (27 − 4) = 23 kW (OR 7 TONS COOLING CAPACITY) IS NEEDED TO MAINTAIN THE CABIN TEMPERATURE AT 27° C (80.6° F) (1 kg/s AT 4° C (39.2° F) FOR AIR AT GC INLET). N_AC_050700_1_0010101_01_03 Preconditioned Airflow Requirements FIGURE-5-7-0-991-001-A01 5-7-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-8-0 Ground Towing Requirements **ON A/C A319-100 Ground Towing Requirements 1. This section provides information on aircraft towing. This aircraft is designed with means for conventional or towbarless towing. Information/procedures can be found for both in AMM 09. Status on towbarless towing equipment qualification can be found in SIL 09-002. One towbar fitting is installed at the front of the leg. The main landing gears have attachment points for towing or debogging (for details, refer ARM 07). This section shows the chart to determine the draw bar pull and tow tractor mass requirements as a function of the following physical characteristics: - Aircraft weight, - Number of engines at idle, - Slope. The chart is based on the engine type with the highest idle thrust level. 2. Towbar design guidelines The aircraft towbar shall comply with the following standards: - SAE AS 1614, ”Main Line Aircraft Towbar Attach Fitting Interface”, - SAE ARP 1915, ”Aircraft Towbar”, - ISO 8267-1, ”Aircraft - Towbar Attachment Fitting - Interface Requirements - Part 1: Main Line Aircraft”, - ISO 9667, ”Aircraft Ground Support Equipment - Towbar - Connection to Aircraft and Tractor”, - EN 12312-7, ”Aircraft Ground Support Equipment - Specific Requirements - Part 7: Aircraft Movement Equipment”, - IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Towbar”. A conventional type towbar is required which should be equipped with a damping system (to protect the nose gear against jerks) and with towing shear pins: - A traction shear pin calibrated at 9 425 daN (21 188 lbf), - A torsion pin calibrated at 826 m.daN (6 092 lbf.ft). The towing head is designed according to SAE AS 1614, cat. I. 5-8-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 DRY C ONCRE WET TE = 0.8 CON C RETE HA = RD 0.57 SN OW .2 5.0 5 60 1.5% SLOPE 1 ENGINE ON 70 65 60 55 50 45 40 05 = 0. ICE A/C WEIGHT (x 1 000 kg) BREAKAWAY RESISTANCE 4% # OF ENGINES ON FOR PB: 1 ENGINE THRUST 525 daN =0 DRAWBAR PULL (x 1 000 kg) 10 8.83 0 0 10 20 30 40 50 60 70 80 TOTAL TRACTION WHEEL LOAD (x 1 000 kg) 0 1 2 0 No. OF ENGINES AT IDLE 0.5 1.0 1.5 2.0 SLOPE ( % ) EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A319 AT 60 000 kg, AT 1.5% SLOPE, 1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS: − − − − − − − ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (60 000 kg), FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%), FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 2, FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED No. OF ENGINES (1), FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS, THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5 000 kg), SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (8 830 kg). N_AC_050800_1_0010201_01_04 Ground Towing Requirements FIGURE-5-8-0-991-001-B01 5-8-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 5-9-0 De-Icing and External Cleaning **ON A/C A319-100 A319neo De-Icing and External Cleaning 1. De-Icing and External Cleaning on Ground The mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heights up to approximately 13 m (43 ft). 2. De-Icing AIRCRAFT TYPE A319 A319 Sharklet/neo AIRCRAFT TYPE Wing Top Surface (Both Sides) m2 100 100 ft2 1 076 1 076 Fuselage Top Surface (Top Third - 120˚ Arc) ft2 m2 A319 A319 Sharklet/neo Wingtip Devices (Both Inside and Outside Surfaces) (Both Sides) ft2 m2 2 22 10 108 122 122 1 313 1 313 VTP (Both Sides) HTP Top Surface (Both Sides) m2 27 27 Nacelle and Pylon (Top Third - 120˚ Arc) (All Engines) ft2 m2 258 24 258 24 ft2 291 291 m2 43 43 ft2 463 463 Total De-Iced Area m2 317 325 ft2 3 412 3 498 NOTE : Dimensions are approximate. 3. External Cleaning AIRCRAFT TYPE Wing Top Surface (Both Sides) m2 A319 A319 Sharklet/neo AIRCRAFT TYPE A319 100 100 ft2 1 076 1 076 HTP Top Surface (Both Sides) ft2 m2 291 27 Wing Lower Surface (Including Flap Track Fairing) (Both Sides) m2 ft2 103 1 109 2 103 1 109 10 HTP Lower Surface (Both Sides) ft2 m2 291 27 5-9-0 Wingtip Devices (Both Inside and Outside Surfaces) (Both Sides) m2 ft2 22 108 VTP (Both Sides) ft2 m2 43 463 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING AIRCRAFT TYPE A319 Sharklet/neo AIRCRAFT TYPE A319 A319 Sharklet/neo HTP Top Surface (Both Sides) m2 ft2 27 291 Fuselage and Belly Fairing ft2 m2 374 4 026 374 4 026 VTP (Both Sides) HTP Lower Surface (Both Sides) m2 ft2 27 291 Nacelle and Pylon (All Engines) 2 ft2 m 73 786 73 786 m2 43 ft2 463 Total Cleaned Area m2 750 758 ft2 8 073 8 159 NOTE : Dimensions are approximate. 5-9-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING OPERATING CONDITIONS 6-1-0 Engine Exhaust Velocities and Temperatures **ON A/C A319-100 Engine Exhaust Velocities and Temperatures 1. General This section shows the estimated engine exhaust efflux velocities and temperatures contours for Ground Idle, Breakaway, Maximum Takeoff conditions. 6-1-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power **ON A/C A319-100 Engine Exhaust Velocities Contours - Ground Idle Power 1. This section gives engine exhaust velocities contours at ground idle power. 6-1-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 120 105 AIRPLANE 90 75 10 60 PLAN 30 25 20 30 20 10 0 9 6 3 0 40 12 0 0 m 20 10 METERS 30 6 3 FEET 40 9 m 12 ft ft 45 30 15 0 100 50 0 45 30 25 ELEVATION 20 15 15 45 150 10 200 250 300 GROUND PLANE 350 V (m/s) 400 **ON A/C A319-100 N_AC_060101_1_0030101_01_00 Engine Exhaust Velocities Ground Idle Power -- CFM56 series engine FIGURE-6-1-1-991-003-A01 6-1-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 90 75 30 (9) 60 50 (15) 45 PLAN 100 (30) 15 0 0 20 40 0 5 10 15 m 60 ft 50 0 30 METERS 0 5 FEET 0 20 40 10 15 m 60 ft 100 (30) ELEVATION 100 50 (15) 150 30 (9) 200 VELOCITY = ft/s (m/s) 250 300 **ON A/C A319-100 N_AC_060101_1_0040101_01_00 Engine Exhaust Velocities Ground Idle Power -- IAE V2500 series engine FIGURE-6-1-1-991-004-A01 6-1-1 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power **ON A/C A319-100 Engine Exhaust Temperatures Contours - Ground Idle Power 1. This section gives engine exhaust temperatures contours at ground idle power. 6-1-2 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 120 105 AIRPLANE 75 300 325 400 PLAN 350 30 15 0 45 60 90 400 350 250 100 50 0 40 30 20 10 0 12 9 6 3 0 0 0 m 20 10 METERS 30 6 3 FEET 40 9 m 12 ft ft 400 350 325 ELEVATION 300 150 200 300 GROUND PLANE T (°K) **ON A/C A319-100 N_AC_060102_1_0030101_01_00 Engine Exhaust Temperatures Ground Idle Power -- CFM56 series engine FIGURE-6-1-2-991-003-A01 6-1-2 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 90 75 60 45 PLAN 308 300 0 20 40 60 0 5 10 15 m METERS 0 5 10 FEET 0 20 40 15 m 60 ft ft 325 318 15 0 30 50 0 ELEVATION 318 325 308 300 100 150 200 TEMPERATURE = °K 250 300 **ON A/C A319-100 N_AC_060102_1_0040101_01_00 Engine Exhaust Temperatures Ground Idle Power -- IAE V2500 series engine FIGURE-6-1-2-991-004-A01 6-1-2 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-1-5 Engine Exhaust Velocities Contours - Takeoff Power **ON A/C A319-100 Engine Exhaust Velocities Contours - Takeoff Power 1. This section gives engine exhaust velocities contours at takeoff power. 6-1-5 Page 1 May 01/14 140 120 100 80 60 40 20 0 FEET m 6-1-5 42 36 30 24 18 12 6 0 m 140 120 100 80 60 40 20 0 METERS 42 36 30 24 18 12 6 0 ft ft 60 30 0 90 300 PLAN 200 100 0 ELEVATION 150 500 V = 40 m/s 120 400 V = 40 m/s 180 600 210 700 270 900 AIRPLANE V = 20 m/s 240 800 300 1000 GROUND PLANE V = 20 m/s 330 1100 360 1200 420 1400 V = 12 m/s 390 1300 V = 12 m/s INCLUDES (WORST CASE) GROUND PLANE HEADWIND (20 KTS.) TAKEOFF POWER @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_060105_1_0030101_01_00 Engine Exhaust Velocities Takeoff Power -- CFM56 series engine FIGURE-6-1-5-991-003-A01 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 34 MPH 20 MPH 90 68 MPH 75 102 MPH 60 45 0 20 40 60 0 5 10 15 m METERS 0 FEET 0 20 5 10 15 m 40 60 ft PLAN 136 MPH 15 0 30 300 250 50 0 ft ELEVATION 100 150 200 MAXIMUM TAKEOFF THRUST TO 990 ft (301 m) TO 575 ft (175 m) **ON A/C A319-100 N_AC_060105_1_0040101_01_00 Engine Exhaust Velocities Takeoff Power -- IAE V2500 series engine FIGURE-6-1-5-991-004-A01 6-1-5 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power **ON A/C A319-100 Engine Exhaust Temperatures Contours - Takeoff Power 1. This section gives engine exhaust temperatures contours at takeoff power. 6-1-6 Page 1 May 01/14 40 20 0 12 6 0 6-1-6 40 20 0 6 0 60 12 18 m METERS FEET 60 18 m ft ft 0 10 40 PLAN T = 425°K 20 ELEVATION T = 425°K 20 T = 370°K 60 T = 370°K 80 T = 315°K 30 100 T = 315°K 40 140 AIRPLANE 120 GROUND PLANE 50 160 INCLUDES (WORST CASE): GROUND PLANE HEADWIND (20 KTS.) TAKEOFF POWER @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_060106_1_0030101_01_00 Engine Exhaust Temperatures Takeoff Power -- CFM56 series engine FIGURE-6-1-6-991-003-A01 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 90 75 PLAN 55°C 45°C 0 20 40 60 0 5 10 15 m METERS 0 FEET 0 20 5 10 15 m 40 60 ft ft 65°C 15 0 30 50 0 ELEVATION 100 35°C 45 150 25°C 60 200 250 300 **ON A/C A319-100 N_AC_060106_1_0040101_01_00 Engine Exhaust Temperatures Takeoff Power -- IAE V2500 series engine FIGURE-6-1-6-991-004-A01 6-1-6 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-2-0 Airport and Community Noise **ON A/C A319-100 Airport and Community Noise 1. Airport and Community Noise Data This section gives data concerning engine maintenance run-up noise to permit evaluation of possible attenuation requirements. 6-2-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-2-1 Noise Data **ON A/C A319-100 Noise Data 1. 2. 