@AIRBUS
A350-900
AIRCRAFT CHARACTERISTICS
AIRPORT AND MAINTENANCE PLANNING
AC
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© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
31707 Blagnac Cedex
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Issue: Jun 01/13
Rev: Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 2 - Apr 01/15
LOCATIONS
CHAPTER 2
Section 2-1
Subject 2-1-0
General Aircraft Characteristics Data
Section 2-3
Subject 2-3-0
Ground Clearances
FIGURE Ground Clearances
FIGURE Ground Clearances
FIGURE Ground Clearances
FIGURE Ground Clearances
FIGURE Ground Clearances
FIGURE Ground Clearances
FIGURE Flap Tracks - Retracted
FIGURE Ground Clearances
Section 2-7
Subject 2-7-0
CHG
CODE
DESCRIPTIONS OF CHANGE
R
R
DESCRIPTION TITLE UPDATED
R
R
N
N
N
N
N
N
ILLUSTRATION
ILLUSTRATION
ILLUSTRATION
ILLUSTRATION
ILLUSTRATION
ILLUSTRATION
N
ILLUSTRATION ADDED
FIGURE Forward Passenger/Crew Doors
R
FIGURE Aft Passenger/Crew Doors
R
FIGURE Nose Landing Gear Doors
R
FIGURE Main Landing Gear Doors
R
ADDED
ADDED
ADDED
ADDED
ADDED
ADDED
Section 2-8
Subject 2-8-0
Escape Slides
R
FIGURE Escape Slides
N
Section 2-9
Subject 2-9-0
ILLUSTRATION ADDED
R
Landing Gear
R
FIGURE Main Landing Gear
R
HIGHLIGHTS
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
FIGURE Nose Landing Gear
Subject 2-9-1
CHG
CODE
R
DESCRIPTIONS OF CHANGE
N
Landing Gear Maintenance Pits
N
FIGURE Maintenance Pit Envelopes
N
ILLUSTRATION ADDED
FIGURE NLG/MLG Extension/Retraction
Pit
FIGURE NLG/MLG Shock Absorber
Removal Pit
FIGURE NLG/MLG Removal Pit
N
ILLUSTRATION ADDED
N
ILLUSTRATION ADDED
N
ILLUSTRATION ADDED
Section 2-14
Subject 2-14-1
Jacking for Maintenance
R
FIGURE Jacking for Maintenance
R
Subject 2-14-2
R
CHAPTER 3
Section 3-1
Subject 3-1-0
N
N
N
General Information
Section 3-3
Subject 3-3-0
N
N
N
Take-Off Weight Limitation
FIGURE ISA Conditions
FIGURE ISA + 15 ˚C (+59 ˚F)
Conditions
Section 3-4
Subject 3-4-0
N
N
N
N
N
Landing Field Length
N
FIGURE Landing Field Length
N
Section 3-5
Subject 3-5-0
Final Approach Speed
ILLUSTRATION ADDED
ILLUSTRATION ADDED
ILLUSTRATION ADDED
N
N
N
HIGHLIGHTS
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
CHAPTER 5
Section 5-4
Subject 5-4-1
Grounding (Earthing) Points
CHG
CODE
DESCRIPTIONS OF CHANGE
R
R
Subject 5-4-2
Hydraulic System
R
Subject 5-4-3
Electrical System
Subject 5-4-10
R
N
Cargo Control Panels
N
FIGURE Forward Cargo Control Panels
N
ILLUSTRATION ADDED
FIGURE Aft Cargo Control Panels
N
ILLUSTRATION ADDED
R
NOTE AMENDED
Section 5-6
Subject 5-6-0
Ground Pneumatic Power Requirements
Section 5-8
Subject 5-8-0
R
Ground Towing Requirements
R
DESCRIPTION TITLE UPDATED
CROSS REFERENCED MANUAL(S)
ADDED/REVISED/DELETED
FIGURE Ground Towing Requirements
R
ILLUSTRATION REVISED
CHAPTER 6
Section 6-1
Subject 6-1-0
Engine Exhaust Velocities and
Temperatures
Subject 6-1-1
Engine Exhaust Velocities - Ground Idle
Power
FIGURE Ground Idle Power - TRENT
XWB Engine
Subject 6-1-2
R
N
N
N
N
N
N
ILLUSTRATION ADDED
N
HIGHLIGHTS
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
Engine Exhaust Temperatures - Ground
Idle Power
FIGURE Ground Idle Power - TRENT
XWB-84 Engine
Subject 6-1-3
CHG
CODE
N
N
DESCRIPTIONS OF CHANGE
ILLUSTRATION ADDED
N
Engine Exhaust Velocities - Breakaway
Power
FIGURE Breakaway Power (11% MTO
Thrust) - TRENT XWB-84 Engine
N
N
ILLUSTRATION ADDED
FIGURE Breakaway Power (22% MTO
Thrust) - TRENT XWB-84 Engine
N
ILLUSTRATION ADDED
Subject 6-1-4
N
Engine Exhaust Temperatures Breakaway Power
N
FIGURE Breakaway Power (11% MTO
Thrust) - TRENT XWB-84 Engine
N
ILLUSTRATION ADDED
FIGURE Breakaway Power (22% MTO
Thrust) - TRENT XWB-84 Engine
N
ILLUSTRATION ADDED
Subject 6-1-5
N
Engine Exhaust Velocities - Max Take-Off
Power
FIGURE Max Take-Off Power - TRENT
XWB-84 Engine (Single)
N
N
ILLUSTRATION ADDED
FIGURE Max Take-Off Power - TRENT
XWB-84 Engine (Twin)
N
ILLUSTRATION ADDED
Subject 6-1-6
Engine Exhaust Temperatures - Max
Take-Off Power
FIGURE Max Take-Off Power - TRENT
XWB-84 Engine
Section 6-3
Subject 6-3-1
Danger Areas of the Engines - Ground Idle
Power
N
N
N
ILLUSTRATION ADDED
N
N
N
HIGHLIGHTS
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
FIGURE Ground Idle Power - TRENT
XWB-84 Engine
Subject 6-3-3
Danger Areas of the Engines - Max TakeOff Power
FIGURE Max Take-Off Power - TRENT
XWB-84 Engine
CHG
CODE
N
DESCRIPTIONS OF CHANGE
ILLUSTRATION ADDED
N
N
N
ILLUSTRATION ADDED
CHAPTER 7
Section 7-1
Subject 7-1-0
General Information
Section 7-2
Subject 7-2-0
R
Landing Gear Footprint
R
FIGURE Landing Gear Footprint
R
Section 7-3
Subject 7-3-0
Maximum Pavement Loads
FIGURE Maximum Pavement Loads
Section 7-4
Subject 7-4-0
R
R
Landing Gear Loading on Pavement
R
FIGURE Landing Gear Loading on
Pavement
FIGURE Landing Gear Loading on
Pavement
Section 7-5
Subject 7-5-0
NOTE AMENDED
R
N
ILLUSTRATION ADDED
R
Flexible Pavement Requirements - US
Army Corps of Engineers Design Method
R
FIGURE Flexible Pavement Requirements
R
FIGURE Flexible Pavement Requirements
N
DESCRIPTION TITLE UPDATED
NOTE AMENDED
ILLUSTRATION ADDED
Section 7-6
HIGHLIGHTS
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
CHG
CODE
DESCRIPTIONS OF CHANGE
Subject 7-6-0
Flexible Pavement Requirements - LCN
Conversion
Section 7-7
Subject 7-7-0
R
Rigid Pavement Requirements - Portland
Cement Association Design Method
R
FIGURE Rigid Pavement Requirements
R
FIGURE Rigid Pavement Requirements
N
Section 7-8
Subject 7-8-0
R
Rigid Pavement Requirements - LCN
Conversion
Subject 07-08-01
R
D
Subject 07-08-02
D
Section 7-9
Subject 7-9-0
R
R
NOTE AMENDED
ILLUSTRATION ADDED
ACN/PCN Reporting System - Flexible
and Rigid Pavements
R
DESCRIPTION TITLE UPDATED
NOTE AMENDED
FIGURE ACN/PCN Reporting System WV000, MRW 268 900 kg, CG 33%
R
ILLUSTRATION REVISED
FIGURE ACN/PCN Reporting System WV001, MRW 275 900 kg, CG 33.2%
N
ILLUSTRATION ADDED
N
D
ILLUSTRATION ADDED
FIGURE ACN Table
Subject 07-09-01
CHAPTER 10
Section 10-0
Subject 10-0-0
Aircraft Rescue and Fire Fighting
R
FIGURE Front Page
R
FIGURE Highly Flammable and Hazardous
Materials and Components
R
HIGHLIGHTS
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
FIGURE Emergency Evacuation Devices
CHG
CODE
R
FIGURE FWD and AFT Lower Deck
Cargo Doors
R
FIGURE APU Compartment Access
R
FIGURE Batteries Location and Access
R
DESCRIPTIONS OF CHANGE
HIGHLIGHTS
Page 7
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 2 - Apr 01/15
CONTENT
CHG
CODE
LAST REVISION
DATE
CHAPTER 1
Subject 1-1-0
Introduction
Jun 01/13
Subject 1-2-0
Glossary
Jun 01/13
CHAPTER 2
Subject 2-1-0
General Aircraft Characteristics Data
R
Apr 01/15
Subject 2-2-0
General Aircraft Dimensions
Jun 01/13
FIGURE General Aircraft Dimensions
Sep 01/14
Subject 2-3-0
Ground Clearances
R
Apr 01/15
FIGURE Ground Clearances
R
Apr 01/15
FIGURE Ground Clearances
N
Apr 01/15
FIGURE Ground Clearances
N
Apr 01/15
FIGURE Ground Clearances
N
Apr 01/15
FIGURE Ground Clearances
N
Apr 01/15
FIGURE Ground Clearances
N
Apr 01/15
FIGURE Flap Tracks - Retracted
N
Apr 01/15
FIGURE Ground Clearances
N
Apr 01/15
Subject 2-4-0
Interior Arrangements - Plan View
Jun 01/13
FIGURE Standard Configuration
Jun 01/13
Subject 2-5-0
Interior Arrangements - Cross Section
Jun 01/13
L.E.C.
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
FIGURE Typical Configuration
LAST REVISION
DATE
Jun 01/13
Subject 2-6-0
Cargo Compartments
Jun 01/13
FIGURE Cargo Compartments
Jun 01/13
Subject 2-7-0
Door Clearances and Location
Sep 01/14
FIGURE Door Identification and Location
Sep 01/14
FIGURE Forward Passenger/Crew Doors
R
Apr 01/15
FIGURE Aft Passenger/Crew Doors
R
Apr 01/15
FIGURE Forward Cargo Compartment Door
Sep 01/14
FIGURE Aft Cargo Compartment Door
Sep 01/14
FIGURE Bulk Cargo Compartment Door
Sep 01/14
FIGURE Nose Landing Gear Doors
R
Apr 01/15
FIGURE Main Landing Gear Doors
R
Apr 01/15
Escape Slides
R
Apr 01/15
FIGURE Escape Slides
N
Apr 01/15
Landing Gear
R
Apr 01/15
FIGURE Main Landing Gear
R
Apr 01/15
FIGURE Nose Landing Gear
R
Apr 01/15
Landing Gear Maintenance Pits
N
Apr 01/15
FIGURE Maintenance Pit Envelopes
N
Apr 01/15
FIGURE NLG/MLG Extension/Retraction Pit
N
Apr 01/15
FIGURE NLG/MLG Shock Absorber Removal Pit
N
Apr 01/15
FIGURE NLG/MLG Removal Pit
N
Apr 01/15
Subject 2-8-0
Subject 2-9-0
Subject 2-9-1
Subject 2-10-0
Exterior Lighting
Jun 01/13
L.E.C.