3. Noise Data for CFM56-5A Series Engine A. Description of test conditions: The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, is centered on the position of the noise reference point. APU: off; ECS: Packs off. B. Engine parameters: 2 engines running C. Meteorological data: The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of the test were as follows: - Temperature: 3˚C (37˚F) - Relative humidity: 66% - Atmospheric pressure: 1 016 hPa - Wind speed: Negligible - No rain. Noise Data for CFM56-5B Series Engine A. Description of test conditions: The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, is centered on the position of the noise reference point. APU: off; ECS: Packs off. B. Engine parameters: 2 engines running C. Meteorological data: The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of the test were as follows: - Temperature: 22˚C (72˚F) - Relative humidity: 42% - Atmospheric pressure: 1 003 hPa - Wind speed: Negligible - No rain. Noise Data for IAE V2500 Series Engine A. Description of test conditions: The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, is centered on the position of the noise reference point. APU: off; ECS: Packs off. B. Engine parameters: 2 engines running 6-2-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING C. Meteorological data: The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of the test were as follows: - Temperature: 27˚C (81˚F) - Relative humidity: 40% - Atmospheric pressure: 1 000 hPa - Wind speed: Negligible - No rain. 6-2-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 GROUND IDLE MAX THRUST POSSIBLE ON BRAKES 20.8% 90% N1 CURVE dB (A) 0° 15° 345° 30° 330° 45° 315° 60° 300° 75° 285° 90° 270° 105° 120° 135° 150° 78 80 82 84 86 88 90 92 94 96 98 100 102 104 106 108 110 112 NOISE REFERENCE POINT 255° 240° 225° 210° N_AC_060201_1_0040101_01_01 Airport and Community Noise CFM56-5A Series Engine FIGURE-6-2-1-991-004-A01 6-2-1 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 POSSIBLE GROUND IDLE MAX THRUST ON BRAKES N1 18.9% 87% CURVE dB (A) 0° 10° 350° 340° 20° 330° 30° 320° 40° 50° 310° 60° 300° 70° 290° 80° 280° 270° 90° 100° 260° 78 80 82 84 86 88 90 92 94 96 98 100 102 104 106 108 110 112 NOISE REFERENCE POINT 110° 120° 130° 140° 150° 250° 240° 230° 220° 210° N_AC_060201_1_0050101_01_01 Airport and Community Noise CFM56-5B Series Engine FIGURE-6-2-1-991-005-A01 6-2-1 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 GROUND IDLE MAX THRUST POSSIBLE ON BRAKES E.P.R 1.012 1.564 N1 25.2% 94.4% CURVE dB (A) 0° 10° 350° 340° 20° 30° 330° 40° 320° 50° 310° 60° 300° 70° 290° 80° 280° 90° 270° 100° 110° 120° 130° 140° 78 80 82 84 86 88 90 92 94 96 98 100 102 104 106 108 110 112 114 NOISE REFERENCE 116 POINT 118 260° 250° 240° 230° 220° 210° 150° N_AC_060201_1_0060101_01_01 Airport and Community Noise IAE V2500 Series Engine FIGURE-6-2-1-991-006-A01 6-2-1 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-3-0 Danger Areas of Engines **ON A/C A319-100 Danger Areas of Engines 1. Danger Areas of the Engines. 6-3-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-3-1 Ground Idle Power **ON A/C A319-100 Ground Idle Power 1. This section gives danger areas of the engines at ground idle power conditions. 6-3-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 RADIUS = 7.2 ft (2.2 m) INLET DANGER AREAS INCLUDE (WORST CASE) GROUND PLANE HEADWIND (20 KTS) INLET HAZARD DIMENSIONS CALCULATED ON 40 ft/sec (12 m/sec) CRITICAL VELOCITY WITH A 3 ft (0.9 m) ADJUSTMENT FOR SAFETY CLOSE ENTRY CORRIDOR FOR WIND DIRECTION > 90° 45° 3.4 ft (1 m) B C NO ENTRY 82 ft (25 m) AFT OF NOZZLE EXIT D NOT TO SCALE WIDTH 72 ft (22 m) E TO 199 ft (61 m) EXHAUST DANGER AREAS INCLUDE (WORST CASE) GROUND PLANE HEADWIND (20 KTS) INLET SUCTION DANGER AREA ENTRY CORRIDOR AREA APPROX. WIND VELOCITY MPH (km/h) A 210−145 (338−233) B 145−105 (233−169) D 105−65 (169−105) 65−20 (105−32) E < 20 (32) C EXHAUST WAKE DANGER AREA 65 MPH (105 km/h) OR GREATER EXHAUST WAKE DANGER AREA 65 MPH (105 km/h) OR LESS POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON "RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIAL WEAPONS PROJECT, NOV. 1951 A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BE COMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR: COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES. A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGE NEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGID STEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY. MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPE AIRCRAFT. LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT BEYOND DANGER AREA N_AC_060301_1_0030101_01_01 Danger Areas of the Engines CFM56 series engine FIGURE-6-3-1-991-003-A01 6-3-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 R = 4.6 m (15 ft) 0.76 m (2.5 ft) 30° TO 235 m (770 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) NOTE: INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER ENTRY CORRIDOR EXHAUST DANGER AREA N_AC_060301_1_0040101_01_01 Danger Areas of the Engines IAE V2500 series engine FIGURE-6-3-1-991-004-A01 6-3-1 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-3-2 Takeoff Power **ON A/C A319-100 Takeoff Power 1. This section gives danger areas of the engines at max. takeoff conditions. 6-3-2 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 INLET DANGER AREAS INCLUDE (WORST CASE) GROUND PLANE HEADWIND (20 KTS) RADIUS = 19.5 ft (5.9 m) INLET HAZARD DIMENSIONS BASED ON 40 ft/sec (12 m/sec) CRITICAL VELOCITY WITH A 3 ft (0.9 m) ADJUSTMENT FOR SAFETY A B NOT TO SCALE NO ENTRY 684 ft (208 m) AFT OF NOZZLE EXIT C D WIDTH 195 ft (59 m) E INLET SUCTION DANGER AREA AREA APPROX. WIND VELOCITY MPH (km/h) A 210−145 (338−233) B 145−105 (233−169) D 105−65 (169−105) 65−20 (105−32) E < 20 (32) C TO 1160 ft (354 m) EXHAUST DANGER AREAS INCLUDE (WORST CASE) GROUND PLANE HEADWIND (20 KTS) EXHAUST WAKE DANGER AREA 65 MPH (105 km/h) OR GREATER EXHAUST WAKE DANGER AREA 65 MPH (105 km/h) OR LESS POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON "RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIAL WEAPONS PROJECT, NOV. 1951 A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BE COMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR: COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES. A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGE NEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGID STEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY. MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPE AIRCRAFT. LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT BEYOND DANGER AREA N_AC_060302_1_0030101_01_01 Danger Areas of the Engines CFM56 series engine FIGURE-6-3-2-991-003-A01 6-3-2 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 R = 5.18 m (17 ft) 1.5 m (5 ft) 30° TO 348 m (1150 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) NOTE: INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER ENTRY CORRIDOR EXHAUST DANGER AREA N_AC_060302_1_0040101_01_01 Danger Areas of the Engines IAE V2500 series engine FIGURE-6-3-2-991-004-A01 6-3-2 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 6-4-1 APU **ON A/C A319-100 A319neo APU - APIC & GARRETT 1. This section gives APU exhaust velocities and temperatures. 6-4-1 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo 300°C 200°C 150°C 572°F 392°F 302°F 120°C 248°F 100°C 212°F 80°C 176°F METERS PLAN 0 5 10 15 20 25 16.404 32.808 49.212 65.616 82.02 FEET 0 45 m/s 147 ft/s 30 m/s 98 ft/s HEIGHT 20 m/s 65 ft/s 5 m/s 16 ft/s 10 m/s 32 ft/s m METERS 5 0 ft 10 32.808 5 16.404 0 0 10 15 20 32.808 49.212 65.616 ELEVATION FEET 0 16.404 N_AC_060401_1_0020101_01_00 Exhaust Velocities and Temperatures APU -- APIC & GARRETT FIGURE-6-4-1-991-002-A01 6-4-1 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING PAVEMENT DATA 7-1-0 General Information **ON A/C A319-100 A319neo General Information 1. General A brief description of the pavement charts that follow will help in airport planning. To aid in the interpolation between the discrete values shown, each aircraft configuration is shown with a minimum range of five loads on the Main Landing Gear (MLG). All curves on the charts represent data at a constant specified tire pressure with: - The aircraft loaded to the Maximum Ramp Weight (MRW), - The CG at its maximum permissible aft position. Pavement requirements for commercial aircraft are derived from the static analysis of loads imposed on the MLG struts. Landing Gear Footprint: Section 07-02-00 presents basic data on the landing gear footprint configuration, MRW and tire sizes and pressures. Maximum Pavement Loads: Section 07-03-00 shows maximum vertical and horizontal pavement loads for certain critical conditions at the tire-ground interfaces. Landing Gear Loading on Pavement: Section 07-04-00 contains charts to find these loads throughout the stability limits of the aircraft at rest on the pavement. These MLG loads are used as the point of entry to the pavement design charts which follow, interpolating load values where necessary. Flexible Pavement Requirements - US Army Corps of Engineers Design Method: Section 07-05-00 uses procedures in Instruction Report No. S-77-1 ”Procedures for Development of CBR Design Curves”, dated June 1977 and as modified according to the methods described in ICAO Aerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCN Method), and utilizing the alpha factors approved by ICAO in October 2007. The report was prepared by the ”U.S. Army Corps Engineers Waterways Experiment Station, Soils and Pavement Laboratory, Vicksburg, Mississippi”. The line showing 10 000 coverages is used to calculate the Aircraft Classification Number (ACN). 7-1-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING Flexible Pavement Requirements - LCN Conversion Method: The flexible pavement charts in Section 07-06-00 show Load Classification Number (LCN) against Equivalent Single Wheel Load (ESWL), and ESWL against pavement thickness. All the LCN curves shown in the ’Flexible Pavement Requirements’ were developed from a computer program based on data in International Civil Aviation Organization (ICAO) document 7920AN/865/2, Aerodrome Manual, Part 2, ”Aerodrome Physical Characteristics”, Second Edition, 1965. Rigid Pavement Requirements - PCA (Portland Cement Association) Design Method: Section 07-07-00 gives the rigid pavement design curves that have been prepared with the use of the Westergaard Equation. This is in general accordance with the procedures outlined in the Portland Cement Association publications, ”Design of Concrete Airport Pavement”, 1973 and ”Computer Program for Airport Pavement Design” (Program PDILB), 1967 both by Robert G. Packard. Rigid Pavement Requirements - LCN Conversion: Section 07-08-00 gives data about the rigid pavement requirements for the LCN conversion: - For the radius of relative stiffness, - For the radius of relative stiffness (other values of E and µ). All the LCN curves shown in Rigid Pavement Requirements - LCN conversion were developed from a computer program based on data in International Civil Aviation Organization (ICAO) document 7920AN/865/2, Aerodrome Manual, Part 2, ”Aerodrome Physical Characteristics”, Second Edition, 1965. Rigid Pavement Requirements - LCN Conversion - Radius of Relative Stiffness: The rigid pavement charts show LCN against ESWL, and ESWL against radius of relative stiffness. Rigid Pavement Requirements - LCN Conversion - Radius of Relative Stiffness (other values of E and µ): The rigid pavement charts show LCN against ESWL, and ESWL against radius of relative stiffness affected by the other values of E and µ. ACN/PCN Reporting System: Section 07-09-00 provides ACN data prepared according to the ACN/PCN system as referenced in ICAO Annex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations” Fourth Edition, July 2004, incorporating Amendments 1 to 6. The ACN/PCN system provides a standardized international aircraft/pavement rating system replacing the various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world. ACN is the Aircraft Classification Number and PCN is the corresponding Pavement Classification Number. An aircraft having an ACN less than or equal to the PCN can operate without restriction on the pavement. Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms. The derived single wheel load is defined as the load on a single tire inflated to 1.25 MPa (181 psi) that would have the same pavement requirements as the aircraft. 7-1-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING Computationally the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1 for flexible pavements to calculate ACN values. The Airport Authority must decide on the method of pavement analysis and the results of their evaluation shown as follows: PCN PAVEMENT SUBGRADE EVALUATION TIRE PRESSURE CATEGORY TYPE CATEGORY METHOD R -- Rigid A -- High W -- No pressure limit T -- Technical X -- High pressure limited to 1.75 U -- Using Aircraft F -- Flexible B -- Medium MPa (254 psi) Y -- Medium pressure limited to 1.25 C -- Low MPa (181 psi) Z -- Low pressure limited to 0.5 MPa D -- Ultra Low (73 psi) For flexible pavements, the four subgrade categories (CBR) are: - A. High Strength B. Medium Strength C. Low Strength D. Ultra Low Strength CBR CBR CBR CBR 15 10 6 3 For rigid pavements, the four subgrade categories (k) are: - A. High Strength - B. Medium Strength - C. Low Strength - D. Ultra Low Strength k = 150 MN/m3 (550 pci) k = 80 MN/m3 (300 pci) k = 40 MN/m3 (150 pci) k = 20 MN/m3 (75 pci) 7-1-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-2-0 Landing Gear Footprint **ON A/C A319-100 A319neo Landing Gear Footprint 1. This section gives data about the landing gear footprint in relation to the aircraft MRW and tire sizes and pressures. The landing-gear footprint information is given for all the operational weight variants of the aircraft. 7-2-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 11.039 m (36.217 ft) 7.590 m (24.901 ft) 0.500 m (1.640 ft) 0.927 m (3.041 ft) WEIGHT VARIANT MAXIMUM RAMP WEIGHT PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP NOSE GEAR TIRE SIZE A319−100 WV000 (CG 36%) 64 400 kg (141 975 lb) 91.4% 30x8.8R15 (30x8.8−15) 11.4 bar (165 psi) 46x17R20 (46x16−20) 11.9 bar (173 psi) A319−100 WV000 (CG 39%) 64 400 kg (141 975 lb) 92.6% 30x8.8R15 (30x8.8−15) 11.4 bar (165 psi) 46x17R20 (46x16−20) 11.9 bar (173 psi) A319−100 70 400 kg WV001 (CG 37.5%) (155 200 lb) 92.1% 30x8.8R15 (30x8.8−15) 12.5 bar (181 psi) 46x17R20 (46x16−20) 12.9 bar (187 psi) NOSE GEAR MAIN GEAR MAIN GEAR TIRE TIRE PRESSURE TIRE SIZE PRESSURE A319−100 WV001 (CG 36%) 70 400 kg (155 200 lb) 91.5% 30x8.8R15 (30x8.8−15) 12.5 bar (181 psi) 46x17R20 (46x16−20) 12.9 bar (187 psi) A319−100 WV002 75 900 kg (167 325 lb) 91.6% 30x8.8R15 (30x8.8−15) 13.2 bar (191 psi) 46x17R20 (46x16−20) 13.8 bar (200 psi) A319−100 68 400 kg WV003 (CG 38.1%) (150 800 lb) 92.3% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) 91.5% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) A319−100 WV003 (CG 36%) 68 400 kg (150 800 lb) N_AC_070200_1_0040101_01_02 Landing Gear Footprint (Sheet 1 of 2) FIGURE-7-2-0-991-004-A01 7-2-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP NOSE GEAR TIRE SIZE 68 400 kg A319−100 WV004 (CG 38.1%) (150 800 lb) 92.3% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) 68 400 kg (150 800 lb) 91.5% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) 70 400 kg A319−100 WV005 (CG 37.5%) (155 200 lb) 92.1% 30x8.8R15 (30x8.8−15) 12.5 bar (181 psi) 46x17R20 (46x16−20) 12.9 bar (187 psi) 70 400 kg (155 200 lb) 91.5% 30x8.8R15 (30x8.8−15) 12.5 bar (181 psi) 46x17R20 (46x16−20) 12.9 bar (187 psi) 73 900 kg A319−100 WV006 (CG 36.52%) (162 925 lb) 91.7% 30x8.8R15 (30x8.8−15) 13.5 bar (196 psi) 46x17R20 (46x16−20) 13.4 bar (194 psi) A319−100 WV006 (CG 36%) 73 900 kg (162 925 lb) 91.5% 30x8.8R15 (30x8.8−15) 13.5 bar (196 psi) 46x17R20 (46x16−20) 13.4 bar (194 psi) A319−100 WV007 75 900 kg (167 325 lb) 91.6% 30x8.8R15 (30x8.8−15) 13.2 bar (191 psi) 46x17R20 (46x16−20) 13.8 bar (200 psi) A319−100 WV008 (CG 39%) 64 400 kg (141 975 lb) 92.6% 30x8.8R15 (30x8.8−15) 11.4 bar (165 psi) 46x17R20 (46x16−20) 11.9 bar (173 psi) A319−100 WV008 (CG 36%) 64 400 kg (141 975 lb) 91.4% 30x8.8R15 (30x8.8−15) 11.4 bar (165 psi) 46x17R20 (46x16−20) 11.9 bar (173 psi) 66 400 kg A319−100 WV009 (CG 38.8%) (146 375 lb) 92.6% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) 66 400 kg (146 375 lb) 91.5% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) 66 400 kg A319−100 WV011 (CG 38.8%) (146 375 lb) 92.6% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) A319−100 WV011 (CG 36%) 66 400 kg (146 375 lb) 91.5% 30x8.8R15 (30x8.8−15) 12.1 bar (175 psi) 46x17R20 (46x16−20) 12.5 bar (181 psi) A319−100 WV012 (CG 39%) 62 400 kg (137 575 lb) 92.6% 30x8.8R15 (30x8.8−15) 11.4 bar (165 psi) 46x17R20 (46x16−20) 11.9 bar (173 psi) A319−100 WV012 (CG 36%) 62 400 kg (137 575 lb) 91.4% 30x8.8R15 (30x8.8−15) 11.4 bar (165 psi) 46x17R20 (46x16−20) 11.9 bar (173 psi) A319 CJ WV002 75 900 kg (167 325 lb) 91.6% 30x8.8R15 (30x8.8−15) 13.9 bar (202 psi) 46x17R20 (46x16−20) 13.8 bar (200 psi) A319 CJ WV005 70 400 kg (155 200 lb) 91.6% 30x8.8R15 (30x8.8−15) 13.9 bar (202 psi) 46x17R20 (46x16−20) 13.8 bar (200 psi) A319 CJ WV010 76 900 kg (169 525 lb) 91.5% 30x8.8R15 (30x8.8−15) 13.9 bar (202 psi) 46x17R20 13.8 bar (200 psi) WEIGHT VARIANT A319−100 WV004 (CG 36%) A319−100 WV005 (CG 36%) A319−100 WV009 (CG 36%) MAXIMUM RAMP WEIGHT NOSE GEAR MAIN GEAR MAIN GEAR TIRE TIRE PRESSURE TIRE SIZE PRESSURE N_AC_070200_1_0040102_01_00 Landing Gear Footprint (Sheet 2 of 2) FIGURE-7-2-0-991-004-A01 7-2-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo 11.039 m (36.217 ft) 7.590 m (24.901 ft) 0.500 m (1.640 ft) 0.927 m (3.041 ft) WEIGHT VARIANT MAXIMUM RAMP WEIGHT PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP NOSE GEAR TIRE SIZE A319NEO WV050 64 400 kg (141 975 lb) 92.6% 30x8.8R15 11.4 bar (165 psi) 46x17R20 11.9 bar (173 psi) A319NEO WV051 64 400 kg (141 975 lb) 92.6% 30x8.8R15 11.4 bar (165 psi) 46x17R20 11.9 bar (173 psi) A319NEO WV052 70 400 kg (155 200 lb) 92.1% 30x8.8R15 12.5 bar (181 psi) 46x17R20 12.9 bar (187 psi) A319NEO WV053 70 400 kg (155 200 lb) 92.1% 30x8.8R15 12.5 bar (181 psi) 46x17R20 12.9 bar (187 psi) A319NEO WV054 75 900 kg (167 325 lb) 91.6% 30x8.8R15 13.2 bar (191 psi) 46x17R20 13.8 bar (200 psi) A319NEO WV055 75 900 kg (167 325 lb) 91.6% 30x8.8R15 13.2 bar (191 psi) 46x17R20 13.8 bar (200 psi) NOSE GEAR MAIN GEAR MAIN GEAR TIRE TIRE PRESSURE TIRE SIZE PRESSURE N_AC_070200_1_0370101_01_00 Landing Gear Footprint FIGURE-7-2-0-991-037-A01 7-2-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-3-0 Maximum Pavement Loads **ON A/C A319-100 A319neo Maximum Pavement Loads 1. This section shows the maximum vertical and horizontal pavement loads for some critical conditions at the tire-ground interfaces. The maximum pavement loads are given for all the operational weight variants of the aircraft. 7-3-0 Page 1 May 01/14 7-3-0 21 % MAC (a) 21 % MAC (a) 21 % MAC (a) 21 % MAC (b) 64 400 kg 9 300 kg (141 975 lb) (20 500 lb) 70 400 kg 10 120 kg (155 200 lb) (22 325 lb) 70 400 kg 10 120 kg (155 200 lb) (22 325 lb) 75 900 kg 10 720 kg (167 325 lb) (23 625 lb) 17 870 kg (39 400 lb) 16 660 kg (36 725 lb) 16 660 kg (36 725 lb) 15 310 kg (33 750 lb) 15 310 kg (33 750 lb) STATIC BRAKING AT 10 ft/s² DECELERATION 4 34 750 kg (76 600 lb) 32 210 kg (71 000 lb) 32 420 kg (71 475 lb) 29 830 kg (65 775 lb) 29 450 kg (64 925 lb) 36 % MAC (a) 36 % MAC (a) 37.5 % MAC (a) 39 % MAC (a) 36 % MAC (a) STATIC LOAD AT MAX AFT CG 5 V(MG) (PER STRUT) NOTE: (a) LOADS CALCULATED USING AIRCRAFT AT MRW. (b) LOADS CALCULATED USING AIRCRAFT AT 74 500 kg (164 250 lb). A319−100 WV002 21 % MAC (a) 64 400 kg 9 300 kg (141 975 lb) (20 500 lb) STATIC LOAD AT MOST FWD CG MAXIMUM RAMP WEIGHT WEIGHT VARIANT V(NG) 3 2 1 A319−100 WV000 (CG 36 %) A319−100 WV000 (CG 39 %) A319−100 WV001 (CG 37.5 %) A319−100 WV001 (CG 36 %) H 11 800 kg (26 000 lb) 10 940 kg (24 125 lb) 10 940 kg (24 125 lb) 10 010 kg (22 075 lb) 10 010 kg (22 075 lb) 27 800 kg (61 275 lb) 25 770 kg (56 800 lb) 25 940 kg (57 175 lb) 23 860 kg (52 600 lb) 23 560 kg (51 925 lb) STEADY BRAKING AT INSTANTANEOUS AT 10 ft/s² BRAKING DECELERATION COEFFICIENT = 0.8 6 H (PER STRUT) V(MG) V(NG) MAXIMUM VERTICAL NOSE GEAR GROUND LOAD AT MOST FWD CG V(MG) MAXIMUM VERTICAL MAIN GEAR GROUND LOAD AT MAX AFT CG H MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING V(NG) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_070300_1_0230101_01_01 Maximum Pavement Loads (Sheet 1 of 3) FIGURE-7-3-0-991-023-A01 Page 2 May 01/14 7-3-0 21 % MAC (a) 21 % MAC (a) 21 % MAC (a) 21 % MAC (a) 70 400 kg 10 120 kg (155 200 lb) (22 325 lb) 70 400 kg 10 120 kg (155 200 lb) (22 325 lb) 73 900 kg 10 610 kg (162 925 lb) (23 400 lb) 73 900 kg 10 610 kg (162 925 lb) (23 400 lb) 21 % MAC (a) 15 310 kg (33 750 lb) 17 870 kg (39 400 lb) 17 460 kg (38 500 lb) 17 460 kg (38 500 lb) 16 660 kg (36 725 lb) 16 660 kg (36 725 lb) 16 230 kg (35 775 lb) 16 230 kg (35 775 lb) 16 230 kg (35 775 lb) 16 230 kg (35 775 lb) STATIC BRAKING AT 10 ft/s² DECELERATION 4 29 830 kg (65 775 lb) 34 750 kg (76 600 lb) 33 820 kg (74 550 lb) 33 890 kg (74 725 lb) 32 210 kg (71 000 lb) 32 420 kg (71 475 lb) 31 280 kg (68 950 lb) 31 560 kg (69 600 lb) 31 280 kg (68 950 lb) 31 560 kg (69 600 lb) 39 % MAC (a) 36 % MAC (a) 36 % MAC (a) 36.52 % MAC (a) 36 % MAC (a) 37.5 % MAC (a) 36 % MAC (a) 38.1 % MAC (a) 36 % MAC (a) 38.1 % MAC (a) STATIC LOAD AT MAX AFT CG 5 V(MG) (PER STRUT) NOTE: (a) LOADS CALCULATED USING AIRCRAFT AT MRW. (b) LOADS CALCULATED USING AIRCRAFT AT 74 500 kg (164 250 lb). 