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
FIGURE Exterior Lighting
LAST REVISION
DATE
Jun 01/13
FIGURE Exterior Lighting
Jun 01/13
FIGURE Exterior Lighting
Jun 01/13
FIGURE Exterior Lighting
Jun 01/13
FIGURE Exterior Lighting
Jun 01/13
Subject 2-11-0
Antennas and Probes Location
Jun 01/13
FIGURE Antennas and Probes Location
Jun 01/13
Subject 2-12-0
Engine and Nacelle
Jun 01/13
FIGURE Engine and Nacelle
Jun 01/13
Subject 2-12-1
APU
Jun 01/13
FIGURE APU
Jun 01/13
Subject 2-13-0
Levelling, Symmetry and Alignement
Jun 01/13
FIGURE Location of Leveling Points
Jun 01/13
Subject 2-14-1
Jacking for Maintenance
R
Apr 01/15
FIGURE Jacking for Maintenance
R
Apr 01/15
Subject 2-14-2
Jacking for wheel change
Jun 01/13
FIGURE Nose Landing Gear Jacking Point Heights
Jun 01/13
FIGURE Main Landing Gear Jacking Point Heights
Jun 01/13
CHAPTER 3
Subject 3-1-0
General Information
N
Apr 01/15
N
Apr 01/15
Subject 3-3-0
Take-Off Weight Limitation
L.E.C.
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
N
LAST REVISION
DATE
Apr 01/15
N
Apr 01/15
Landing Field Length
N
Apr 01/15
FIGURE Landing Field Length
N
Apr 01/15
N
Apr 01/15
FIGURE ISA Conditions
FIGURE ISA + 15 ˚C (+59 ˚F) Conditions
Subject 3-4-0
Subject 3-5-0
Final Approach Speed
CHAPTER 4
Subject 4-2-0
Turning Radii
Jun 01/13
FIGURE Turning Radii
Jun 01/13
Subject 4-3-0
Minimum Turning Radii
Jun 01/13
FIGURE Minimum Turning Radii
Jun 01/13
Subject 4-4-0
Visibility from Cockpit in Static Position
Jun 01/13
FIGURE Visibility from Cockpit in Static Position
Jun 01/13
Subject 4-5-0
Introduction
Jun 01/13
Subject 4-5-1
90˚ Turn - Runway to Taxiway
Jun 01/13
FIGURE 90˚ Turn - Runway to Taxiway
Jun 01/13
Subject 4-5-2
135˚ Turn - Runway to Taxiway
Jun 01/13
FIGURE 135˚ Turn - Runway to Taxiway
Jun 01/13
Subject 4-5-3
180˚ Turn on a Runway
Jun 01/13
FIGURE 180˚ Turn on a Runway
Jun 01/13
Subject 4-5-4
L.E.C.
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
90˚ Turn - Taxiway to Taxiway
FIGURE 90˚ Turn - Taxiway to Taxiway
CHG
CODE
LAST REVISION
DATE
Jun 01/13
Jun 01/13
Subject 4-5-5
135˚ Turn - Taxiway to Taxiway
Jun 01/13
FIGURE 135˚ Turn - Taxiway to Taxiway
Jun 01/13
Subject 4-6-0
Runway Holding Bay (Apron)
Jun 01/13
FIGURE Runway Holding Bay (Apron)
Jun 01/13
Subject 4-7-0
Minimum Line-Up Distance Corrections
Sep 01/14
FIGURE 90˚ Turn on Runway Entry
Sep 01/14
FIGURE 180˚ Turn on Runway Turn Pad
Sep 01/14
FIGURE 180˚ Turn on Runway Width
Sep 01/14
Subject 4-8-0
Aircraft Mooring
Jun 01/13
FIGURE Aircraft Mooring
Sep 01/14
CHAPTER 5
Subject 5-1-0
Aircraft Servicing Arrangements
Jun 01/13
Subject 5-1-1
Typical Ramp Layout (Open Apron)
Sep 01/14
FIGURE Typical Ramp Layout (Open Apron)
Sep 01/14
Subject 5-1-2
Typical Ramp Layout (Gate)
Sep 01/14
FIGURE Typical Ramp Layout (Gate)
Sep 01/14
Subject 5-2-0
Terminal Operations - Full Servicing Turn Round Time
Sep 01/14
FIGURE Full Servicing Turn Round Time Chart
Sep 01/14
Subject 5-3-0
L.E.C.
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
Terminal Operations - Transit Turn Round Time
FIGURE Transit Turn Round Time Chart
LAST REVISION
DATE
Sep 01/14
Sep 01/14
Subject 5-4-0
Ground Service Connections Layout
Sep 01/14
FIGURE Ground Service Connections Layout
Sep 01/14
Subject 5-4-1
Grounding (Earthing) Points
R
Apr 01/15
FIGURE Grounding (Earthing) Point - NLG
Sep 01/14
FIGURE Grounding (Earthing) Point - MLG
Sep 01/14
Subject 5-4-2
Hydraulic System
R
Apr 01/15
FIGURE Green Ground Service Panel
Sep 01/14
FIGURE Yellow Ground Service Panel
Sep 01/14
Subject 5-4-3
Electrical System
R
Apr 01/15
FIGURE Electrical Service Panel
Jun 01/13
FIGURE RAT
Sep 01/14
Subject 5-4-4
Oxygen System
Sep 01/14
FIGURE Oxygen System
Jun 01/13
FIGURE Crew Oxygen Storage - Location
Sep 01/14
Subject 5-4-5
Fuel System
Sep 01/14
FIGURE Refuel/Defuel Control Panel
Sep 01/14
FIGURE Refuel/Defuel Couplings
Sep 01/14
FIGURE Overpressure Protectors and NACA Vent Intake
Sep 01/14
Subject 5-4-6
Pneumatic System
Sep 01/14
FIGURE Low Pressure Ground Connectors
Sep 01/14
L.E.C.
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
FIGURE High Pressure Ground Connectors
LAST REVISION
DATE
Sep 01/14
Subject 5-4-7
Engine Oil Servicing
Sep 01/14
FIGURE Engine Oil Servicing
Sep 01/14
VFG Oil Servicing
Sep 01/14
FIGURE VFG Oil Servicing
Sep 01/14
Starter Oil Servicing
Sep 01/14
FIGURE Starter Oil Servicing
Sep 01/14
APU Oil Servicing
Sep 01/14
FIGURE APU Oil Servicing
Sep 01/14
Subject 5-4-8
Potable Water System
Sep 01/14
FIGURE Potable-Water Ground Service Panel
Sep 01/14
FIGURE Forward Drain Port
Sep 01/14
FIGURE Potable-Water Tanks Location
Sep 01/14
Subject 5-4-9
Waste Water System
Sep 01/14
FIGURE Waste-Water Ground Service Panel
Sep 01/14
FIGURE Waste Tanks Location
Jun 01/13
Subject 5-4-10
Cargo Control Panels
N
Apr 01/15
FIGURE Forward Cargo Control Panels
N
Apr 01/15
FIGURE Aft Cargo Control Panels
N
Apr 01/15
Subject 5-5-0
Engine Starting Pneumatic Requirements
Sep 01/14
FIGURE Example for Use of the Charts
Sep 01/14
FIGURE Engine Starting Pneumatic Requirements
Sep 01/14
Subject 5-6-0
Ground Pneumatic Power Requirements
R
Apr 01/15
L.E.C.
Page 7
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
FIGURE Ground Pneumatic Power Requirements
LAST REVISION
DATE
Jun 01/13
Subject 5-7-0
Preconditioned Airflow Requirements
Jun 01/13
FIGURE Preconditioned Airflow Requirements
Jun 01/13
Subject 5-8-0
Ground Towing Requirements
R
Apr 01/15
FIGURE Ground Towing Requirements
R
Apr 01/15
Subject 5-9-0
De-icing and External cleaning
Jun 01/13
CHAPTER 6
Subject 6-1-0
Engine Exhaust Velocities and Temperatures
N
Apr 01/15
Engine Exhaust Velocities - Ground Idle Power
N
Apr 01/15
FIGURE Ground Idle Power - TRENT XWB Engine
N
Apr 01/15
Engine Exhaust Temperatures - Ground Idle Power
N
Apr 01/15
FIGURE Ground Idle Power - TRENT XWB-84 Engine
N
Apr 01/15
Engine Exhaust Velocities - Breakaway Power
N
Apr 01/15
FIGURE Breakaway Power (11% MTO Thrust) - TRENT XWB-84
Engine
N
Apr 01/15
FIGURE Breakaway Power (22% MTO Thrust) - TRENT XWB-84
Engine
N
Apr 01/15
Engine Exhaust Temperatures - Breakaway Power
N
Apr 01/15
FIGURE Breakaway Power (11% MTO Thrust) - TRENT XWB-84
Engine
N
Apr 01/15
FIGURE Breakaway Power (22% MTO Thrust) - TRENT XWB-84
Engine
N
Apr 01/15
Subject 6-1-1
Subject 6-1-2
Subject 6-1-3
Subject 6-1-4
L.E.C.
Page 8
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
LAST REVISION
DATE
Engine Exhaust Velocities - Max Take-Off Power
N
Apr 01/15
FIGURE Max Take-Off Power - TRENT XWB-84 Engine (Single)
N
Apr 01/15
FIGURE Max Take-Off Power - TRENT XWB-84 Engine (Twin)
N
Apr 01/15
Engine Exhaust Temperatures - Max Take-Off Power
N
Apr 01/15
FIGURE Max Take-Off Power - TRENT XWB-84 Engine
N
Apr 01/15
Danger Areas of the Engines - Ground Idle Power
N
Apr 01/15
FIGURE Ground Idle Power - TRENT XWB-84 Engine
N
Apr 01/15
Danger Areas of the Engines - Max Take-Off Power
N
Apr 01/15
FIGURE Max Take-Off Power - TRENT XWB-84 Engine
N
Apr 01/15
Subject 6-1-5
Subject 6-1-6
Subject 6-3-1
Subject 6-3-3
Subject 6-4-0
APU Exhaust Velocities and Temperatures
Jun 01/13
FIGURE APU Exhaust Velocities and Temperatures
Jun 01/13
CHAPTER 7
Subject 7-1-0
General Information
R
Apr 01/15
Landing Gear Footprint
R
Apr 01/15
FIGURE Landing Gear Footprint
R
Apr 01/15
Maximum Pavement Loads
R
Apr 01/15
FIGURE Maximum Pavement Loads
R
Apr 01/15
Landing Gear Loading on Pavement
R
Apr 01/15
FIGURE Landing Gear Loading on Pavement
R
Apr 01/15
FIGURE Landing Gear Loading on Pavement
N
Apr 01/15
Subject 7-2-0
Subject 7-3-0
Subject 7-4-0
L.E.C.
Page 9
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
LAST REVISION
DATE
Flexible Pavement Requirements - US Army Corps of Engineers
Design Method
R
Apr 01/15
FIGURE Flexible Pavement Requirements
R
Apr 01/15
FIGURE Flexible Pavement Requirements
N
Apr 01/15
R
Apr 01/15
Rigid Pavement Requirements - Portland Cement Association Design
Method
FIGURE Rigid Pavement Requirements
R
Apr 01/15
R
Apr 01/15
FIGURE Rigid Pavement Requirements
N
Apr 01/15
R
Apr 01/15
ACN/PCN Reporting System - Flexible and Rigid Pavements
R
Apr 01/15
FIGURE ACN/PCN Reporting System - WV000, MRW 268 900 kg,
CG 33%
FIGURE ACN/PCN Reporting System - WV001, MRW 275 900 kg,
CG 33.2%
FIGURE ACN Table
R
Apr 01/15
N
Apr 01/15
N
Apr 01/15
Subject 7-5-0
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion
Subject 7-7-0
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion
Subject 7-9-0
CHAPTER 8
Subject 8-0-0
Scaled Drawings
Jun 01/13
FIGURE Scaled Drawings
Jun 01/13
CHAPTER 10
Subject 10-0-0
Aircraft Rescue and Fire Fighting
R
Apr 01/15
FIGURE Front Page
R
Apr 01/15
FIGURE Highly Flammable and Hazardous Materials and Components
R
Apr 01/15
L.E.C.
Page 10
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
FIGURE Crew Rest Compartments Location
LAST REVISION
DATE
Jun 01/13
FIGURE Wheel/Brake Overheat
Jun 01/13
FIGURE Composite Materials Location
Jun 01/13
FIGURE Ground Lock Safety Devices
Jun 01/13
FIGURE Emergency Evacuation Devices
R
Apr 01/15
FIGURE Pax/Crew Doors and Emergency Exits
Jun 01/13
FIGURE Cockpit Emergency Exit
Jun 01/13
FIGURE FWD and AFT Lower Deck Cargo Doors
R
FIGURE Control Panels
FIGURE APU Compartment Access
Apr 01/15
Jun 01/13
R
Apr 01/15
FIGURE Aircraft Ground Clearances
Jun 01/13
FIGURE Structural Break-in Points
Jun 01/13
FIGURE Batteries Location and Access
R
Apr 01/15
L.E.C.
Page 11
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TABLE OF CONTENTS
1
1-1-0
1-2-0
SCOPE
INTRODUCTION
Glossary
2
AIRCRAFT DESCRIPTION
2-1-0
General Aircraft Characteristics Data
2-2-0
General Aircraft Dimensions
2-3-0
Ground Clearances
2-4-0
Interior Arrangements - Plan View
2-5-0
Interior Arrangements - Cross Section
2-6-0
Cargo Compartments
2-7-0
Door Clearances and Location
2-8-0
Escape Slides
2-9-0
Landing Gear
2-9-1
Landing Gear Maintenance Pits
2-10-0
Exterior Lighting
2-11-0
Antennas and Probes Location
2-12-0
Engine and Nacelle
2-12-1
APU
2-13-0
Levelling, Symmetry and Alignement
2-14-1
Jacking for Maintenance
2-14-2
Jacking of the Landing Gear
3
3-1-0
3-3-0
3-4-0
3-5-0
AIRCRAFT PERFORMANCE
General Information
Take-Off Weight Limitation
Landing Field Length
Final Approach Speed
4
4-2-0
4-3-0
4-4-0
4-5-0
4-5-1
GROUND MANEUVERING
Turning Radii
Minimum Turning Radii
Visibility from Cockpit in Static Position
Runway and Taxiway Turn Paths
90˚ Turn - Runway to Taxiway
T.O.C.
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2
4-5-3
4-5-4
4-5-5
4-6-0
4-7-0
4-8-0
135˚ Turn - Runway to Taxiway
180˚ Turn on a Runway
90˚ Turn - Taxiway to Taxiway
135˚ Turn - Taxiway to Taxiway
Runway Holding Bay (Apron)
Minimum Line-Up Distance Corrections
Aircraft Mooring
5
TERMINAL SERVICING
5-1-0
Aircraft Servicing Arrangements
5-1-1
Typical Ramp Layout (Open Apron)
5-1-2
Typical Ramp Layout (Gate)
5-2-0
Terminal Operations - Full Servicing Turn Round Time
5-3-0
Terminal Operations - Transit Turn Round Time
5-4-0
Ground Service Connections Layout
5-4-1
Grounding (Earthing) Points
5-4-2
Hydraulic System
5-4-3
Electrical System
5-4-4
Oxygen System
5-4-5
Fuel System
5-4-6
Pneumatic System
5-4-7
Oil System
5-4-8
Potable Water System
5-4-9
Waste Water System
5-4-10
Cargo Control Panels
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
6
6-1-0
6-1-1
6-1-2
6-1-3
6-1-4
6-1-5
OPERATING CONDITIONS
Engine Exhaust Velocities and Temperatures
Engine Exhaust Velocities - Ground Idle Power
Engine Exhaust Temperatures - Ground Idle Power
Engine Exhaust Velocities - Breakaway Power
Engine Exhaust Temperatures - Breakaway Power
Engine Exhaust Velocities - Max Take-Off Power
T.O.C.
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6
6-3-1
6-3-3
6-4-0
Engine Exhaust Temperatures - Max Take-Off Power
Danger Areas of the Engines - Ground Idle Power
Danger Areas of the Engines - Max Take-Off Power
APU Exhaust Velocities and Temperatures
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 - US 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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0
INTRODUCTION
**ON A/C A350-900
Introduction
1.
General
The A350 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (AC)
manual is issued for the A350-900 series aircraft to provide necessary data to airport operators and
airlines for airport facilities planning.
The data given in this issue of the A350 AIRCRAFT CHARACTERISTICS AIRPORT AND
MAINTENANCE PLANNING (AC) can be subject to change pending completion of the design and
flight test phase. It is given for guidance only and does not constitute a contractual commitment.
This document is not customized and must not be used for training purposes.
The A350 XWB is a new family of mid-size medium to long range new technology aircraft that will
deliver superior fuel efficiency, passenger comfort, environmental characteristics and economics, with
a global market coverage.
The aircraft is designed to offer multiple payload capabilities with a consistant range ability across
the family.
The A350 XWB is equipped with two Rolls-Royce Trent XWB engines.
This engine will incorporate the most advanced technologies to provide the best aircraft performance,
maintainability, lowest fuel consumption and environmental impact.
Reflecting market needs, the A350 XWB offers a high level of cargo hold capability and flexibility.
Two wide cargo doors and a Cargo Loading System (CLS) compatible with most lower deck cargo
containers and pallet standards, allowing interlining operations, ease the loading.
The A350 XWB provides easy and cost effective ground handling minimizing aircraft turn round time.
The innovative A350 XWB design increases planning flexibility to perform maintenance during the
aircraft scheduled downtime.
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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1-2-0
Glossary
**ON A/C A350-900
Glossary
1. List of Abbreviations
Aircraft
A/C
ACN
Aircraft Classification Number
APU
Auxiliary Power Unit
Business Class
B/C
California Bearing Ratio
CBR
CC
Cargo Compartment
CG
Center of Gravity
E
Young’s Modulus
ESWL
Equivalent Single Wheel Load
FAA
Federal Aviation Administration
FDL
Fuselage Datum Line
FR
Frame
FSTE
Full Size Trolley Equivalent
FWD
Forward
GPU
Ground Power Unit
Ground Support Equipment
GSE
ICAO
International Civil Aviation Organisation
International Standard Atmosphere
ISA
L
Radius of relative stiffness
LCN
Load Classification Number
LD
Load Device
LD
Lower Deck
LH
Left Hand
LP
Low Pressure
LPS
Last Pax Seating
MAC
Mean Aerodynamic Chord
MAX
Maximum
MIN
Minimum
MLG
Main Landing Gear
NLG
Nose Landing Gear
Outside Air Temperature
OAT
PAX
Passenger
PBB
Passenger Boarding Bridge
1-2-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PCA
PCN
PRM
RH
ULD
US
VFG
WV
Y/C
2.
Portland Cement Association
Pavement Classification Number
Passenger with Reduced Mobility
Right Hand
Unit Load Device
United States
Variable Frequency Generator
Weight Variant
Economic 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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-0
General Aircraft Characteristics Data
**ON A/C A350-900
General Aircraft Characteristics Data
1.
The following table provides characteristics of A350--900 Models, these data are specific to each
Weight Variant:
Aircraft Characteristics
WV000
WV001
Maximum Taxi Weight
(MTW)
Maximum Ramp Weight
(MRW)
Maximum Take-Off
Weight (MTOW)
Maximum Landing
Weight (MLW)
Maximum Zero Fuel
Weight (MZFW)
2.
WV002
268900 kg
(592824 lb)
275900 kg
(608256 lb)
272900 kg
(601642 lb)
268000 kg
(590839 lb)
205000 kg
(451948 lb)
192000 kg
(423288 lb)
275000 kg
(606272 lb)
207000 kg
(456357 lb)
195700 kg
(431445 lb)
272000 kg
(599658 lb)
207000 kg
(456357 lb)
194000 kg
(427697 lb)
The following table provides characteristics of A350--900 Models, these data are common to each
Weight Variant:
Standard Seating Capacity
Usable Fuel Capacity
(density = 0.785 kg/l)
Pressurized Fuselage Volume
Cockpit Volume
Passenger Compartment Volume
Usable Volume, FWD CC
(Based on LD3)
Usable Volume, AFT CC
(Based on LD3)
Aircraft Characteristics
315 (2 class)
138000 l
(36456.4 USgal)
108330 kg
(238827.0 lb)
971 m3
(34291.0 ft.3)
8.23 m3
(291.0 ft.3)
473.7 m3
(16729.0 ft.3)
89.4 m3
(3157.0 ft.3)
71.5 m3
(2525.0 ft.3)
2-1-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Usable Volume, Bulk CC
Water Volume, FWD CC
Water Volume, AFT CC
Water Volume, Bulk CC
Aircraft Characteristics
9.12 m3
(322.07 ft.3)
113.4 m3
(4004.7 ft.3)
95.8 m3
(3383.16 ft.3)
11.4 m3
(402.59 ft.3)
2-1-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0
General Aircraft Dimensions
**ON A/C A350-900
General Aircraft Dimensions
1.
This section provides general aircraft dimensions.