64 400 kg 9 300 kg (141 975 lb) (20 500 lb) 21 % MAC (a) 68 400 kg 9 860 kg (150 800 lb) (21 750 lb) A319−100 WV008 (CG 39 %) 21 % MAC (a) 68 400 kg 9 860 kg (150 800 lb) (21 750 lb) 21 % MAC (b) 21 % MAC (a) 68 400 kg 9 860 kg (150 800 lb) (21 750 lb) 75 900 kg 10 720 kg (167 325 lb) (23 625 lb) 21 % MAC (a) 68 400 kg 9 860 kg (150 800 lb) (21 750 lb) A319−100 WV007 A319−100 WV003 (CG 38.1 %) A319−100 WV003 (CG 36 %) A319−100 WV004 (CG 38.1 %) A319−100 WV004 (CG 36 %) A319−100 WV005 (CG 37.5 %) A319−100 WV005 (CG 36 %) A319−100 WV006 (CG 36.52 %) A319−100 WV006 (CG 36 %) STATIC LOAD AT MOST FWD CG MAXIMUM RAMP WEIGHT WEIGHT VARIANT V(NG) 3 2 1 10 010 kg (22 075 lb) 11 800 kg (26 000 lb) 11 480 kg (25 325 lb) 11 480 kg (25 325 lb) 10 940 kg (24 125 lb) 10 940 kg (24 125 lb) 10 630 kg (23 425 lb) 10 630 kg (23 425 lb) 10 630 kg (23 425 lb) 10 630 kg (23 425 lb) 23 860 kg (52 600 lb) 27 800 kg (61 275 lb) 27 050 kg (59 650 lb) 27 110 kg (59 775 lb) 25 770 kg (56 800 lb) 25 940 kg (57 175 lb) 25 020 kg (55 175 lb) 25 250 kg (55 675 lb) 25 020 kg (55 175 lb) 25 250 kg (55 675 lb) STEADY BRAKING AT INSTANTANEOUS AT 10 ft/s² BRAKING DECELERATION COEFFICIENT = 0.8 6 H (PER STRUT) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_070300_1_0230102_01_00 Maximum Pavement Loads (Sheet 2 of 3) FIGURE-7-3-0-991-023-A01 Page 3 May 01/14 7-3-0 20.4 % MAC (a) 20.4 % MAC (a) 14 % MAC (b) 62 400 kg 9 170 kg (137 575 lb) (20 200 lb) 62 400 kg 9 170 kg (137 575 lb) (20 200 lb) 75 900 kg 11 540 kg (167 325 lb) (25 450 lb) 17 790 kg (39 225 lb) 17 990 kg (39 650 lb) 17 880 kg (39 425 lb) 15 000 kg (33 075 lb) 15 000 kg (33 075 lb) 15 770 kg (34 775 lb) 15 770 kg (34 775 lb) 15 770 kg (34 775 lb) 15 770 kg (34 775 lb) 15 310 kg (33 750 lb) STATIC BRAKING AT 10 ft/s² DECELERATION 4 35 180 kg (77 550 lb) 32 240 kg (71 075 lb) 34 750 kg (76 625 lb) 28 530 kg (62 900 lb) 28 900 kg (63 725 lb) 30 360 kg (66 950 lb) 30 730 kg (67 750 lb) 30 360 kg (66 950 lb) 30 730 kg (67 750 lb) 29 450 kg (64 925 lb) 36 % MAC (a) 36 % MAC (a) 36 % MAC (a) 36 % MAC (a) 39 % MAC (a) 36 % MAC (a) 38.8 % MAC (a) 36 % MAC (a) 38.8 % MAC (a) 36 % MAC (a) STATIC LOAD AT MAX AFT CG 5 V(MG) (PER STRUT) NOTE: (a) LOADS CALCULATED USING AIRCRAFT AT MRW. (b) LOADS CALCULATED USING AIRCRAFT AT 67 500 kg (148 800 lb). 14 % MAC (b) 21 % MAC (a) 66 400 kg 9 580 kg (146 375 lb) (21 125 lb) 76 900 kg 11 540 kg (169 525 lb) (25 450 lb) 21 % MAC (a) 66 400 kg 9 580 kg (146 375 lb) (21 125 lb) A319 CJ WV010 21 % MAC (a) 66 400 kg 9 580 kg (146 375 lb) (21 125 lb) 14 % MAC (b) 21 % MAC (a) 66 400 kg 9 580 kg (146 375 lb) (21 125 lb) 70 400 kg 11 550 kg (155 200 lb) (25 450 lb) 21 % MAC (a) 64 400 kg 9 300 kg (141 975 lb) (20 500 lb) A319 CJ WV005 A319 CJ WV002 A319−100 WV008 (CG 36 %) A319−100 WV009 (CG 38.8 %) A319−100 WV009 (CG 36 %) A319−100 WV011 (CG 38.8 %) A319−100 WV011 (CG 36 %) A319−100 WV012 (CG 39 %) A319−100 WV012 (CG 36 %) STATIC LOAD AT MOST FWD CG MAXIMUM RAMP WEIGHT WEIGHT VARIANT V(NG) 3 2 1 11 950 kg (26 350 lb) 10 940 kg (24 125 lb) 11 800 kg (26 000 lb) 9 700 kg (21 375 lb) 9 700 kg (21 375 lb) 10 320 kg (22 750 lb) 10 320 kg (22 750 lb) 10 320 kg (22 750 lb) 10 320 kg (22 750 lb) 10 010 kg (22 075 lb) 28 140 kg (62 050 lb) 25 800 kg (56 875 lb) 27 800 kg (61 300 lb) 22 820 kg (50 325 lb) 23 120 kg (50 975 lb) 24 290 kg (53 550 lb) 24 590 kg (54 200 lb) 24 290 kg (53 550 lb) 24 590 kg (54 200 lb) 23 560 kg (51 925 lb) STEADY BRAKING AT INSTANTANEOUS AT 10 ft/s² BRAKING DECELERATION COEFFICIENT = 0.8 6 H (PER STRUT) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 N_AC_070300_1_0230104_01_00 Maximum Pavement Loads (Sheet 3 of 3) FIGURE-7-3-0-991-023-A01 Page 4 May 01/14 H 7-3-0 21 % MAC (a) 21 % MAC (a) 21 % MAC (a) 21 % MAC (a) 21 % MAC (b) 21 % MAC (b) 64 400 kg 9 300 kg (141 975 lb) (20 500 lb) 64 400 kg 9 300 kg (141 975 lb) (20 500 lb) 70 400 kg 10 120 kg (155 200 lb) (22 325 lb) 70 400 kg 10 120 kg (155 200 lb) (22 325 lb) 75 900 kg 10 720 kg (167 325 lb) (23 625 lb) 75 900 kg 10 720 kg (167 325 lb) (23 625 lb) A319NEO WV050 A319NEO WV051 A319NEO WV052 A319NEO WV053 A319NEO WV054 A319NEO WV055 17 870 kg (39 400 lb) 17 870 kg (39 400 lb) 16 660 kg (36 725 lb) 16 660 kg (36 725 lb) 15 310 kg (33 750 lb) 15 310 kg (33 750 lb) STATIC BRAKING AT 10 ft/s² DECELERATION 34 750 kg (76 600 lb) 34 750 kg (76 600 lb) 32 420 kg (71 475 lb) 32 420 kg (71 475 lb) 29 830 kg (65 775 lb) 29 830 kg (65 775 lb) 36 % MAC (a) 36 % MAC (a) 37.5 % MAC (a) 37.5 % MAC (a) 39 % MAC (a) 39 % MAC (a) STATIC LOAD AT MAX AFT CG 5 V(MG) (PER STRUT) NOTE: (a) LOADS CALCULATED USING AIRCRAFT AT MRW. (b) LOADS CALCULATED USING AIRCRAFT AT 74 500 kg (164 250 lb). STATIC LOAD AT MOST FWD CG MAXIMUM RAMP WEIGHT WEIGHT VARIANT V(NG) 3 2 1 4 11 800 kg (26 000 lb) 11 800 kg (26 000 lb) 10 940 kg (24 125 lb) 10 940 kg (24 125 lb) 10 010 kg (22 075 lb) 10 010 kg (22 075 lb) 27 800 kg (61 275 lb) 27 800 kg (61 275 lb) 25 940 kg (57 175 lb) 25 940 kg (57 175 lb) 23 860 kg (52 600 lb) 23 860 kg (52 600 lb) STEADY BRAKING AT INSTANTANEOUS AT 10 ft/s² BRAKING DECELERATION COEFFICIENT = 0.8 6 H (PER STRUT) V(MG) V(NG) MAXIMUM VERTICAL NOSE GEAR GROUND LOAD AT MOST FWD CG V(MG) MAXIMUM VERTICAL MAIN GEAR GROUND LOAD AT MAX AFT CG H MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING V(NG) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo N_AC_070300_1_0400101_01_00 Maximum Pavement Loads FIGURE-7-3-0-991-040-A01 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-4-0 Landing Gear Loading on Pavement **ON A/C A319-100 A319neo Landing Gear Loading on Pavement 1. Landing Gear Loading on Pavement This section gives data about the landing gear loading on pavement. The MLG loading on pavement graphs are given for the weight variants that produce (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG load for each type of aircraft. Example, see FIGURE 7-4-0-991-003-A, calculation of the total weight on the MLG for: - An aircraft with a MRW of 62 400 kg (137 575 lb), - The aircraft gross weight is 60 000 kg (132 275 lb), - A percentage of weight on the MLG of 91.5% (percentage of weight on the MLG at MRW and maximum aft CG). The total weight on the MLG group is 54 890 kg (121 000 lb). NOTE : The CG in the figure title is the CG used for ACN/LCN calculation. 7-4-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 80 80 170 75 75 160 70 150 65 CG FOR ACN CALCULATION 36% MAC 140 MTOW − 62 000 kg 60 60 MLW 20.4% MAC 130 55 55 50 50 110 45 100 120 (x 1 000 lb) AIRCRAFT GROSS WEIGHT 65 (x 1 000 kg) WEIGHT ON MAIN LANDING GEAR (x 1 000 kg) 70 MZFW 45 LANDING 40 40 90 TAKE OFF 80 35 80 82 84 86 88 90 92 94 96 98 35 100 PERCENTAGE OF WEIGHT ON MAIN GEAR N_AC_070400_1_0030101_01_00 Landing Gear Loading on Pavement WV012, MRW 62 400 kg, CG 36% FIGURE-7-4-0-991-003-A01 7-4-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 80 80 CG FOR ACN CALCULATION 36% MAC 75 170 75 MTOW − 76 500 kg 70 26% MAC 150 65 140 MLW 60 60 55 55 50 110 45 100 LANDING 40 120 50 MZFW 45 130 40 (x 1 000 lb) AIRCRAFT GROSS WEIGHT 65 (x 1 000 kg) WEIGHT ON MAIN LANDING GEAR (x 1 000 kg) 70 160 90 TAKE OFF 80 35 80 82 84 86 88 90 92 94 96 98 35 100 PERCENTAGE OF WEIGHT ON MAIN GEAR N_AC_070400_1_0040101_01_00 Landing Gear Loading on Pavement WV010, MRW 76 900 kg, CG 36% FIGURE-7-4-0-991-004-A01 7-4-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo 80 80 170 75 75 160 70 150 CG FOR ACN CALCULATION 39% MAC 65 140 MLW MTOW − 64 000 kg 60 60 21% MAC 55 55 50 130 120 50 110 45 100 (x 1 000 lb) AIRCRAFT GROSS WEIGHT 65 (x 1 000 kg) WEIGHT ON MAIN LANDING GEAR (x 1 000 kg) 70 MZFW 45 LANDING 40 40 90 TAKE OFF 80 35 80 82 84 86 88 90 92 94 96 98 35 100 PERCENTAGE OF WEIGHT ON MAIN GEAR N_AC_070400_1_0050101_01_00 Landing Gear Loading on Pavement WV050, MRW 64 400 kg, CG 39% FIGURE-7-4-0-991-005-A01 7-4-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo 80 80 170 CG FOR ACN CALCULATION 36% MAC 75 75 160 MTOW − 75 500 kg 70 26% MAC 150 65 140 MLW 60 60 55 55 50 MZFW 45 120 50 110 45 100 LANDING 40 130 40 (x 1 000 lb) AIRCRAFT GROSS WEIGHT 65 (x 1 000 kg) WEIGHT ON MAIN LANDING GEAR (x 1 000 kg) 70 90 TAKE OFF 80 35 80 82 84 86 88 90 92 94 96 98 35 100 PERCENTAGE OF WEIGHT ON MAIN GEAR N_AC_070400_1_0060101_01_00 Landing Gear Loading on Pavement WV054, MRW 75 900 kg, CG 36% FIGURE-7-4-0-991-006-A01 7-4-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method **ON A/C A319-100 A319neo Flexible Pavement Requirements - US Army Corps of Engineers Design Method 1. This section gives data about the flexible pavement requirements. The flexible pavement requirement graphs are given at standard tire pressure for the weight variants producing (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG load for each type of aircraft. They are calculated with the US Army Corps of Engineers Design Method. To find a flexible pavement thickness, you must know the Subgrade Strength (CBR), the annual departure level and the weight on one MLG. The line that shows 10 000 coverages is used to calculate the Aircraft Classification Number (ACN). The procedure that follows is used to develop flexible pavement design curves: - With the scale for pavement thickness at the bottom and the scale for CBR at the top, a random line is made to show 10 000 coverages, - A plot is then made of the incremental values of the weight on the MLG, - Annual departure lines are made based on the load lines of the weight on the MLG that is shown on the graph. Example, see FIGURE 7-5-0-991-003-A, calculation of the thickness of the flexible pavement for MLG: - An aircraft with a MRW of 62 400 kg (137 575 lb), - A ”CBR” value of 10, - An annual departure level of 3 000, - The load on one MLG of 25 000 kg (55 125 lb). The required flexible pavement thickness is 46.5 cm (18 in). NOTE : The CG in the figure title is the CG used for ACN calculation. 