2-2-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
66.61 m
(218.54 ft)
9.09 m
(29.82 ft)
6.09 m
(19.98 ft)
3.04 m
(9.97 ft)
9.42 m
(30.91 ft)
4.63 m
(15.19 ft)
7.79 m
(25.56 ft)
28.66 m
(94.03 ft)
65.26 m
(214.11 ft)
64.75 m
(212.43 ft)
18.79 m
(61.65 ft)
1.74 m
(5.71 ft)
0.75 m
(2.46 ft)
10.60 m
(34.78 ft)
12.87 m
(42.22 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
P_AC_020200_1_0010001_01_02
General Aircraft Dimensions
(Sheet 1 of 2)
FIGURE-2-2-0-991-001-A01
2-2-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
66.80 m
(219.16 ft)
2.46 m
(8.07 ft)
6.21 m
(20.37 ft)
13.47 m
(44.19 ft)
7.86 m 10.50 m
(25.79 ft) (34.45 ft)
12.75 m
(41.83 ft)
5.96 m
(19.55 ft)
17.02 m
(55.84 ft)
9.62 m
(31.56 ft)
21.97 m
(72.08 ft)
5.18 m
(16.99 ft)
2.88 m
(9.45 ft)
46.68 m
(153.15 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
P_AC_020200_1_0010001_02_02
General Aircraft Dimensions
(Sheet 2 of 2)
FIGURE-2-2-0-991-001-A01
2-2-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0
Ground Clearances
**ON A/C A350-900
Ground Clearances
1.
This section provides the heights 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 FWD CG and a AFT CG,
- An aircraft at MRW with a FWD CG and a AFT CG,
- Aircraft on jacks, FDL at 6.50 m (21.33 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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
CP1 RD1
D1
D2
D3
W2 W1 C3 D4
AP
N1
VT HT
C2 F2 BF3
F4
BF1
MRW
A/C CONFIGURATION
C1 F1
F3
140 000 kg (308 647 lb)
BF2
FWD CG (26%) AFT CG (33.2%)
D5
A/C JACKED
FDL = 6.5 m
FWD CG (20%) AFT CG (40%)
(21.33 ft)
m
m
m
ft
ft
ft
5.16 16.93 5.38 17.65 6.37 20.91
5.22 17.14 5.34 17.51 6.37 20.91
5.33 17.47 5.27 17.28 6.37 20.91
5.40 17.73 5.21 17.10 6.37 20.90
7.33 24.05 7.61 24.97 8.59 28.18
3.20 10.50 3.38 11.08 4.39 14.40
3.43 11.25 3.29 10.78 4.43 14.52
3.43 11.25 3.26 10.70 4.41 14.47
3.71 12.18
2.52
8.27
8.88
2.71
3.71 12.18
2.70
8.85
2.59
8.48
8.61 28.26 8.78 28.82 9.80 32.14
8.59 28.17 8.45 27.71 9.58 31.45
2.57
8.44
2.67
8.75
3.71 12.17
3.16 10.37
2.08
6.81
2.08
6.82
8.80
2.59
8.51
2.68
3.71 12.18
5.94 19.49 6.21 20.36 7.18 23.55
4.07 13.35 4.35 14.27 5.32 17.45
9.57 31.41 9.44 30.96 10.57 34.69
7.14 23.44 7.05 23.12 8.17 26.80
7.88 25.84 7.56 24.80 8.77 28.77
6.82 22.38 6.52 21.38 7.72 25.34
17.38 57.03 17.06 55.99 18.27 59.96
0.87
0.94
3.08
6.54
2.87
1.99
m
m
ft
ft
5.11
16.76
5.06 16.60
D1
5.13
16.82
5.10 16.74
D2
5.17 16.96
5.16
16.91
D3
5.22 17.13
5.18
16.98
D4
DOORS
7.25 23.79
7.31
23.98
D5
3.09 10.15
3.13
10.27
C1
10.58
3.26 10.68
3.22
C2
3.21
10.54
3.25 10.67
C3
2.45
7.92
8.05
2.41
F1
2.53
2.50
8.30
8.22
F2
28.02
8.50 27.90
8.54
F3
8.38
27.50
8.41 27.60
F4
8.03
8.09
2.45
2.47
FUSELAGE
BF1
6.34
1.93
6.34
1.93
BF2
2.52
2.50
8.20
8.27
BF3
19.38
5.85 19.19
5.91
CP1
13.26
3.98 13.06
4.04
RD1
30.74
9.40 30.85
9.37
W1
WINGS
6.96
6.98 22.90
22.83
W2
7.60
7.67 25.16
24.92
HT
6.62 21.71 6.55
21.48
TAILPLANE
AP
56.11
17.17 56.34 17.10
VT
0.74
0.76
2.43
2.48
N1
ENGINE/
N1 WITH
NACELLE
0.59
1.93
0.60
1.97
0.72
2.36
0.78
2.55
1.84
6.02
DRAIN MAST
NOTE:
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER
OF THE DOOR SILL AND FROM FLOOR LEVEL.
P_AC_020300_1_0010001_01_03
Ground Clearances
FIGURE-2-3-0-991-001-A01
2-3-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
B
C
D
E
F
G
H
J
LEADING EDGE SLATS EXTENDED
140 000 kg (308 647 lb)
MRW
DESCRIPTION
DN* INBD
DN* OUTBD
SLAT 1 INBD
SLAT 1/2
SLAT 2/3
SLAT 3/4
SLAT 4/5
SLAT 5/6
SLAT 6 OUTBD
FWD CG (26%) AFT CG (33.2%) FWD CG (20%) AFT CG (40%)
A
B
C
D
E
F
G
H
J
m
3.41
4.58
4.60
4.98
5.33
5.67
5.98
6.28
6.62
ft
11.20
15.01
15.10
16.33
17.48
18.59
19.63
20.61
21.71
m
3.43
4.58
4.61
4.98
5.33
5.66
5.97
6.27
6.60
ft
11.25
15.03
15.12
16.33
17.47
18.57
19.59
20.56
21.64
m
3.55
4.71
4.74
5.12
5.48
5.82
6.14
6.44
6.78
NOTE:
* DN − DROOP NOSE
ft
11.63
15.47
15.56
16.80
17.97
19.09
20.13
21.13
22.24
m
3.61
4.74
4.77
5.13
5.46
5.79
6.09
6.37
6.69
ft
11.85
15.56
15.64
16.82
17.93
18.99
19.97
20.91
21.95
P_AC_020300_1_0020001_01_00
Ground Clearances
Leading Edge Slats - Extended
FIGURE-2-3-0-991-002-A01
2-3-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
G
F
E
D
C
B
A
FLAPS EXTENDED
140 000 kg (308 647 lb)
MRW
DESCRIPTION
FLAP 1 INBD
FLAP 1/2
FLAP 2 OUTBD
FLAP 3 INBD
FLAP 3/4
FLAP 4/5
FLAP 5 OUTBD
FWD CG (26%) AFT CG (33.2%) FWD CG (20%) AFT CG (40%)
A
B
C
D
E
F
G
m
2.54
3.26
4.06
4.12
4.86
5.40
5.65
ft
8.32
10.71
13.34
13.51
15.96
17.72
18.52
m
2.53
3.25
4.05
4.11
4.85
5.38
5.63
ft
8.29
10.67
13.30
13.47
15.91
17.67
18.46
m
2.69
3.42
4.22
4.27
5.02
5.56
5.81
ft
8.82
11.21
13.84
14.01
16.47
18.24
19.05
m
2.65
3.37
4.17
4.23
4.96
5.49
5.73
ft
8.69
11.07
13.69
13.86
16.28
18.01
18.79
P_AC_020300_1_0030001_01_00
Ground Clearances
Trailing Edge Flaps - Extended
FIGURE-2-3-0-991-003-A01
2-3-0
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
J
H
G
F
E D
C
B
A
SPOILERS EXTENDED
140 000 kg (308 647 lb)
MRW
DESCRIPTION
SPOILER 1 INBD
SPOILER 1/2
SPOILER 2 OUTBD
SPOILER 3 INBD
SPOILER 3/4
SPOILER 4/5
SPOILER 5/6
SPOILER 6/7
SPOILER 7 OUTBD
FWD CG (26%) AFT CG (33.2%) FWD CG (20%) AFT CG (40%)
A
B
C
D
E
F
G
H
J
m
5.00
5.46
5.91
6.06
6.30
6.51
6.69
6.87
7.04
ft
16.39
17.91
19.40
19.87
20.66
21.34
21.96
22.54
23.11
m
4.99
5.45
5.91
6.05
6.29
6.49
6.68
6.86
7.03
ft
16.37
17.89
19.38
19.84
20.63
21.31
21.92
22.49
23.06
m
5.15
5.61
6.07
6.21
6.45
6.66
6.85
7.03
7.20
ft
16.89
18.41
19.90
20.36
21.16
21.85
22.47
23.05
23.63
m
5.12
5.58
6.03
6.17
6.41
6.61
6.80
6.97
7.13
ft
16.78
18.30
19.79
20.26
21.03
21.70
22.30
22.86
23.40
P_AC_020300_1_0040001_01_00
Ground Clearances
Spoilers - Extended
FIGURE-2-3-0-991-004-A01
2-3-0
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
D
C
B
A
AILERONS DOWN
140 000 kg (308 647 lb)
MRW
DESCRIPTION
AILERON 1 INBD
AILERON 1 OUTBD
AILERON 2 INBD
AILERON 2 OUTBD
FWD CG (26%) AFT CG (33.2%) FWD CG (20%) AFT CG (40%)
A
B
C
D
m
5.91
6.32
6.31
6.80
ft
19.38
20.73
20.69
22.30
m
5.89
6.30
6.29
6.77
ft
19.32
20.66
20.62
22.22
m
6.07
6.48
6.47
6.96
ft
19.91
21.27
21.23
22.84
m
5.99
6.39
6.38
6.85
ft
19.65
20.97
20.93
22.49
P_AC_020300_1_0050001_01_00
Ground Clearances
Ailerons - Down
FIGURE-2-3-0-991-005-A01
2-3-0
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
D
C B
A
AILERONS UP
140 000 kg (308 647 lb)
MRW
DESCRIPTION
AILERON 1 INBD
AILERON 1 OUTBD
AILERON 2 INBD
AILERON 2 OUTBD
FWD CG (26%) AFT CG (33.2%) FWD CG (20%) AFT CG (40%)
A
B
C
D
m
6.92
7.16
7.17
7.45
ft
22.72
23.50
23.54
24.43
m
6.91
7.14
7.15
7.42
ft
22.66
23.43
23.47
24.35
m
7.08
7.33
7.34
7.61
ft
23.24
24.04
24.07
24.98
m
7.01
7.23
7.24
7.50
ft
22.99
23.74
23.77
24.62
P_AC_020300_1_0060001_01_00
Ground Clearances
Ailerons - Up
FIGURE-2-3-0-991-006-A01
2-3-0
Page 7
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
C
B
A
FLAP TRACKS RETRACTED
140 000 kg (308 647 lb)
MRW
DESCRIPTION
FLAP TRACK 1
FLAP TRACK 2
FLAP TRACK 3
FWD CG (26%) AFT CG (33.2%) FWD CG (20%) AFT CG (40%)
A
B
C
m
3.72
4.53
5.17
ft
12.22
14.87
16.96
m
3.72
4.52
5.16
ft
12.19
14.84
16.92
m
3.87
4.68
5.33
ft
12.71
15.37
17.47
m
3.84
4.64
5.27
ft
12.61
15.24
17.30
P_AC_020300_1_0070001_01_00
Flap Tracks - Retracted
FIGURE-2-3-0-991-007-A01
2-3-0
Page 8
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
C
B
A
FLAP TRACKS EXTENDED
140 000 kg (308 647 lb)
MRW
DESCRIPTION
FLAP TRACK 1
FLAP TRACK 2
FLAP TRACK 3
FWD CG (26%) AFT CG (33.2%) FWD CG (20%) AFT CG (40%)
A
B
C
m
2.82
3.34
4.00
ft
9.26
10.95
13.11
m
2.81
3.32
3.98
ft
9.23
10.90
13.06
m
2.98
3.49
4.16
ft
9.77
11.46
13.63
m
2.93
3.43
4.08
ft
9.62
11.27
13.40
P_AC_020300_1_0080001_01_00
Ground Clearances
Flap Tracks - Extended
FIGURE-2-3-0-991-008-A01
2-3-0
Page 9
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-0
Interior Arrangements - Plan View
**ON A/C A350-900
Interior Arrangements - Plan View
1.
This section gives the standard configuration.
2-4-0
Page 1
Apr 01/15
A
G
L
S
A L
PASSENGER
DOOR 1 LH
L
G
PASSENGER
DOOR 1 RH
ITEM
G
L
A
S
G
DESIGNATION
(12)
GALLEY
(9)
LAVATORY
ATTENDANT SEAT (8)
(1)
STOWAGE
PASSENGER
DOOR 2 LH
A
A
PASSENGER
DOOR 2 RH
2-4-0
SEAT PITCHES: ECONOMY 32 in.
BUSINESS 60 in.
G
A
A
G G
G G
G
G
PASSENGER
DOOR 4 LH
L
L
PASSENGER
DOOR 4 RH
48 BUSINESS CLASS (6−ABREAST)
267 ECONOMY CLASS (9−ABREAST)
PASSENGER SEATS (315 TOTAL)
PASSENGER
DOOR 3 LH
L A
L
L
L A
PASSENGER
DOOR 3 RH
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_020400_1_0010001_01_01
Standard Configuration
FIGURE-2-4-0-991-001-A01
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0
Interior Arrangements - Cross Section
**ON A/C A350-900
Interior Arrangements - Cross Section
1.
This section gives the typical configuration.
2-5-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
BUSINESS CLASS / FIRST CLASS 6 ABREAST
1.50 m
(59 in)
0.55 m
(21.5 in)
0.18 m
(7 in)
0.57 m
(22.5 in)
0.09 m
(3.5 in)
BASELINE ECONOMY CLASS 9 ABREAST
1.53 m
(60.11 in)
0.04 m
(1.5 in)
0.46 m
(18 in)
0.46 m
(18.1in)
NOTE:
AISLE WIDTH MAY VARY DEPENDING ON ACTUAL CABIN
CONFIGURATION SELECTED BY CUSTOMER
P_AC_020500_1_0010001_01_01
Typical Configuration
FIGURE-2-5-0-991-001-A01
2-5-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-0
Cargo Compartments
**ON A/C A350-900
Cargo Compartments
1.
This section gives cargo compartments :
- Locations and dimensions,
- Loading combinations.
2-6-0
Page 1
Apr 01/15
2.90 m
(114.55 in)
FR19
16.221 m
(638.62 in)
LOWER DECK
FORWARD CARGO
COMPARTMENT
FR44
2-6-0
13.578 m
(535.57 in)
2.85 m
(112.34 in)
LOWER DECK
AFT CARGO
COMPARTMENT
FR61
FR85
0.95 m
(37.4 in)
1.91 m
(75.20 in)
LOWER DECK
BULK CARGO
COMPARTMENT
FR82
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_020600_1_0020001_01_00
Cargo Compartments
Locations and Dimensions (Sheet 1 of 2)
FIGURE-2-6-0-991-002-A01
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
STANDARD: 20 LD3 CONTAINERS
STANDARD: 6 PALLETS 88 in / 96 in X 125 in
STANDARD: 16 LD3 CONTAINERS
STANDARD: 5 PALLETS 88 in / 96 in X 125 in
**ON A/C A350-900
P_AC_020600_1_0020001_02_00
Cargo Compartments
Loading Combinations (Sheet 2 of 2)
FIGURE-2-6-0-991-002-A01
2-6-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0
Door Clearances and Location
**ON A/C A350-900
Door Clearances and Location
1.
This section provides door clearances and location.
2-7-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
DOOR
1L
DOOR
3L
DOOR
2L
DOOR
4L
BULK CARGO DOOR
DOOR
4R
DOOR
1R
DOOR
3R
DOOR
2R
AFT CARGO DOOR
COCKPIT ESCAPE
HATCH
FWD CARGO DOOR
P_AC_020700_1_0010001_01_02
Door Identification and Location
(Sheet 1 of 2)
FIGURE-2-7-0-991-001-A01
2-7-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
52.55 m
(172.41 ft)
37.93 m
(124.44 ft)
18.86 m
(61.88 ft)
6.82 m
(22.38 ft)
49.99 m
(164.01 ft)
4.12 m
(13.52 ft)
11.68 m
(38.32 ft)
47.30 m
(155.18 ft)
P_AC_020700_1_0010001_02_02
Door Identification and Location
(Sheet 2 of 2)
FIGURE-2-7-0-991-001-A01
2-7-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
PASSENGER/CREW DOOR
1LH, 1RH
0.73 m
(2.40 ft)
0.86 m
(2.82 ft)
2.46 m
(8.07 ft)
FWD
1.26 m
(4.13 ft)
2.16 m
(7.09 ft)
0.06 m
(0.20 ft)
SEE CHAPTER
2−3
FWD
P_AC_020700_1_0020003_01_01
Forward Passenger/Crew Doors
(Sheet 1 of 2)
FIGURE-2-7-0-991-002-C01
2-7-0
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
PASSENGER/CREW DOOR
2LH, 2RH
0.84 m
(2.76 ft)
0.69 m
(2.26 ft)
2.47 m
(8.10 ft)
FWD
2.16 m
(7.09 ft)
1.26 m
(4.13 ft)
0.06 m
(0.20 ft)
SEE CHAPTER
2−3
FWD
P_AC_020700_1_0020003_02_01
Forward Passenger/Crew Doors
(Sheet 2 of 2)
FIGURE-2-7-0-991-002-C01
2-7-0
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
PASSENGER/CREW DOOR
3LH, 3RH
0.84 m
(2.76 ft)
2.47 m
(8.10 ft)
0.69 m
(2.26 ft)
FWD
2.11 m
(6.92 ft)
1.26 m
(4.13 ft)
0.06 m
(0.20 ft)
SEE CHAPTER
2−3
FWD
P_AC_020700_1_0030001_01_01
Aft Passenger/Crew Doors
(Sheet 1 of 2)
FIGURE-2-7-0-991-003-A01
2-7-0
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
PASSENGER/CREW DOOR
4LH, 4RH
0.87 m
(2.85 ft)
0.74 m
(2.43 ft)
FWD
2.39 m
(7.84 ft)
1.26 m
(4.13 ft)
FWD
0.06 m
(0.20 ft)
2.16 m
(7.09 ft)
SEE CHAPTER
2−3
P_AC_020700_1_0030001_02_01
Aft Passenger/Crew Doors
(Sheet 2 of 2)
FIGURE-2-7-0-991-003-A01
2-7-0
Page 7
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
2.91 m
(9.55 ft)
FWD
A
2.55 m
(8.37 ft)
1.76 m
(5.77 ft)
0.27 m
(0.89 ft)
SEE CHAPTER 2−3
2.40 m
(7.87 ft)
0.74 m
(2.43 ft)
A A
P_AC_020700_1_0040001_01_00
Forward Cargo Compartment Door
FIGURE-2-7-0-991-004-A01
2-7-0
Page 8
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
FWD
2.85 m
(9.35 ft)
A
2.53 m
(8.30 ft)
2.40 m
(7.87 ft)
1.75 m
(5.74 ft)
0.27 m
(0.89 ft)
SEE CHAPTER 2−3
0.75 m
(2.46 ft)
A A
P_AC_020700_1_0050001_01_00
Aft Cargo Compartment Door
FIGURE-2-7-0-991-005-A01
2-7-0
Page 9
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
0.95 m
(3.12 ft)
FWD
1.76 m
(5.77 ft)
A
0.76 m
(2.49 ft)
SEE CHAPTER 2−3
A A
P_AC_020700_1_0060001_01_00
Bulk Cargo Compartment Door
FIGURE-2-7-0-991-006-A01
2-7-0
Page 10
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
B
1.06 m
(3.48 ft)
61.8°
R 0.78 m
(2.56 ft)
R 1.06 m
(3.48 ft)
0.77 m
(2.53 ft)
2.93 m
(9.61 ft)
2.00 m
(6.56 ft)
A
P_AC_020700_1_0070001_01_01
Nose Landing Gear Doors
Forward Nose Landing Gear Doors (Sheet 1 of 2)
FIGURE-2-7-0-991-007-A01
2-7-0
Page 11
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
0.76 m
(2.49 ft)
69.8°
R 0.71 m
(2.33 ft)
R 0.72 m
(2.36 ft)
0.59 m
(1.94 ft)
2.15 m
(7.05 ft)
2.03 m
(6.66 ft)
B
P_AC_020700_1_0070001_02_01
Nose Landing Gear Doors
Aft Nose Landing Gear Doors (Sheet 2 of 2)
FIGURE-2-7-0-991-007-A01
2-7-0
Page 12
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
2.75 m
(9.02 ft)
1.63 m
(5.35 ft)
81.3°
R 2.43 m
(7.97 ft)
0.13 m 0.19 m
(0.43 ft) (0.62 ft)
A
P_AC_020700_1_0080001_01_01
Main Landing Gear Doors
FIGURE-2-7-0-991-008-A01
2-7-0
Page 13
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0
Escape Slides
**ON A/C A350-900
Escape Slides
1.
General
This section provides location of escape facilities and related clearances.
2.
Location
Escape facilities are provided at the following locations:
- One cockpit escape rope is kept in a dedicated stowage compartment adjacent to the escape
hatch,
- One slide-raft at each passenger/crew door (total eight).
2-8-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
CABIN DUAL−LANE
SLIDE/RAFT
CABIN DUAL−LANE
SLIDE/RAFT
CABIN DUAL−LANE
SLIDE/RAFT
COCKPIT
ESCAPE ROPE
CABIN SINGLE−LANE
SLIDE/RAFT
NOTE:
RH SHOWN, LH SYMMETRICAL
P_AC_020800_1_0020001_01_00
Escape Slides
(Sheet 1 of 2)
FIGURE-2-8-0-991-002-A01
2-8-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOTE:
RH SHOWN, LH SYMMETRICAL
GRID EQUALS 1 m (3.28 ft) IN REALITY
0
3
6
9
12
15
18
21
24
27
30
33
EMERGENCY DESCENT THROUGH THE
ESCAPE HATCH WITH THE ESCAPE ROPE
**ON A/C A350-900
P_AC_020800_1_0020001_02_00
Escape Slides
(Sheet 2 of 2)
FIGURE-2-8-0-991-002-A01
2-8-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0
Landing Gear
**ON A/C A350-900
Landing Gear
1.
MLG System Description
The two MLGs are mounted in the LH and RH wing just outboard of the wing root within the
trailing edge.
The MLGs retract sideways into bays in the fuselage. Each MLG has a four wheel twin-tandem bogie.
Each MLG has one related main door operated by a single door actuator.
Each MLG has a gear uplock and a door uplock.