7-5-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 SUBGRADE STRENGTH − CBR 3 6 10 15 20 30 40 60 80 60 80 WEIGHT ON ONE MAIN LANDING GEAR 28 530 kg (62 900 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 10 000 COVERAGES USED FOR ACN CALCULATIONS ALPHA FACTOR = 0.9 ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000 *20 YEAR PAVEMENT LIFE 3 10 6 10 15 20 15 (in) 30 40 (cm) 20 30 60 80 40 100 120 150 180 FLEXIBLE PAVEMENT THICKNESS 46x17R20 (46x16−20) TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) N_AC_070500_1_0030101_01_00 Flexible Pavement Requirements WV012, MRW 62 400 kg, CG 36 % FIGURE-7-5-0-991-003-A01 7-5-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 SUBGRADE STRENGTH − CBR 3 6 10 15 20 30 40 60 80 WEIGHT ON ONE MAIN LANDING GEAR 35 180 kg (77 550 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 10 000 COVERAGES USED FOR ACN CALCULATIONS ALPHA FACTOR = 0.9 ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000 *20 YEAR PAVEMENT LIFE 3 10 6 10 15 20 15 (in) 30 20 40 (cm) 30 60 80 40 60 80 100 120 150 180 FLEXIBLE PAVEMENT THICKNESS 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) N_AC_070500_1_0040101_01_00 Flexible Pavement Requirements WV010, MRW 76 900 kg, CG 36 % FIGURE-7-5-0-991-004-A01 7-5-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo SUBGRADE STRENGTH − CBR 3 6 10 15 20 30 40 60 80 WEIGHT ON ONE MAIN LANDING GEAR 29 830 kg (65 775 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 10 000 COVERAGES USED FOR ACN CALCULATIONS ALPHA FACTOR = 0.9 ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000 *20 YEAR PAVEMENT LIFE 3 10 6 10 15 20 15 (in) 30 20 40 (cm) 30 60 80 40 60 80 100 120 150 180 FLEXIBLE PAVEMENT THICKNESS 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) N_AC_070500_1_0050101_01_00 Flexible Pavement Requirements WV050, MRW 64 400 kg, CG 39 % FIGURE-7-5-0-991-005-A01 7-5-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo SUBGRADE STRENGTH − CBR 3 6 10 15 20 30 40 60 80 WEIGHT ON ONE MAIN LANDING GEAR 34 750 kg (76 600 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 10 000 COVERAGES USED FOR ACN CALCULATIONS ALPHA FACTOR = 0.9 ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000 *20 YEAR PAVEMENT LIFE 3 10 6 10 15 20 15 (in) 30 20 40 (cm) 30 60 80 40 60 80 100 120 150 180 FLEXIBLE PAVEMENT THICKNESS 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) N_AC_070500_1_0060101_01_00 Flexible Pavement Requirements WV054, MRW 75 900 kg, CG 36 % FIGURE-7-5-0-991-006-A01 7-5-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-6-0 Flexible Pavement Requirements - LCN Conversion **ON A/C A319-100 A319neo Flexible Pavement Requirements - LCN Conversion 1. This section gives data about the flexible pavement requirements for Load Classification Number (LCN) conversion. The flexible pavement requirement graphs are given at standard tire pressure for the weight variants producing (at the MRW and max aft CG) the lowest MLG load and the highest MLG load for each type of aircraft. They are calculated with the LCN conversion method. To find the aircraft weight that a flexible pavement can support, you must know the LCN of the pavement and the thickness. Example, see FIGURE 7-6-0-991-006-A, calculation of the weight on one MLG for flexible pavement: - An aircraft with a MRW of 62 400 kg (137 575 lb), - The flexible pavement thickness is 508 mm (20 in) with a related LCN of 53. The weight on one MLG is 25 000 kg (55 125 lb). 2. Flexible Pavement Requirements - LCN Table The tables in FIGURE 7-6-0-991-004-A and FIGURE 7-6-0-991-028-A provides LCN data in a tabular format similar to the one used by ICAO in the ”Aerodrome Design Manual Part 3, Pavements Edition 1977”. In order to use the system accurately, you should know the total pavement thickness for flexible pavement. However, the pavement thickness for a particular runway is not frequently published in the standard airport information sources (Jeppesen, AERAD, DOD, etc.). Therefore it is common practice to use a standard thickness (20 in) when determining the LCN and the ESWL of the aircraft. If the LCN for an intermediate weight between the MRW and the empty weight of the aircraft is required, or if the real thickness is known, refer to the figures that follow. NOTE : The CG in the figure title is the CG used for LCN calculation. 7-6-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 WEIGHT VARIANT ALL UP MASS (kg) A319−100 WV000 (CG 36%) A319−100 WV000 (CG 39%) A319−100 WV001 (CG 37.5%) A319−100 WV001 (CG 36%) A319−100 WV002 A319−100 WV003 (CG 38.1%) A319−100 WV003 (CG 36%) A319−100 WV004 (CG 38.1%) A319−100 WV004 (CG 36%) A319−100 WV005 (CG 37.5%) A319−100 WV005 (CG 36%) A319−100 WV006 (CG 36.52%) A319−100 WV006 (CG 36%) 64 400 41 000 64 400 41 000 70 400 41 000 70 400 41 000 75 900 41 000 68 400 41 000 68 400 41 000 68 400 41 000 68 400 41 000 70 400 41 000 70 400 41 000 73 900 41 000 73 900 41 000 LOAD ON TIRE ONE MAIN PRESSURE GEAR LEG (MPa) (%) 45.7 45.7 46.3 46.3 46.1 46.0 45.8 45.7 45.8 45.7 46.1 46.1 45.7 45.7 46.1 46.1 45.7 45.7 46.1 46.0 45.8 45.7 45.9 45.8 45.8 45.7 1.19 1.19 1.29 1.29 1.38 1.25 1.25 1.25 1.25 1.29 1.29 1.34 1.34 FLEXIBLE PAVEMENT ESWL LCN x 1 000 kg x 1 000 lb h = 510 mm (20 in) 18 40 61 25 39 11 18 40 62 25 39 11 20 44 69 25 40 11 20 44 69 40 11 24 47 76 21 11 24 41 19 43 66 25 40 11 19 66 42 40 11 24 19 43 66 25 40 11 19 66 42 40 11 24 44 20 69 25 40 11 44 20 69 40 24 11 46 73 21 24 41 11 46 73 21 11 24 41 N_AC_070600_1_0040101_01_00 Flexible Pavement Requirements LCN Table (Sheet 1 of 2) FIGURE-7-6-0-991-004-A01 7-6-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 WEIGHT VARIANT ALL UP MASS (kg) A319−100 WV007 A319−100 WV008 (CG 39%) A319−100 WV008 (CG 36%) A319−100 WV009 (CG 38.8%) A319−100 WV009 (CG 36%) A319−100 WV011 (CG 38.8%) A319−100 WV011 (CG 36%) A319−100 WV012 (CG 39%) A319−100 WV012 (CG 36%) A319 CJ WV002 A319 CJ WV005 A319 CJ WV010 75 900 41 000 64 400 41 000 64 400 41 000 66 400 41 000 66 400 41 000 66 400 41 000 66 400 41 000 62 400 41 000 62 400 41 000 75 900 41 000 70 400 41 000 76 900 41 000 LOAD ON TIRE ONE MAIN PRESSURE GEAR LEG (MPa) (%) 45.8 45.7 46.3 46.3 45.7 45.7 46.3 46.2 45.7 45.7 46.3 46.2 45.7 45.7 46.3 46.3 45.7 45.7 45.8 45.8 45.8 45.7 45.7 45.8 1.38 1.19 1.19 1.25 1.25 1.25 1.25 1.19 1.19 1.38 1.38 1.38 FLEXIBLE PAVEMENT ESWL LCN x 1 000 kg x 1 000 lb h = 510 mm (20 in) 47 76 21 11 24 41 40 62 18 25 39 11 61 40 18 25 39 11 65 19 41 25 40 11 64 19 41 40 24 11 65 19 41 25 40 11 64 19 41 40 24 11 60 39 18 25 39 11 59 38 17 25 39 11 76 47 21 24 41 11 43 20 71 24 41 11 77 48 22 24 41 11 N_AC_070600_1_0040102_01_00 Flexible Pavement Requirements LCN Table (Sheet 2 of 2) FIGURE-7-6-0-991-004-A01 7-6-0 Page 3 May 01/14 0 10 10 20 30 40 50 60 70 80 750 1 000 EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) 7-6-0 30 40 50 2 000 10 30 40 50 60 5 10 15 20 25 30 35 0 80 100 LOAD CLASSIFICATION NUMBER (LCN) 20 WEIGHT ON ONE MAIN LANDING GEAR 28 530 kg (62 900 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 46x17R20 (46x16−20) TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. 60 70 80 1 500 FLEXIBLE PAVEMENT THICKNESS (in) 20 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 500 FLEXIBLE PAVEMENT THICKNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) N_AC_070600_1_0060101_01_00 Flexible Pavement Requirements - LCN WV012, MRW 62 400 kg, CG 36 % FIGURE-7-6-0-991-006-A01 Page 4 May 01/14 0 10 10 20 30 40 50 60 70 80 750 1 000 EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) 7-6-0 30 40 50 60 100 10 30 40 50 60 5 10 15 20 25 30 35 0 80 100 LOAD CLASSIFICATION NUMBER (LCN) 20 WEIGHT ON ONE MAIN LANDING GEAR 35 180 kg (77 550 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. FLEXIBLE PAVEMENT THICKNESS (in) 20 80 1 500 2 000 2 500 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 500 FLEXIBLE PAVEMENT THICKNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) N_AC_070600_1_0070101_01_00 Flexible Pavement Requirements - LCN WV010, MRW 76 900 kg, CG 36 % FIGURE-7-6-0-991-007-A01 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo WEIGHT VARIANT ALL UP MASS (kg) A319NEO WV050 A319NEO WV051 A319NEO WV052 A319NEO WV053 A319NEO WV054 A319NEO WV055 64 400 41 000 64 400 41 000 70 400 41 000 70 400 41 000 75 900 41 000 75 900 41 000 LOAD ON TIRE ONE MAIN PRESSURE GEAR LEG (MPa) (%) 46.3 46.3 46.3 46.3 46.1 46.0 46.1 46.0 45.8 45.7 45.8 45.7 1.19 1.19 1.29 1.29 1.38 1.38 FLEXIBLE PAVEMENT ESWL LCN x 1 000 kg x 1 000 lb h = 510 mm (20 in) 18 40 62 25 39 11 40 62 18 25 39 11 44 69 20 25 40 11 44 69 20 25 40 11 47 76 21 24 41 11 47 76 21 24 41 11 N_AC_070600_1_0280101_01_00 Flexible Pavement Requirements LCN Table FIGURE-7-6-0-991-028-A01 7-6-0 Page 6 May 01/14 0 10 10 20 30 40 50 60 70 80 750 1 000 EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) 7-6-0 30 40 50 2 000 10 30 40 50 60 5 10 15 20 25 30 35 0 80 100 LOAD CLASSIFICATION NUMBER (LCN) 20 WEIGHT ON ONE MAIN LANDING GEAR 29 830 kg (65 775 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. 60 70 80 1 500 FLEXIBLE PAVEMENT THICKNESS (in) 20 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 500 FLEXIBLE PAVEMENT THICKNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) N_AC_070600_1_0080101_01_00 Flexible Pavement Requirements - LCN WV050, MRW 64 400 kg, CG 39 % FIGURE-7-6-0-991-008-A01 Page 7 May 01/14 0 10 10 20 30 40 50 60 70 80 750 1 000 EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) 7-6-0 30 40 50 2 000 10 30 40 50 60 5 10 15 20 25 30 35 0 80 100 LOAD CLASSIFICATION NUMBER (LCN) 20 WEIGHT ON ONE MAIN LANDING GEAR 34 750 kg (76 600 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. 60 70 80 1 500 FLEXIBLE PAVEMENT THICKNESS (in) 20 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 500 FLEXIBLE PAVEMENT THICKNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) N_AC_070600_1_0090101_01_00 Flexible Pavement Requirements - LCN WV054, MRW 75 900 kg, CG 36 % FIGURE-7-6-0-991-009-A01 Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method **ON A/C A319-100 A319neo Rigid Pavement Requirements - Portland Cement Association Design Method 1. This section gives data about the rigid pavement requirements for the PCA (Portland Cement Association) design method. The rigid pavement requirement graphs are given at standard tire pressure for the weight variants producing (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG load for each A/C type. They are calculated with the PCA design method. To find a rigid pavement thickness, you must know the Subgrade Modulus (k), the permitted working stress and the weight on one MLG. The procedure that follows is used to develop rigid pavement design curves: - With the scale for pavement thickness on the left and the scale for permitted working stress on the right, a random load line is made. This represents the MLG maximum weight to be shown, - A plot is then made of all values of the subgrade modulus (k values), - More load lines for the incremental values of the weight on the MLG are made based on the curve for k = 150 MN/m3, which is already shown on the graph. Example, see FIGURE 7-7-0-991-005-A, calculation of the thickness of the rigid pavement for the MLG: - An aircraft with a MRW of 62 400 kg (137 575 lb), - A k value of 150 MN/m3 (550 lbf/in3), - A permitted working stress of 31.64 kg/cm2 (450 lb/in2), - The load on one MLG is 20 000 kg (44 100 lb). The required rigid pavement thickness is 186 mm (7 in). NOTE : The CG in the figure title is the CG used for ACN calculation. 