The MLG has a double side stay arrangement to improve load distribution on the composite wing.
Each side stay has a separate lock stay assembly to provide a positive means to lock the landing gear
in the extended position for landing and ground manoeuvres.
Each MLG leg contains a single-stage oleo shock strut consisting of a sliding piston and a main fitting
that is supported by the two folding side stays and pivots on the top of the main fitting for
extension/retraction.
In flight, the MLGs are retracted and locked up.
The MLG doors are closed and locked to enclose the MLG bay in flight and on the ground, only
opening when the landing gear is extending or retracting.
Hydraulic power for the MLG extension/retraction comes from the Green Hydraulic System.
2.
NLG System Description
The NLG is located in the forward lower fuselage on the aircraft centerline below the cockpit.
It is forward retracting and consists of a twin wheel axle mounted on a main fitting that incorporates
a single-stage oleo shock strut supported by a forward drag stay.
The NLG main fitting accommodates the steering assembly for the NWS system.
In flight, the NLG is retracted and locked up while the four sideways opening NLG Doors are closed
and locked to enclose the NLG bay.
The two forward doors are each operated by two independent door actuators.
When retracted, the NLG is held by an uplock and the two main NLG doors are held by a single door
uplock assembly, containing an uplock hook for each door.
The hydraulically powered Forward NLG Doors are also closed after the NLG is extended.
The aft doors are mechanically driven and remain open when the NLG is extended.
Hydraulic power for the NLG extension/retraction comes from the Yellow hydraulic system.
3.
Landing Gear Extension and Retraction System
The Landing Gear Extension and Retraction System is made up of three sub-systems:
- Normal extension and retraction system, for normal extension and retraction
- Alternate extension system, for extension in flight if the normal system is unavailable
- Ground door opening system, to allow on-ground access to the landing gear bays for maintenance
purposes.
2-9-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FIXED FAIRING
DOOR
HINGE DOOR
C
B
A
D
FREE−FALL
RAMP
HINGE
ACTUATOR
MAIN DOOR
HINGE
A
LH SHOWN
RH SYMMETRICAL
F
MECHANICAL
LINKAGE
FREE−FALL
RAMP
UP−LOCK
FITTING
FREE−FALL
ROD
B
C
P_AC_020900_1_0010001_01_01
Main Landing Gear
Doors Overview (Sheet 1 of 3)
FIGURE-2-9-0-991-001-A01
2-9-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FORWARD LOCK
STAY ACTUATOR
RETRACTION
ACTUATOR
FORWARD
LOCK STAY
G
MAIN FITTING
FORWARD
SIDE STAY
SLIDING
PISTON
E
FORWARD
DOWNLOCK
SPRINGS
BOGIE
AFT LOCK
STAY ACTUATOR
AFT
LOCK STAY
G
BOGIE PITCH
TRIMMER
ACTUATOR
D
AFT DOWNLOCK
SPRINGS
AFT SIDE STAY
UPPER
TORQUE LINK
LOWER
TORQUE LINK
E
P_AC_020900_1_0010001_02_01
Main Landing Gear
Overview (Sheet 2 of 3)
FIGURE-2-9-0-991-001-A01
2-9-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
SAFETY
PIN
SAFETY
COLLAR
WARNING
FLAG
LOCK STAY
SAFETY
PIN
F
SAFETY
PIN
WARNING
FLAG
G
01
TYPICAL
NOTE:
01 FORWARD LOCK STAY SHOWN, AFT SIMILAR
P_AC_020900_1_0010001_03_01
Main Landing Gear
Safety Devices (Sheet 3 of 3)
FIGURE-2-9-0-991-001-A01
2-9-0
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
FORWARD
DOOR
B
ACTUATOR
C
E
AFT DOOR
HINGE
A
HINGE
PROTECTIVE
PLATE
DOOR STOP
INTER
DOOR STOP
ROD FITTING
B
RH SHOWN
LH SYMMETRICAL
P_AC_020900_1_0020001_01_01
Nose Landing Gear
Doors Overview (Sheet 1 of 4)
FIGURE-2-9-0-991-002-A01
2-9-0
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RETRACTION ACTUATOR
F
LOCK STAY ACTUATOR
UPPER DRAG
STAY
FORWARD/ AFT
LOCK STAYS
LOWER DRAG
STAY
MAIN FITTING
DOWNLOCK
SPRINGS
D
G
STEERING
ASSEMBLY
TOWING
FITTING
C
UPPER
TORQUE LINK
SLIDING
PISTON
LOWER
TORQUE LINK
D
P_AC_020900_1_0020001_02_01
Nose Landing Gear
Overview (Sheet 2 of 4)
FIGURE-2-9-0-991-002-A01
2-9-0
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
SAFETY
COLLAR
WARNING
FLAG
SAFETY
PIN
E
SAFETY PIN
LOCK STAY
WARNING FLAG
F
P_AC_020900_1_0020001_03_01
Nose Landing Gear
Safety Devices (Sheet 3 of 4)
FIGURE-2-9-0-991-002-A01
2-9-0
Page 7
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
H
J
2GN
1GN
G
WARNING
FLAG
H
FWD
J
FWD
P_AC_020900_1_0020001_04_01
Nose Landing Gear
Service Panels (Sheet 4 of 4)
FIGURE-2-9-0-991-002-A01
2-9-0
Page 8
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-1
Landing Gear Maintenance Pits
**ON A/C A350-900
Landing Gear Maintenance Pits
1.
General
The minimum maintenance pit envelopes for landing gear shock absorber maintenance are shown in
Figures FIGURE 2-9-1-991-001-A, FIGURE 2-9-1-991-002-A, FIGURE 2-9-1-991-003-A and FIGURE
2-9-1-991-004-A.
The landing gears are shown with simplified gear structure.
The three envelopes show the minimum dimensions for these maintenance operations:
- Extension and retraction
- Gear removal
- Piston removal.
Pit envelopes shown represent minimum sizing required to accommodate landing gear tires and
removal tooling. Dimensions for the below cases are to be added in the shown envelopes:
- Clearance allowances for working area
- Operator access
- Functional clearances
- Tooling
- Civil engineering considerations.
The maintenance pits are symmetrical about the aircraft centerline and all dimensions shown are
minimum dimensions with zero clearances.
The dimensions for the pits have been determined as follows:
- The aircraft starting condition is with weight on wheels supported by jacks over the pits.
- The pit depths are then based on the shock absorbers lowering to the fully extended position plus
allowances for tooling.
- The length and width of the pits allow the gear to rotate after the weight is taken off the landing
gear
- The landing gear tires are in the maximum grown condition
- The MLG wheels, brakes and bogie beams are removed before the piston is removed
- The NLG wheels are removed before the piston is removed
- Both the MLG and the NLG pistons are removed vertically.
The pit depth for the MLG piston removal is based on the removal pallet support leg being installed
at its maximum length (upper pin hole position).
The landing gear piston trolley for MLG and NLG may be positioned FWD or AFT of the landing
gears depending on the chosen removal orientation (rotation FWD or AFT).
Dimensions for elevators and associated mechanisms must be added to those in Figures FIGURE
2-9-1-991-001-A, FIGURE 2-9-1-991-002-A, FIGURE 2-9-1-991-003-A and FIGURE 2-9-1-991-004-A.
2-9-1
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
A.
Elevators
These can be either mechanical or hydraulic. They are used to:
- Permit easy movement of persons and equipment around the landing gears
- Lift and remove landing gear assemblies out of the pits.
B.
Jacking
The aircraft must be in position over the pits to put the gear on the elevators. The jack must be
installed and engaged with all the jacking points, AC 2-14-1 for aircraft maintenance jacking.
When lowering the elevators, the aircraft weight will be transferred from the wheels to the jacks.
The landing gears must not be in contact with the elevators during retraction/extension tests.
The aircraft must not bend when it is jacked and when its weight is off the wheels.
When tripod support jacks are used, the tripod-base circle radius must be limited because the
locations required for positioning the columns are close to the sides of the pits.
2-9-1
Page 2
Apr 01/15
2-9-1
1.73 m
(5.68 ft)
3.14 m
(10.30 ft)
1.63 m
(5.35 ft)
0.91 m
(2.99 ft)
NLG REMOVAL PIT OUTLINE
2.26 m
(7.42 ft)
FWD
3.85 m
(12.63 ft)
3.41 m
(11.19 ft)
2.57 m
(8.43 ft)
WING
2.30 m
(7.55 ft) JACKING
POINT
MLG REMOVAL PIT OUTLINE
MLG SHOCK ABSORBER
REMOVAL PIT
MLG EXTENSION/RETRACTION
PIT OUTLINE
4.16 m
(13.65 ft)
WING JACKING POINT
AIRCRAFT CENTER LINE
NLG EXTENSION/RETRACTION
PIT OUTLINE
NLG SHOCK ABSORBER
REMOVAL PIT OUTLINE
NOTE:
ENVELOPES SHOWN WITH ZERO CLEARANCE TO OUTSIDE EDGE OF TIRES.
FWD
JACKING
1.14 m POINT
(3.74 ft)
0.38 m
(1.25 ft)
10.11 m
(33.17 ft)
1.52 m
(4.99 ft)
1.16 m
(3.81 ft)
A/C DATUM X = 0
38.56 m
(126.51 ft)
2.05 m
(6.73 ft)
8.71 m
(28.58 ft)
2.22 m
(7.28 ft)
3.50 m
(11.48 ft)
1.84 m
(6.04 ft)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_020901_1_0010001_01_00
Maintenance Pit Envelopes
FIGURE-2-9-1-991-001-A01
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
0.38° REF
AIRCRAFT JACKED AT 20% MAC
FUSELAGE DATUM LINE
FWD
NLG FULLY EXTENDED
NLG WEIGHT ON WHEELS
0.44 m
(1.44 ft)
NLG TIRES RETRACTION
SWEEP
GROUND PLANE
0.11° REF
AIRCRAFT JACKED AT 41% MAC
NLG EXTENSION/RETRACTION
PIT
2.25 m
(7.38 ft)
FUSELAGE DATUM LINE
MLG TIRES
RETRACTION SWEEPS
FWD
MLG FULLY EXTENDED
MLG WEIGHT ON WHEELS
0.90 m
(2.95 ft)
GROUND PLANE
MLG EXTENSION/RETRACTION
PIT
P_AC_020901_1_0020001_01_00
NLG/MLG Extension/Retraction Pit
FIGURE-2-9-1-991-002-A01
2-9-1
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
0.38° REF
AIRCRAFT JACKED AT 20% MAC
FUSELAGE DATUM LINE
FWD
NLG FULLY EXTENDED
0.09 m
(0.30 ft)
NLG WEIGHT
ON WHEELS
CLEARANCE BETWEEN
BOTTOM OF MAIN FITTING
AND TOP OF PISTON
EXTENT OF PIT TO ALLOW
REMOVAL OF THE NLG
SHOCK ABSORBER WITH
TROLLEY POSITIONED
AFT OF NLG
SLIDING TUBE
GROUND PLANE
1.85 m
(6.07 ft)
NLG SHOCK ABSORBER
REMOVAL PIT
2.03 m
(6.66 ft)
NLG SHOCK ABSORBER
REMOVAL TROLLEY
2.03 m
(6.66 ft)
0.11° REF
AIRCRAFT JACKED AT 41% MAC
FUSELAGE DATUM LINE
FWD
MLG FULLY EXTENDED
CLEARANCE BETWEEN
BOTTOM OF MAIN FITTING
AND TOP OF PISTON
MLG WEIGHT ON WHEELS
2.25 m
(7.38 ft)
EXTENT OF PIT TO ALLOW
ROTATION OF THE SLIDER
FWD OF MLG
MLG SHOCK ABSORBER
REMOVAL PIT
MLG REMOVAL TOOL
TRANSPORTATION PALLET
0.09 m
(0.30 ft)
GROUND PLANE
MLG SLIDER
TRANSPORTATION PALLET
2.40 m
(7.87 ft)
2.80 m
(9.19 ft)
P_AC_020901_1_0030001_01_00
NLG/MLG Shock Absorber Removal Pit
FIGURE-2-9-1-991-003-A01
2-9-1
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
0.38° REF
AIRCRAFT JACKED AT 20% MAC
**ON A/C A350-900
FUSELAGE DATUM LINE
NLG LOWERED UNTIL ZERO
CLEARANCE BETWEEN TOP OF
NLG AND NOSE FUSELAGE PROFILE
FWD
EXTENT OF PIT TO
ALLOW REMOVAL OF
THE NLG AND TROLLEY
TO GROUND LEVEL WITH
ZERO CLEARANCE TO
THE NOSE FUSELAGE
NLG WEIGHT
ON WHEELS
EXTENT OF PIT
WITH NLG TROLLEY
TOWING HANDLE
EXTENDED 0.94 m
(3.08 ft)
NLG PISTON
NLG TROLLEY
GROUND PLANE
NLG REMOVAL PIT
3.52 m
(11.55 ft)
4.60 m
(15.09 ft)
0.63 m
(2.07 ft)
7.66 m
(25.13 ft)
8.74 m
(28.67 ft)
0.11° REF
AIRCRAFT JACKED AT 41% MAC
FUSELAGE DATUM LINE
FWD
MLG LOWERED
UNTIL ZERO
CLEARANCE
BETWEEN TOP OF
MLG AND LOWER
WING O/S SKIN LINE
MLG PISTON
MLG WEIGHT ON WHEELS
MLG REMOVAL PIT
MLG TROLLEY
GROUND PLANE
1.36 m
(4.46 ft)
1.12 m
(3.67 ft)
EXTENT OF PIT
WITH MLG TROLLEY
TOWING HANDLE
EXTENDED
4.06 m
(13.32 ft)
5.55 m
(18.21 ft)
P_AC_020901_1_0040001_01_00
NLG/MLG Removal Pit
FIGURE-2-9-1-991-004-A01
2-9-1
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0
Exterior Lighting
**ON A/C A350-900
Exterior Lighting
1.
This section gives the location of the aircraft exterior lighting.
EXTERIOR LIGHTING
ITEM
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
DESCRIPTION
RIGHT NAVIGATION LIGHT (GREEN)
LEFT NAVIGATION LIGHT (RED)
TAIL NAVIGATION LIGHT (WHITE)
UPPER ANTI-COLLISION LIGHT/BEACON
(RED)
LOWER ANTI-COLLISION LIGHT/BEACON
(RED)
LOGO LIGHTS
ENGINE SCAN LIGHTS
WING SCAN LIGHTS
WING STROBE LIGHT (HIGH INTENSITY,
WHITE)
TAIL STROBE LIGHT (HIGH INTENSITY,
WHITE)
TAXI CAMERA LIGHTS (NLG)
TAXI CAMERA LIGHTS (MLG)
LANDING LIGHTS
RUNWAY TURN-OFF LIGHTS
TAXI LIGHTS
TAKE-OFF LIGHTS
CARGO COMPARTMENT FLOOD LIGHTS
LANDING GEAR BAY/WELL LIGHTS (DOME)
2-10-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
9
3
6
1
6
4
9
2
7
8
7
8
11
12
5
12
10
P_AC_021000_1_0010002_01_00
Exterior Lighting
FIGURE-2-10-0-991-001-B01
2-10-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
13
13
16
15
16
14
6
6
P_AC_021000_1_0020001_01_00
Exterior Lighting
FIGURE-2-10-0-991-002-A01
2-10-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
3
5
1
2
4
8
7
11
11
14
14
15
P_AC_021000_1_0030002_01_00
Exterior Lighting
FIGURE-2-10-0-991-003-B01
2-10-0
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
10
12
12
9
9
16
13
13
P_AC_021000_1_0040001_01_00
Exterior Lighting
FIGURE-2-10-0-991-004-A01
2-10-0
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
18
17
17
18
EXAMPLE FOR LIGHT N° 17
CEILING LIGHT
SPOT LIGHT
P_AC_021000_1_0050001_01_00
Exterior Lighting
FIGURE-2-10-0-991-005-A01
2-10-0
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0
Antennas and Probes Location
**ON A/C A350-900
Antennas and Probes Location
1.
This section gives the location of antennas and probes.
2-11-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
15
1
2
3 4
5 6 7
23
28
24
27 26 25
8
9
10
11 12
13
14
17
22 21 20 19 18
16
29
30
31
32
40
1 − LOC
2 − SSA 1
3 − TAT PROBE 1, 2
4 − ICE PROBE
5 − GNSS 1
6 − GNSS 2
7 − TCAS 2 (TOP)
8 − WACS
9 − SATCOM
10 − VHF 1
11 − ADF 1
12 − ADF 2
13 − VHF 3
14 − ELT
15 − HF
16 − MARKER
17 − ISP LH
18 − DME 2
19 − RADIO ALT R2
20 − RADIO ALT E2
39 38 37 36 35 34 33
21 − DME 1
22 − TCAS 1 (BOTTOM)
23 − PITOT
24 − MFP 1
25 − AOA
26− ICE PROBE DETECTOR
27 − GLIDE
28 − WEATHER RADAR
29 − VOR
30 − ISP RH
31 − TCAS 1 (TOP)
32 − SSA 2, 3
33 − ICE PROBE PROTECTOR
34 − MFP 2, 3
35 − RADIO ALT E1
36 − RADIO ALT R1
37 − RADIO ALT R3
38 − RADIO ALT E3
39 − TCAS 2 (BOTTOM)
40 − VHF 2
NOTE:
LOCATION DEPENDING OF AIRCRAFT CONFIGURATION
P_AC_021100_1_0010001_01_00
Antennas and Probes Location
FIGURE-2-11-0-991-001-A01
2-11-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0
Engine and Nacelle
**ON A/C A350-900
Engine and Nacelle
1.
Power Plant
The A350--900 has two main power plants, one installed under each wing on a pylon.
Each power plant can be lowered for removal from its pylon.
The power plant comprises the:
- Nacelle,
- Engine.
2.
Nacelle
The nacelle comprises the following assemblies:
- Air intake,
- Fan cowls,
- Thrust reverser,
- Exhaust system.
3.
A.
Fan Cowl
A power door opening system is installed to assist in opening the cowls.
The cowls have access doors for fan case-mounted components.
B.
Thrust Reverser
The engine thrust reverser consists primarily of a inner fixed structure and an outer translating
sleeve.
The fan exhaust stream is reversed by the cascades and blocker doors, which form part of the
translating sleeve actuated by an electrical Thrust Reverser Actuation System (TRAS).
A power door opening system is used to assist thrust reverser cowl opening.
The thrust reverser latching system is designed so that the remote latches close only when the
hooks are engaged.
Means are provided to latch and secure a thrust reverser in the stowed position.
Means are provided to permit actuation of the thrust reversers without engine operation, for
maintenance purposes, either using the TRAS powered by the aircraft or by manual drive with
external Ground Support Equipment (GSE).
C.
Exhaust System
The exhaust system consists of a primary nozzle and a center body plug.
The exhaust system is designed to optimize aerodynamics and acoustic performance.
Engine
A.
Ignition
Each engine is equipped with a dual ignition system controlled by the FADEC.
Each engine is equipped with an automatic flame-out protection.
2-12-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B.
Cooling System
A nacelle cooling and ventilating system automatically provides the airflow required for cooling
engine and nacelle accessories and associated structure.
C.
Power Control
Forward thrust of each engine is controlled by a throttle control lever mounted on the center
pedestal in the cockpit.
Thrust reverser control is by means of a separate lever for each engine.
D.
Engine Master Control
Engine fuel shutoff is controlled by switches installed on the center pedestal.
E.
Emergency Shutdown
Actuation of the fire controls closes the associated LP valves.
F.
Indicating
Indications for each engine are displayed on the Control and Display System (CDS).
G.
Oil
The propulsion system has an independent integral oil system that is able to provide the
appropriate quantity of oil, at the temperature necessary for continuous propulsion system
operation, for all achievable conditions within the propulsion system operating envelope.
Means are provided for gravity filling.
It is possible to visually check and replenish the engine oil level without opening the fan cowl
door.
Magnetic chip detectors are installed in the lubrication system.
H.
Starting
The engine is equipped with a pneumatic air turbine starter.
The starter can be supplied with air either from the APU, or the other engine, or an Air Start
Unit (AS).
Standard types of GSE can be used.
2-12-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
5.09 m
(16.70 ft)
0.72 m
(2.39 ft)
11.10 m
(36.42 ft)
2.03 m
(6.66 ft)
1.53 m
(5.02 ft)
1.68 m
(5.51 ft)
1.94 m
(6.36 ft)
2.09 m
(6.86 ft)
1.40 m
(4.59 ft)
6.40 m
(21 ft)
1.65 m
(5.41 ft)
3.94 m
(12.93 ft)
3.17 m
(10.40 ft)
3.52 m
(11.55 ft)
1.48 m
(4.86 ft)
0.89 m
(2.92 ft)
REFER
TO SECTION
2−3−0
NOTE:
APPROXIMATE DIMENSIONS DEPENDING ON AIRCRAFT CONFIGURATION
P_AC_021200_1_0010001_01_00
Engine and Nacelle
(Sheet 1 of 3)
FIGURE-2-12-0-991-001-A01
2-12-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
C
A
FC
A
D
TR
B
B
5.50 m
(18.04 ft)
1.01 m
(3.31 ft)
C
D
6.39 m
(20.96 ft)
1.28 m
(4.20 ft)
NOTE:
APPROXIMATE DIMENSIONS DEPENDING ON AIRCRAFT CONFIGURATION.
FC: FAN COWL AND TR: THRUST REVERSER
P_AC_021200_1_0010001_02_00
Engine and Nacelle
(Sheet 2 of 3)
FIGURE-2-12-0-991-001-A01
2-12-0
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
C
A
FC
A
TR=45°
D
TR
B
B
6.42 m
(21.06 ft)
1.51 m
(4.95 ft)
FC=50°
C
D
7.13 m
(23.40 ft)
1.81 m
(5.94 ft)
NOTE:
APPROXIMATE DIMENSIONS DEPENDING ON AIRCRAFT CONFIGURATION.
FC: FAN COWL AND TR: THRUST REVERSER
P_AC_021200_1_0010001_03_00
Engine and Nacelle
(Sheet 3 of 3)
FIGURE-2-12-0-991-001-A01
2-12-0
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-1
APU
**ON A/C A350-900
APU
1.