7-7-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 46x17R20 (46x16−20) TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) 70 1 000 14 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG WEIGHT ON ONE MAIN LANDING GEAR 28 530 kg (62 900 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 34 13 32 12 900 60 800 24 600 k = 20 MN/m³ k = 40 MN/m³ k = 80 MN/m³ k = 150 MN/m³ 40 9 500 8 400 7 300 22 ALLOWABLE WORKING STRESS 10 (kg/cm²) 26 50 700 11 (lb/in²) 28 (in) RIGID PAVEMENT THICKNESS (cm) 30 30 20 18 20 16 200 6 NOTE: THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR k ARE EXACT. FOR LOADS LESS THAN MAXIMUM, THE CURVES ARE EXACT FOR k = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF k. REFERENCE: "DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION. N_AC_070700_1_0050101_01_00 Rigid Pavement Requirements WV012, MRW 62 400 kg, CG 36 % FIGURE-7-7-0-991-005-A01 7-7-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) 900 15 38 60 36 14 34 13 k = 20 MN/m³ k = 40 MN/m³ k = 80 MN/m³ k = 150 MN/m³ 800 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 50 700 500 10 400 9 300 (kg/cm²) 11 (lb/in²) 28 40 30 26 ALLOWABLE WORKING STRESS 600 12 30 (in) RIGID PAVEMENT THICKNESS (cm) 32 24 20 22 8 20 18 7 WEIGHT ON ONE MAIN LANDING GEAR 35 180 kg (77 550 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) NOTE: THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR k ARE EXACT. FOR LOADS LESS THAN MAXIMUM, THE CURVES ARE EXACT FOR k = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF k. 200 10 100 REFERENCE: "DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION. N_AC_070700_1_0060101_01_00 Rigid Pavement Requirements WV010, MRW 76 900 kg, CG 36 % FIGURE-7-7-0-991-006-A01 7-7-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) 70 1 000 14 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG WEIGHT ON ONE MAIN LANDING GEAR 29 830 kg (65 775 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 34 13 32 12 900 60 800 24 600 k = 20 MN/m³ k = 40 MN/m³ k = 80 MN/m³ k = 150 MN/m³ 40 9 500 8 400 7 300 22 ALLOWABLE WORKING STRESS 10 (kg/cm²) 26 50 700 11 (lb/in²) 28 (in) RIGID PAVEMENT THICKNESS (cm) 30 30 20 18 20 16 200 6 NOTE: THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR k ARE EXACT. FOR LOADS LESS THAN MAXIMUM, THE CURVES ARE EXACT FOR k = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF k. REFERENCE: "DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION. N_AC_070700_1_0070101_01_00 Rigid Pavement Requirements WV050, MRW 64 400 kg, CG 39 % FIGURE-7-7-0-991-007-A01 7-7-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) 14 WEIGHT ON ONE MAIN LANDING GEAR 34 750 kg (76 600 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 34 13 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 70 1 000 900 32 60 12 800 11 700 24 600 k = 20 MN/m³ k = 40 MN/m³ k = 80 MN/m³ k = 150 MN/m³ 40 9 500 8 400 7 300 22 ALLOWABLE WORKING STRESS 10 (kg/cm²) 26 50 (lb/in²) 28 (in) RIGID PAVEMENT THICKNESS (cm) 30 30 20 18 20 16 200 6 NOTE: THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR k ARE EXACT. FOR LOADS LESS THAN MAXIMUM, THE CURVES ARE EXACT FOR k = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF k. REFERENCE: "DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION. N_AC_070700_1_0080101_01_00 Rigid Pavement Requirements WV054, MRW 75 900 kg, CG 36 % FIGURE-7-7-0-991-008-A01 7-7-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-8-0 Rigid Pavement Requirements - LCN Conversion **ON A/C A319-100 A319neo Rigid Pavement Requirements - LCN Conversion 1. This section gives data about the rigid pavement requirements for the Load Classification Number (LCN) conversion (radius of relative stiffness). The rigid pavement requirement graphs are given at standard tire pressure for the weight variants producing (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG load for each type of aircraft. To find the aircraft weight that a rigid pavement can support, you must know the LCN of the pavement and the radius of relative stiffness (L). The calculation of the radius of relative stiffness (L) is done with the formula and the table given in ”Radius of Relative Stiffness” (L values based on Young’s Modulus (E) of 4 000 000 psi and Poisson’s Ratio ( µ ) of 0.15), see FIGURE 7-8-0-991-009-A. Example, see FIGURE 7-8-0-991-010-A, calculation of the aircraft weight through the radius of relative stiffness (L) of the rigid pavement for the MLG: - An aircraft with a MRW of 62 400 kg (137 575 lb), - The radius of relative stiffness is shown at 762 mm (30 in) with a related LCN of 56. The weight on one MLG is 25 000 kg (55 125 lb). The following tables provide LCN data in a tabular format similar to the one used by ICAO in the ”Aerodrome Design Manual Part 3, Pavements - Edition 1977”. In order to use the system accurately you should know the total pavement radius of relative stiffness (L-value) for rigid pavement. However, the pavement radius of relative stiffness for a particular runway are not frequently published in the standard airport information sources (Jeppesen, AERAD, DOD, etc.). Therefore it is common practice to use a standard radius of relative stiffness (30 inches) when determining the LCN and the ESWL of the aircraft. If the LCN for an intermediate weight between the maximum ramp weight and the empty weight of the aircraft is required or if the real thickness is known, refer to the figures that follow. 2. Radius of Relative Stiffness (Other values of E and µ ) This section gives data about the rigid pavement requirements for the Load Classification Number (LCN) conversion (radius of relative stiffness) with other values of E (Young’s modulus) and µ (Poisson’s ratio). The other values of E and µ have an effect on the radius of relative stiffness (L-value). The effect of E and µ on the radius of relative stiffness (L-value) is shown in the graphs in FIGURE 7-8-0-991-014-A. The table in FIGURE 7-8-0-991-009-A shows L-values based on a Young’s modulus (E) of 4 000 000 psi and a Poisson’s ratio ( µ ) of 0.15. To find the L-value, you must know the values of E and µ . Example, see FIGURE 7-8-0-991-014-A, calculation of the L-values of the rigid pavement for an E of 3 000 000 psi. 7-8-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING The ”E” factor is 0.931. The radius of relative stiffness (L-value) is the value found in the table (see FIGURE 7-8-0-991-009A) multiplied by 0.931. NOTE : The CG in the figure title is the CG used for LCN calculation. 7-8-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 WEIGHT VARIANT ALL UP MASS (kg) A319−100 WV000 (CG 36%) A319−100 WV000 (CG 39%) A319−100 WV001 (CG 37.5%) A319−100 WV001 (CG 36%) A319−100 WV002 A319−100 WV003 (CG 38.1%) A319−100 WV003 (CG 36%) A319−100 WV004 (CG 38.1%) A319−100 WV004 (CG 36%) A319−100 WV005 (CG 37.5%) A319−100 WV005 (CG 36%) A319−100 WV006 (CG 36.52%) A319−100 WV006 (CG 36%) A319−100 WV007 A319−100 WV008 (CG 39%) A319−100 WV008 (CG 36%) 64 400 41 000 64 400 41 000 70 400 41 000 70 400 41 000 75 900 41 000 68 400 41 000 68 400 41 000 68 400 41 000 68 400 41 000 70 400 41 000 70 400 41 000 73 900 41 000 73 900 41 000 75 900 41 000 64 400 41 000 64 400 41 000 LOAD ON TIRE ONE MAIN PRESSURE GEAR LEG (MPa) (%) 45.7 45.7 46.3 46.3 46.1 46.0 45.8 45.7 45.8 45.7 46.1 46.1 45.7 45.7 46.1 46.1 45.7 45.7 46.1 46.0 45.8 45.7 45.9 45.8 45.8 45.7 45.8 45.7 46.3 46.3 45.7 45.7 1.19 1.19 1.29 1.29 1.38 1.25 1.25 1.25 1.25 1.29 1.29 1.34 1.34 1.38 1.19 1.19 RIGID PAVEMENT ESWL LCN x 1 000 kg x 1 000 lb L = 760 mm (30 in) 43 20 65 12 26 41 44 20 66 42 12 27 22 48 74 42 12 26 21 47 73 42 12 26 23 51 81 43 12 26 46 21 71 42 12 27 46 70 21 42 12 26 46 21 71 42 12 27 46 21 70 42 12 26 74 22 48 42 12 26 21 47 73 42 12 26 23 50 78 42 12 26 50 22 78 42 12 26 51 81 23 43 12 26 44 20 66 42 12 27 20 43 65 12 26 41 N_AC_070800_1_0060101_01_00 Rigid Pavement Requirements LCN Table (Sheet 1 of 2) FIGURE-7-8-0-991-006-A01 7-8-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 WEIGHT VARIANT ALL UP MASS (kg) A319−100 WV009 (CG 38.8%) A319−100 WV009 (CG 36%) A319−100 WV011 (CG 38.8%) A319−100 WV011 (CG 36%) A319−100 WV012 (CG 39%) A319−100 WV012 (CG 36%) A319 CJ WV002 A319 CJ WV005 A319 CJ WV010 66 400 41 000 66 400 41 000 66 400 41 000 66 400 41 000 62 400 41 000 62 400 41 000 75 900 41 000 70 400 41 000 76 900 41 000 LOAD ON TIRE ONE MAIN PRESSURE GEAR LEG (MPa) (%) 46.3 46.2 45.7 45.7 46.3 46.2 45.7 45.7 46.3 46.3 45.7 45.7 45.8 45.8 45.8 45.7 45.7 45.8 1.25 1.25 1.25 1.25 1.19 1.19 1.38 1.38 1.38 RIGID PAVEMENT ESWL LCN x 1 000 kg x 1 000 lb L = 760 mm (30 in) 20 45 69 12 27 42 20 44 68 12 26 42 45 20 69 12 27 42 44 68 20 42 12 26 42 19 64 42 12 27 19 42 63 41 12 26 51 23 81 43 12 26 47 76 21 43 12 26 52 23 82 43 12 26 N_AC_070800_1_0060102_01_00 Rigid Pavement Requirements LCN Table (Sheet 2 of 2) FIGURE-7-8-0-991-006-A01 7-8-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo WEIGHT VARIANT ALL UP MASS (kg) A319NEO WV050 A319NEO WV051 A319NEO WV052 A319NEO WV053 A319NEO WV054 A319NEO WV055 64 400 41 000 64 400 41 000 70 400 41 000 70 400 41 000 75 900 41 000 75 900 41 000 LOAD ON TIRE ONE MAIN PRESSURE GEAR LEG (MPa) (%) 46.3 46.3 46.4 46.3 46.0 46.0 46.0 46.0 45.8 45.7 45.7 45.7 1.19 1.19 1.29 1.29 1.38 1.38 RIGID PAVEMENT ESWL LCN x 1 000 kg x 1 000 lb L = 760 mm (30 in) 44 20 66 12 27 42 44 20 66 42 12 27 22 48 74 42 12 26 22 48 74 42 12 26 23 51 81 42 12 26 51 23 81 42 12 26 N_AC_070800_1_0070101_01_00 Rigid Pavement Requirements LCN Table FIGURE-7-8-0-991-007-A01 7-8-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo RADIUS OF RELATIVE STIFFNESS (L) VALUES IN INCHES L= 4 WHERE Ed 12 (1 − = 24.1652 4 )k d k E = YOUNG’S MODULUS = 4 x 10 psi k = SUBGRADE MODULUS, lb/in d = RIGID PAVEMENT THICKNESS, (in) = POISSON’S RATIO = 0.15 d k = 75 k = 100 k = 150 k = 200 k = 250 k = 300 k = 350 k = 400 k = 550 6.0 6.5 7.0 7.5 31.48 33.43 35.34 37.22 29.30 31.11 32.89 34.63 26.47 28.11 29.72 31.29 24.63 26.16 27.65 29.12 23.30 24.74 26.15 27.54 22.26 23.64 24.99 26.32 21.42 22.74 24.04 25.32 20.72 22.00 23.25 24.49 19.13 20.31 21.47 22.61 8.0 8.5 9.0 9.5 39.06 40.88 42.67 44.43 36.35 38.04 39.71 41.35 32.85 34.37 35.88 37.36 30.57 31.99 33.39 34.77 28.91 30.25 31.58 32.89 27.62 28.91 30.17 31.42 26.58 27.81 29.03 30.23 25.70 26.90 28.08 29.24 23.74 24.84 25.93 27.00 10.0 10.5 11.0 11.5 46.18 47.90 49.60 51.28 42.97 44.57 46.16 47.72 38.83 40.28 41.71 43.12 36.14 37.48 38.81 40.13 34.17 35.45 36.71 37.95 32.65 33.87 35.07 36.26 31.42 32.59 33.75 34.89 30.39 31.52 32.64 33.74 28.06 29.11 30.14 31.16 12.0 12.5 13.0 13.5 52.94 54.59 56.22 57.83 49.27 50.80 52.32 53.82 44.52 45.90 47.27 48.63 41.43 42.72 43.99 45.26 39.18 40.40 41.61 42.80 37.44 38.60 39.75 40.89 36.02 37.14 38.25 39.35 34.84 35.92 36.99 38.06 32.17 33.17 34.16 35.14 14.0 14.5 15.0 15.5 59.43 61.02 62.59 64.15 55.31 56.78 58.25 59.70 49.98 51.31 52.63 53.94 46.51 47.75 48.98 50.20 43.98 45.16 46.32 47.47 42.02 43.15 44.26 45.36 40.44 41.51 42.58 43.64 39.11 40.15 41.19 42.21 36.12 37.08 38.03 38.98 16.0 16.5 17.0 17.5 65.69 67.23 68.75 70.26 61.13 62.56 63.98 65.38 55.24 56.53 57.81 59.08 51.41 52.61 53.80 54.98 48.62 49.75 50.88 52.00 46.45 47.54 48.61 49.68 44.70 45.74 46.77 47.80 43.23 44.24 45.24 46.23 39.92 40.85 41.78 42.70 18.0 19.0 20.0 21.0 71.76 74.73 77.66 80.55 66.78 69.54 72.27 74.96 60.34 62.84 65.30 67.74 56.15 58.48 60.77 63.04 53.11 55.31 57.47 59.62 50.74 52.84 54.91 56.96 48.82 50.84 52.84 54.81 47.22 49.17 51.10 53.01 43.61 45.41 47.19 48.95 22.0 23.0 24.0 25.0 83.41 86.24 89.04 91.81 77.63 80.26 82.86 85.44 70.14 72.52 74.87 77.20 65.28 67.49 69.68 71.84 61.73 63.83 65.90 67.95 58.98 60.98 62.96 64.92 56.75 58.68 60.58 62.46 54.89 56.75 58.59 60.41 50.69 52.41 54.11 55.79 REFERENCE: PORTLAND CEMENT ASSOCIATION. N_AC_070800_1_0090101_01_00 Radius of Relative Stiffness (L) FIGURE-7-8-0-991-009-A01 7-8-0 Page 6 May 01/14 7-8-0 0 10 20 30 40 50 60 70 80 20 1 000 1 500 2 000 2 500 40 50 60 70 80 90 100 30 50 60 70 80 LOAD CLASSIFICATION NUMBER (LCN) 40 WEIGHT ON ONE MAIN LANDING GEAR 28 530 kg (62 900 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 90 0 5 10 15 20 25 30 35 46x17R20 (46x16−20) TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. RADIUS OF RELATIVE STIFFNESS (in) 30 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 750 RADIUS OF RELATIVE STIFFNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) N_AC_070800_1_0100101_01_00 Rigid Pavement Requirements - LCN WV012, MRW 62 400 kg, CG 36 % FIGURE-7-8-0-991-010-A01 Page 7 May 01/14 7-8-0 0 10 20 30 40 50 60 70 80 10 750 1 000 1 500 30 40 2 500 50 60 70 80 100 10 30 40 50 60 80 100 LOAD CLASSIFICATION NUMBER (LCN) 20 WEIGHT ON ONE MAIN LANDING GEAR 35 180 kg (77 550 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 0 5 10 15 20 25 30 35 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. RADIUS OF RELATIVE STIFFNESS (in) 20 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 500 RADIUS OF RELATIVE STIFFNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) N_AC_070800_1_0110101_01_00 Rigid Pavement Requirements - LCN WV010, MRW 76 900 kg, CG 36 % FIGURE-7-8-0-991-011-A01 Page 8 May 01/14 7-8-0 0 10 20 30 40 50 60 70 80 20 1 000 1 500 2 000 2 500 40 50 60 70 80 90 100 30 50 60 70 80 LOAD CLASSIFICATION NUMBER (LCN) 40 WEIGHT ON ONE MAIN LANDING GEAR 29 830 kg (65 775 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 90 0 5 10 15 20 25 30 35 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. RADIUS OF RELATIVE STIFFNESS (in) 30 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 750 RADIUS OF RELATIVE STIFFNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) N_AC_070800_1_0120101_01_00 Rigid Pavement Requirements - LCN WV050, MRW 64 400 kg, CG 39 % FIGURE-7-8-0-991-012-A01 Page 9 May 01/14 7-8-0 0 10 20 30 40 50 60 70 80 20 1 000 1 500 2 000 2 500 40 50 60 70 80 90 100 30 50 60 70 80 LOAD CLASSIFICATION NUMBER (LCN) 40 WEIGHT ON ONE MAIN LANDING GEAR 34 750 kg (76 600 lb) 25 000 kg (55 125 lb) 20 000 kg (44 100 lb) 15 000 kg (33 075 lb) 10 000 kg (22 050 lb) 90 0 5 10 15 20 25 30 35 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) NOTE: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL PART 2 PAR 4.1.3 SECOND EDITION 1965. RADIUS OF RELATIVE STIFFNESS (in) 30 MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG 750 RADIUS OF RELATIVE STIFFNESS (mm) @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo EQUIVALENT SINGLE WHEEL LOAD (1 000 kg) EQUIVALENT SINGLE WHEEL LOAD (1 000 lb) N_AC_070800_1_0130101_01_00 Rigid Pavement Requirements - LCN WV054, MRW 75 900 kg, CG 36 % FIGURE-7-8-0-991-013-A01 Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo EFFECT OF E ON L VALUES 1.10 1.05 E FACTOR 1.00 0.95 0.90 0.85 0.80 0 1 2 3 4 5 E, YOUNG’S MODULUS (10 psi) EFFECT OF ON L VALUES 1.015 FACTOR 1.010 1.005 1.000 0.995 0.00 0.05 0.10 0.15 0.20 0.25 , POISSON’S RATIO NOTE: BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF RADIUS OF RELATIVE STIFFNESS (L) TABLE. N_AC_070800_1_0140101_01_00 Radius of Relative Stiffness (Effect of E and µ on ”L” Values) FIGURE-7-8-0-991-014-A01 7-8-0 Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements **ON A/C A319-100 A319neo Aircraft Classification Number - Flexible and Rigid Pavements 1. This section gives data about the Aircraft Classification Number (ACN) for an aircraft gross weight in relation to a subgrade strength value for flexible and rigid pavement. The flexible and rigid pavement requirement graphs are given at standard tire pressure for the weight variants producing (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG load for each type of aircraft. To find the ACN of an aircraft on flexible and rigid pavement, you must know the aircraft gross weight and the subgrade strength. NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on that pavement, subject to any limitation on the tire pressure. (Ref: ICAO Aerodrome Design Manual, Part 3, Chapter 1, Second Edition 1983). Example, see FIGURE 7-9-0-991-007-A (sheet 1), calculation of the ACN for flexible pavement for: - An aircraft with a MRW of 62 400 kg (137 575 lb), - An aircraft gross weight of 55 000 kg (121 250 lb), - A low subgrade strength (code C). The ACN for flexible pavement is 29. Example, see FIGURE 7-9-0-991-007-A (sheet 2), calculation of the ACN for rigid pavement for: - An aircraft with a MRW of 62 400 kg (137 575 lb), - An aircraft gross weight of 55 000 kg (121 250 lb), - A medium subgrade strength (code B). The ACN for rigid pavement is 30. 2. Aircraft Classification Number - ACN table The tables in FIGURE 7-9-0-991-006-A and FIGURE 7-9-0-991-009-A provide ACN data in tabular format similar to the one used by ICAO in the ”Aerodrome Design Manual Part 3, Pavements Edition 1983”. If the ACN for an intermediate weight between MRW and the minimum weight of the aircraft is required, refer to the figures that follow. NOTE : The CG in the figure title is the CG used for ACN calculation. 7-9-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 ACN FOR LOAD ON RIGID PAVEMENT TIRE ALL UP ONE MAIN WEIGHT SUBGRADES − MN/m³ MASS (kg) GEAR LEG PRESSURE VARIANT (MPa) High Medium Low Ultra−low (%) 150 80 40 20 45.7 39 37 64 400 34 A319−100 41 1.19 WV000 (CG 36%) 45.7 23 41 000 20 24 22 39 37 35 64 400 46.3 A319−100 41 1.19 WV000 (CG 39%) 25 23 20 41 000 46.3 22 46 44 39 70 400 46.1 A319−100 42 1.29 WV001 (CG 37.5%) 41 000 25 46.0 24 22 21 46 44 39 70 400 45.8 A319−100 41 1.29 WV001 (CG 36%) 45.7 25 23 41 000 22 21 51 49 46 44 75 900 45.8 A319−100 1.38 WV002 45.7 25 41 000 24 22 21 44 40 38 68 400 46.1 A319−100 42 1.25 WV003 (CG 38.1%) 41 000 25 23 46.1 22 21 45.7 44 40 37 68 400 A319−100 42 1.25 WV003 (CG 36%) 45.7 23 20 41 000 24 22 44 40 38 68 400 46.1 A319−100 42 1.25 WV004 (CG 38.1%) 41 000 25 23 46.1 22 21 45.7 44 40 37 68 400 A319−100 42 1.25 WV004 (CG 36%) 45.7 23 20 41 000 24 22 46 44 39 70 400 46.1 A319−100 42 1.29 WV005 (CG 37.5%) 41 000 25 46.0 24 22 21 46 44 39 70 400 45.8 A319−100 41 1.29 WV005 (CG 36%) 45.7 25 23 41 000 22 21 49 47 44 73 900 45.9 A319−100 42 1.34 WV006 (CG 36.52%) 41 000 25 45.8 24 22 21 49 47 44 73 900 45.8 A319−100 42 1.34 WV006 (CG 36%) 45.7 25 41 000 24 22 21 ACN FOR FLEXIBLE PAVEMENT SUBGRADES − CBR High Medium Low Ultra−low 15 10 6 3 32 36 32 41 19 19 21 24 32 36 33 42 19 19 24 21 35 46 36 41 19 19 24 21 40 46 36 35 19 19 24 21 45 50 40 39 19 19 21 24 45 35 39 34 19 19 21 24 45 35 39 34 19 19 21 24 45 39 35 34 19 19 21 24 45 39 35 34 19 19 21 24 46 36 35 41 19 19 21 24 40 46 36 35 19 19 21 24 49 39 43 37 19 19 24 21 49 39 43 37 19 19 24 21 N_AC_070900_1_0060101_01_00 Aircraft Classification Number ACN Table (Sheet 1 of 2) FIGURE-7-9-0-991-006-A01 7-9-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 WEIGHT VARIANT A319−100 WV007 A319−100 WV008 (CG 39%) A319−100 WV008 (CG 36%) A319−100 WV009 (CG 38.8%) A319−100 WV009 (CG 36%) A319−100 WV011 (CG 38.8%) A319−100 WV011 (CG 36%) A319−100 WV012 (CG 39%) A319−100 WV012 (CG 36%) A319 CJ WV002 A319 CJ WV005 A319 CJ WV010 ACN FOR LOAD ON RIGID PAVEMENT TIRE ALL UP ONE MAIN SUBGRADES − MN/m³ MASS (kg) GEAR LEG PRESSURE (MPa) High Medium Low Ultra−low (%) 150 80 40 20 75 900 45.8 44 46 49 51 1.38 45.7 41 000 25 21 22 24 35 37 39 64 400 46.3 41 1.19 20 23 25 41 000 46.3 22 45.7 37 39 34 64 400 41 1.19 45.7 23 20 41 000 24 22 39 43 37 66 400 46.3 41 1.25 25 46.2 41 000 24 21 22 45.7 38 36 66 400 41 42 1.25 45.7 23 20 41 000 24 22 39 43 37 66 400 46.3 41 1.25 25 41 000 46.2 24 21 22 45.7 38 36 66 400 41 42 1.25 45.7 23 20 41 000 24 22 36 38 40 33 62 400 46.3 1.19 23 25 20 41 000 46.3 22 45.7 33 35 37 39 62 400 1.19 45.7 41 000 20 23 22 24 44 46 49 51 75 900 45.8 1.38 41 000 25 45.8 21 22 24 40 44 46 70 400 45.8 42 1.38 45.7 41 000 25 21 22 24 45.7 76 900 44 47 49 51 1.38 45.8 25 41 000 21 22 24 ACN FOR FLEXIBLE PAVEMENT SUBGRADES − CBR High Medium Low Ultra−low 15 10 6 3 45 39 40 50 19 19 21 24 32 33 36 42 19 19 21 24 32 32 36 41 19 19 21 24 33 34 38 44 19 19 21 24 33 34 37 43 19 19 24 21 33 34 38 44 19 19 24 21 33 34 37 43 19 19 24 21 31 32 35 41 19 19 21 24 30 31 34 40 19 19 21 24 45 39 40 50 19 19 21 24 36 37 40 46 19 19 21 24 45 39 51 41 19 19 21 24 N_AC_070900_1_0060102_01_00 Aircraft Classification Number ACN Table (Sheet 2 of 2) FIGURE-7-9-0-991-006-A01 7-9-0 Page 3 May 01/14 7-9-0 15 20 25 30 35 40 45 35 90 40 ALPHA FACTOR = 0.9 SUBGRADE STRENGTH D − CBR 3 (ULTRA LOW) C − CBR 6 (LOW) B − CBR 10 (MEDIUM) A − CBR 15 (HIGH) 80 45 50 (x 1 000 kg) 110 (x 1 000 lb) 55 120 130 60 140 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. AIRCRAFT GROSS WEIGHT 100 46x17R20 (46x16−20) TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) 65 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0070101_01_00 Aircraft Classification Number Flexible Pavement - WV012, MRW 62 400 kg, CG 36 % (Sheet 1 of 2) FIGURE-7-9-0-991-007-A01 Page 4 May 01/14 7-9-0 15 20 25 30 35 40 45 35 90 40 45 50 (x 1 000 kg) 110 (x 1 000 lb) 55 120 130 60 140 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. AIRCRAFT GROSS WEIGHT 100 SUBGRADE STRENGTH D − k = 20 MN/m³ (ULTRA LOW) C − k = 40 MN/m³ (LOW) B − k = 80 MN/m³ (MEDIUM) A − k = 150 MN/m³ (HIGH) 80 46x17R20 (46x16−20) TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) 65 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0070102_01_00 Aircraft Classification Number Rigid Pavement - WV012, MRW 62 400 kg, CG 36 % (Sheet 2 of 2) FIGURE-7-9-0-991-007-A01 Page 5 May 01/14 7-9-0 10 15 20 25 30 35 40 45 50 55 60 35 80 100 40 45 ALPHA FACTOR = 0.9 SUBGRADE STRENGTH D − CBR 3 (ULTRA LOW) C − CBR 6 (LOW) B − CBR 10 (MEDIUM) A − CBR 15 (HIGH) 90 50 110 130 AIRCRAFT GROSS WEIGHT 55 60 (x 1 000 kg) 120 140 65 150 70 160 75 170 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. (x 1 000 lb) 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) 80 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0080101_01_00 Aircraft Classification Number Flexible Pavement - WV010, MRW 76 900 kg, CG 36 % (Sheet 1 of 2) FIGURE-7-9-0-991-008-A01 Page 6 May 01/14 7-9-0 10 15 20 25 30 35 40 45 50 55 60 35 80 100 110 40 45 50 SUBGRADE STRENGTH D − k = 20 MN/m³ (ULTRA LOW) C − k = 40 MN/m³ (LOW) B − k = 80 MN/m³ (MEDIUM) A − k = 150 MN/m³ (HIGH) 90 130 AIRCRAFT GROSS WEIGHT 55 60 (x 1 000 kg) 120 140 65 150 70 160 75 170 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. (x 1 000 lb) 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) 80 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0080102_01_00 Aircraft Classification Number Rigid Pavement - WV010, MRW 76 900 kg, CG 36 % (Sheet 2 of 2) FIGURE-7-9-0-991-008-A01 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo WEIGHT VARIANT A319NEO WV050 A319NEO WV051 A319NEO WV052 A319NEO WV053 A319NEO WV054 A319NEO WV055 ACN FOR LOAD ON RIGID PAVEMENT TIRE ALL UP ONE MAIN SUBGRADES − MN/m³ MASS (kg) GEAR LEG PRESSURE (MPa) High Medium Low Ultra−low (%) 150 80 40 20 39 37 64 400 46.3 35 41 1.19 25 23 41 000 46.3 20 22 39 37 64 400 46.3 35 41 1.19 25 23 41 000 46.3 20 22 46 44 70 400 46.1 39 42 1.29 25 41 000 46.0 24 22 21 46 44 70 400 46.1 39 42 1.29 25 41 000 46.0 24 22 21 51 49 46 75 900 45.8 44 1.38 45.7 25 41 000 24 22 21 51 49 46 75 900 45.8 44 1.38 45.7 25 41 000 24 22 21 ACN FOR FLEXIBLE PAVEMENT SUBGRADES − CBR High Medium Low Ultra−low 15 10 6 3 36 33 32 42 19 19 24 21 36 33 32 42 19 19 24 21 46 36 35 41 19 19 24 21 46 36 35 41 19 19 24 21 45 50 40 39 19 19 21 24 45 50 40 39 19 19 24 21 N_AC_070900_1_0090101_01_00 Aircraft Classification Number ACN Table FIGURE-7-9-0-991-009-A01 7-9-0 Page 8 May 01/14 7-9-0 15 20 25 30 35 40 45 35 90 40 ALPHA FACTOR = 0.9 SUBGRADE STRENGTH D − CBR 3 (ULTRA LOW) C − CBR 6 (LOW) B − CBR 10 (MEDIUM) A − CBR 15 (HIGH) 80 45 50 (x 1 000 kg) 110 (x 1 000 lb) 55 120 130 60 140 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. AIRCRAFT GROSS WEIGHT 100 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) 65 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0100101_01_00 Aircraft Classification Number Flexible Pavement - WV050, MRW 64 400 kg, CG 39 % (Sheet 1 of 2) FIGURE-7-9-0-991-010-A01 Page 9 May 01/14 7-9-0 15 20 25 30 35 40 45 35 90 40 45 50 (x 1 000 kg) 110 (x 1 000 lb) 55 120 130 60 140 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. AIRCRAFT GROSS WEIGHT 100 SUBGRADE STRENGTH D − k = 20 MN/m³ (ULTRA LOW) C − k = 40 MN/m³ (LOW) B − k = 80 MN/m³ (MEDIUM) A − k = 150 MN/m³ (HIGH) 80 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi) 65 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0100102_01_00 Aircraft Classification Number Rigid Pavement - WV050, MRW 64 400 kg, CG 39 % (Sheet 2 of 2) FIGURE-7-9-0-991-010-A01 Page 10 May 01/14 7-9-0 15 20 25 30 35 40 45 50 55 35 80 100 40 45 ALPHA FACTOR = 0.9 SUBGRADE STRENGTH D − CBR 3 (ULTRA LOW) C − CBR 6 (LOW) B − CBR 10 (MEDIUM) A − CBR 15 (HIGH) 90 50 110 130 AIRCRAFT GROSS WEIGHT 55 60 (x 1 000 kg) 120 140 65 150 70 160 75 170 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. (x 1 000 lb) 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) 80 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0110101_01_00 Aircraft Classification Number Flexible Pavement - WV054, MRW 75 900 kg, CG 36 % (Sheet 1 of 2) FIGURE-7-9-0-991-011-A01 Page 11 May 01/14 7-9-0 15 20 25 30 35 40 45 50 55 35 80 100 110 40 45 50 SUBGRADE STRENGTH D − k = 20 MN/m³ (ULTRA LOW) C − k = 40 MN/m³ (LOW) B − k = 80 MN/m³ (MEDIUM) A − k = 150 MN/m³ (HIGH) 90 130 AIRCRAFT GROSS WEIGHT 55 60 (x 1 000 kg) 120 140 65 150 70 160 75 170 ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983. SEE SECTION 7−4−0. (x 1 000 lb) 46x17R20 TIRES TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi) 80 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319neo AIRCRAFT CLASSIFICATION NUMBER (ACN) N_AC_070900_1_0110102_01_00 Aircraft Classification Number Rigid Pavement - WV054, MRW 75 900 kg, CG 36 % (Sheet 2 of 2) FIGURE-7-9-0-991-011-A01 Page 12 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING SCALED DRAWINGS 8-0-0 SCALED DRAWINGS **ON A/C A319-100 A319neo Scaled Drawings 1. This section provides the scaled drawings. NOTE : When printing this drawing, make sure to adjust for proper scaling. 8-0-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 15 5 10 METERS 0 0 10 FEET 20 30 40 50 **ON A/C A319-100 A319neo 0 0 10 FEET 20 30 5 10 METERS 40 50 15 NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING. N_AC_080000_1_0020101_01_00 Scaled Drawing FIGURE-8-0-0-991-002-A01 8-0-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING AIRCRAFT RESCUE AND FIRE FIGHTING 10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING **ON A/C A319-100 A319neo Aircraft Rescue and Fire Fighting 1. Aircraft Rescue and Fire Fighting Charts This sections gives data related to aircraft rescue and fire fighting. The figures contained in this section are the figures that are in the Aircraft Rescue and Fire Fighting Charts poster available for download on AIRBUSWorld and the Airbus website. 10-0-0 Page 1 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING / MAY 2014 **ON A/C A319-100 A319neo N_AC_100000_1_0170101_01_00 Front Page FIGURE-10-0-0-991-017-A01 10-0-0 Page 2 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_100000_1_0180101_01_00 Highly Flammable and Hazardous Materials and Components FIGURE-10-0-0-991-018-A01 10-0-0 Page 3 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING BAT−1 FR1 A ACCESS VIA ACCESS DOOR 822 FR24 BAT−2 A **ON A/C A319-100 A319neo N_AC_100000_1_0560101_01_00 Batteries Location and Access FIGURE-10-0-0-991-056-A01 10-0-0 Page 4 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_100000_1_0190101_01_00 Wheel/Brake Overheat Wheel Safety Area (Sheet 1 of 2) FIGURE-10-0-0-991-019-A01 10-0-0 Page 5 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_100000_1_0190102_01_00 Wheel/Brake Overheat Recommendations (Sheet 2 of 2) FIGURE-10-0-0-991-019-A01 10-0-0 Page 6 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING AFRP + CFRP Aramid Fiber Reinforced Plastic (AFRP) Glass Fiber Reinforced Plastic (GFRP) Carbon Fiber Reinforced Plastic (CFRP) **ON A/C A319-100 A319neo N_AC_100000_1_0200101_01_00 Composite Materials FIGURE-10-0-0-991-020-A01 10-0-0 Page 7 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING A A B B **ON A/C A319-100 A319neo N_AC_100000_1_0210101_01_00 L/G Ground Lock Safety Devices FIGURE-10-0-0-991-021-A01 10-0-0 Page 8 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING −9 GRID EQUALS 1 m (3.28 ft) IN REALITY −6 0 −3 EMERGENCY DESCENT THROUGH THE WINDOW OPENING WITH THE ESCAPE ROPE FWD CABIN ESCAPE SLIDE COCKPIT ESCAPE ROPE OFF WING ESCAPE SLIDE AFT CABIN ESCAPE SLIDE **ON A/C A319-100 A319neo N_AC_100000_1_0220101_01_00 Emergency Evacuation Devices FIGURE-10-0-0-991-022-A01 10-0-0 Page 9 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_100000_1_0230101_01_00 Pax/Crew Doors FIGURE-10-0-0-991-023-A01 10-0-0 Page 10 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_100000_1_0240101_01_00 Emergency Exit Hatch FIGURE-10-0-0-991-024-A01 10-0-0 Page 11 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 134AR /154AR 198CB **ON A/C A319-100 A319neo N_AC_100000_1_0250101_01_00 FWD and AFT Lower Deck Cargo Doors FIGURE-10-0-0-991-025-A01 10-0-0 Page 12 May 01/14 10-0-0 ENG 1 FIRE OFF OFF RWY TURN OFF ON L OFF RETRACT OFF ON LAND R OFF WING ON ON ON BEACON FAULT FAULT EXT LT ENG 1 ANTI ICE OFF NOSE OFF 1 OFF TAXI 2 B OFF BUS TIE A U T O AC ESS BUS OFF FAULT A U T O C ON AVAIL START ON FAULT MASTER SW APU ON V ON FAULT A U T O BRT OFF SIGNS SEAT BELTS NO SMOKING ON ON A U T O OFF OFF OFF OFF DIM BRT OFF OFF ARM ON DIM BRT TEST ON ANN LT EMER EXIT LT OVHD INTEG LT INT LT STBY COMPASS DOME ON UP E L E C 35VU F I R E 25VU DITCHING FAULT TEST DISCH SQUIB AGENT 2 IDG 2 LDG ELEV AUTO OFF FAULT GEN 2 AC BUS 2 CABIN PRESS ALTN FAULT FIRE PUSH 2 DC BUS 2 ENG MAN V/S CTL MODE SEL ON AVAIL A AC ESS FEED DISCH SQUIB AGENT 1 D EXT PWR BAT 2 TEST PROBE/WINDOW HEAT OFF A BAT DISCH SQUIB AGENT FIRE PUSH APU FAULT T.O NAV & LOGO ON ON FAULT ENG 2 OFF FAULT FAULT V APU GEN BAT 1 GEN 1 AC BUS 1 DC BUS 1 PUSH WING A U T O FAULT IDG 1 GALY & CAB A U T OFF O OFF COMMERCIAL TEST SQUIB DISCH SQUIB AGENT 2 E C DISCH STROBE ON E L E C F I R E AGENT 1 B ENG A U T O ON 2 OFF A U T O OFF CAB FANS DISCH RAIN RPLNT D FAST SLOW OVRD FAULT WIPER DISCH SMOKE VENTILATION TEST AFT HOT OFF OFF COLD FAULT AFT AFT ISOL VALVE 22VU RESET APU SHUT OFF ADIRU & APU FIRE AVNCS VENT FAULT HOT AIR CARGO SMOKE EXTRACT DISCH SMOKE FWD MAIN START ON 1 OVRD FAULT BLOWER DISCH CKPT CALL FLT INT LIGHT TEST CKPT CALL AVAIL CARGO ELT NOT IN USE EXT PWR 108VU CRANK ENG 1 MASTER1 1 FAULT FIRE OFF ON ENG E MODE NORM 2 FAULT FIRE ENG 2 IGN START MASTER2 OFF ON @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_100000_1_0260101_01_00 Control Panels FIGURE-10-0-0-991-026-A01 Page 13 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING 316AR A 315AL A **ON A/C A319-100 A319neo N_AC_100000_1_0270101_01_00 APU Access Door FIGURE-10-0-0-991-027-A01 10-0-0 Page 14 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING K4 K3 **ON A/C A319-100 A319neo N_AC_100000_1_0280101_01_00 Aircraft Ground Clearances FIGURE-10-0-0-991-028-A01 10-0-0 Page 15 May 01/14 @A319/A319NEO AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING **ON A/C A319-100 A319neo N_AC_100000_1_0290101_01_00 Structural Break-in Points FIGURE-10-0-0-991-029-A01 10-0-0 Page 16 May 01/14

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