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 the top right area of the tail cone.
The exhaust gases pass overboard at the end of the fuselage cone.
2-12-1
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
Z315, Z316
ENGINE
A
FR112
EXHAUST
SYSTEM
AIR SYSTEM
B
IGNITION
AND
STARTING
SYSTEM
FR104
A
ENGINE FUEL
AND
CONTROL
SYSTEM
AIR SYSTEM
FR104
FR109
B
OIL
SYSTEM
P_AC_021201_1_0010001_01_00
APU
FIGURE-2-12-1-991-001-A01
2-12-1
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0
Levelling, Symmetry and Alignement
**ON A/C A350-900
Levelling, Symmetry and Alignement
1.
Quick Leveling
There are three alternative procedures to level the aircraft:
- Quick leveling procedure with Air Data/Inertial Reference System (ADIRS),
- 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 10 and 17 for longitudinal leveling) and under the wings (points 1 LH and 1 RH 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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RIB5
RIB4
FR92
1RH
17
RIB5
RIB4
10
1LH
FR22
FR23
P_AC_021300_1_0010001_01_00
Location of Leveling Points
FIGURE-2-13-0-991-001-A01
2-13-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-1
Jacking for Maintenance
**ON A/C A350-900
Jacking for Maintenance
1.
2.
Aircraft Jacking Points for Maintenance
A.
The A350-900 can be jacked:
- At not more than 164000 kg (361558 lb),
- Within the limits of the permissible wind speed when the aircraft is jacked outside a closed
environment.
B.
Primary Jacking Points
The aircraft is provided with three primary jacking points:
- One located on the forward lower left fuselage (FR12),
- Two located under the wings (one under each wing, RIB9).
C.
Auxiliary Jacking Point (Safety Stay)
- When the aircraft is on jacks, a safety stay is placed under the fuselage at FR98 to prevent
tail tipping caused by accidental displacement of the aircraft center of gravity.
- The safety point must not be used for lifting the aircraft.
Jacks and Safety Stay
A.
Jack Design
- The maximum eligible static load given in table (FIGURE 2-14-1-991-001-A) are the
maximum loads applicable on jack fittings.
- In fully retracted position (jack stroke at minimum), the height of the jacks is such that the
jack may be placed beneath the aircraft under the most adverse conditions, namely, tires
deflated and shock absorbers depressurized, with a sufficient clearance between the aircraft
jacking point and the jack upper end.
- The jacks stroke enables the aircraft to be jacked up so that the Fuselage Datum Line
(FDL) may be positioned up to 7.30 m (23.95 ft.) from the ground to allow all required
maintenance procedure and in particular, the removal/installation of the landing-gear shock
absorbers.
B.
Safety Stay
The stay stroke enables the aircraft tail to be supported up to the Fuselage Datum Line (FDL)
positioned at 7.30 m (23.95 ft.) from the ground.
2-14-1
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RIB9
WING JACKING POINT
B
FUSELAGE DATUM LINE
SAFETY POINT
FR12
A
FR98
C
Y
X
FWD JACKING POINT
B’
WING JACKING POINT
RIB9
X
MAXIMUM
LOAD ELIGIBLE
Y
m
ft
m
ft
daN
FORWARD FUSELAGE
JACKING POINT
A
4.77
15.65
−1.72
−5.64
18630
WING JACKING
POINT
B
33.22
108.99
8.71
28.58
76600
B’
33.22
108.99
−8.71
−28.58
76600
SAFETY STAY
C
58.75
192.75
0
0
7650
NOTE:
SAFETY STAY IS NOT USED FOR JACKING.
P_AC_021401_1_0010001_01_00
Jacking for Maintenance
Jacking Points Location (Sheet 1 of 5)
FIGURE-2-14-1-991-001-A01
2-14-1
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FUSELAGE DATUM LINE
L
N
M
CONFIGURATION
AIRCRAFT ON WHEELS, SHOCK−ABSORBER
DEFLATED, TIRES DEFLATED (RH)
A/C ON JACKS, FDL AT 6.50 m (21.33 ft),
A/C FUSELAGE PARALLEL TO THE GROUND,
SHOCK−ABSORBER RELAXED, CLEARANCE
OF MAIN GEAR WHEELS = 1.17 m (3.84 ft)
(STANDARD TIRES *), CLEARANCE OF
NOSE GEAR WHEELS = 1.38 m (4.53 ft)
(STANDARD TIRES *)
AIRCRAFT ON WHEELS (STANDARD TIRES *)
MAXIMUM JACKING WEIGHT
= 164 000 kg (361 558 lb)
AIRCRAFT ON WHEELS (STANDARD TIRES *)
A/C WEIGHT = 142 000 kg (313 056 lb)
CG
POSITION
(% MAC)
HEIGHT
L
M
m
ft
m
N
ft
4.70 LH 15.42 LH
4.00 RH 13.12 RH
4.68 LH 15.35 LH
4.00 RH 13.12 RH
m
ft
4.71
15.45
4.48
14.70
20
3.12 10.24
41
3.36
20
4.32 14.17
5.66
18.57
6.12
20.08
41
4.32 14.17
5.66
18.57
6.12
20.08
20
3.06
10.04
4.58
15.03
5.15
16.90
41
3.29
10.79
4.57
14.99
4.91
16.11
20
3.09
10.14
4.62
15.16
5.19
17.03
41
3.34
10.96
4.60
15.09
4.93
16.18
11.02
NOTE:
* STANDARD TIRES: NOSE LANDING GEAR = 1 050 x 395 R16
MAIN LANDING GEAR = 1 400 x 530 R23
P_AC_021401_1_0010001_02_01
Jacking for Maintenance
Jacking Dimensions (Sheet 2 of 5)
FIGURE-2-14-1-991-001-A01
2-14-1
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
Z120
FR11
FR12
FR12
FR13
FR13
FR14
NOSE JACK
ADAPTOR
A
P_AC_021401_1_0010001_03_00
Jacking for Maintenance
Forward Jacking Point (Sheet 3 of 5)
FIGURE-2-14-1-991-001-A01
2-14-1
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RIB9
REAR SPAR
A
571FB (671FB)
A
Z571 (Z671)
PLATE COVER
PROTECTOR
A
WING JACK
ADAPTOR
A
A A
P_AC_021401_1_0010001_04_01
Jacking for Maintenance
Wing Jacking Point (Sheet 4 of 5)
FIGURE-2-14-1-991-001-A01
2-14-1
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FR98
BEAM5
Z310
FR98
A
B
A
AFT JACK
ADAPTOR
FR98
B
FWD
P_AC_021401_1_0010001_05_01
Jacking for Maintenance
Auxiliary Jacking Point - Safety (Sheet 5 of 5)
FIGURE-2-14-1-991-001-A01
2-14-1
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-2
Jacking of the Landing Gear
**ON A/C A350-900
Jacking for wheel change
1.
General
To replace either the wheel or brake unit assemblies on any of the landing gears, it is necessary to lift
the landing gear with a jack.
The landing gear can be lifted by a pillar jack or with a cantilever jack.
NOTE : You can lift the aircraft at Maximum Ramp Weight (MRW).
2.
Nose Landing Gear (NLG)
To lift the NLG axle with a jack, a dome shaped pad is installed between the wheels.
The reaction loads at the jacking position are shown in FIGURE 2-14-2-991-002-A.
NOTE : The maximum load at NLG jacking point is 33758 daN.
3.
Main Landing Gear (MLG)
To lift the MLG bogie with jacks, a dome shaped pad is installed below the FWD and AFT ends of
each bogie beam.
Each pair of wheels and brake units can be replaced on the end of the bogie that is lifted.
Both FWD and AFT ends of the bogie beam can be lifted together, but the bogie beam must be kept
level during the lift to prevent damage.
The reaction loads at the jacking position are shown in FIGURE 2-14-2-991-003-A.
NOTE : The maximum load at each MLG jacking point is 83892.5 daN.
2-14-2
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
A
B
FWD
A
− A : DOME HEIGHT
− B : DISTANCE BETWEEN TYRES
A350−900 NLG (1 050 x 395 R16)
CONFIGURATION (ASSUME
ALL OTHER TYRES ON
THE A/C ARE INTACT)
WEIGHT (T)
2 TYRES (NORMAL)
MRW
1 FLAT TYRE
CG
(% MAC)
DIM A
DIM B
mm
in
mm
in
26.2
291
11.45
261
10.27
MRW
26.2
227
8.93
214
8.42
2 FLAT TYRES & 50% RIM
FLANGE DAMAGE
MLW
20
75
2.95
191
7.51
2 FLAT TYRES & NO RIM
FLANGE DAMAGE
MLW
20
97
3.81
191
7.51
P_AC_021402_1_0020001_01_00
Nose Landing Gear Jacking Point Heights
FIGURE-2-14-2-991-002-A01
2-14-2
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
A
C
B
FWD
− A : DOME HEIGHT
− B : DISTANCE BETWEEN TYRES
− C : DISTANCE BETWEEN BRAKE RODS AND GROUND
A
A350−900 MLG (1 400 x 530 R23)
CONFIGURATION
DIM A
DIM A
DIM B
DIM B
(ASSUME ALL OTHER WEIGHT
CG
AFT
FWD
AFT
FWD
TYRES ON THE A/C
(T)
(% MAC)
mm
in
mm
in
mm
in
mm
in
ARE INTACT)
4 TYRES (NORMAL)
33.2
378 14.88 378 14.88 1 029 40.51 1 036 40.78
MRW
FWD INNER TYRE
33.2
304 11.96 381 15.00 981 38.62 1 041 40.98
MRW
UNSERVICEABLE
FWD OUTER TYRE
33.2
285 11.22 374 14.72 974 38.34 1 033 40.66
MRW
UNSERVICEABLE
AFT INNER TYRE
33.2
381 15.00 304 11.96 1 032 40.62 983 38.70
MRW
UNSERVICEABLE
AFT OUTER TYRE
33.2
374 14.72 285 11.22 1 025 40.35 975 38.38
MRW
UNSERVICEABLE
2 FLAT FWD TYRES
42
129 5.07 404 15.90 967 38.07 1 071 42.16
MLW
& 50% RIM DAMAGE
2 FLAT AFT TYRES
42
404 15.90 129 5.07 1 060 41.73 967 38.07
MLW
& 50% RIM DAMAGE
4 FLAT TYRES &
42
136 5.35 136 5.35 967 38.07 967 38.07
MLW
50% RIM DAMAGE
2 FLAT FWD TYRES
42
159 6.25 403 15.86 967 38.07 1 071 42.16
MLW
& NO RIM DAMAGE
2 FLAT AFT TYRES
42
403 15.86 159 6.25 1 059 41.69 967 38.07
MLW
& NO RIM DAMAGE
4 FLAT TYRES &
42
166 6.53 166 6.53 967 38.07 967 38.07
MLW
NO RIM DAMAGE
TYRE CHANGE
FWD MAX GROWN
TYRE 25 mm
33.2
541 21.29 378 14.88 1 113 43.81 1 029 40.51
MRW
FROM GROUND
AFT MAX GROWN
33.2
378 14.88 541 21.29 1 029 40.51 1 113 43.81
MRW
TYRE 25 mm
FROM GROUND
8 FLAT TYRES &
26.2
118 4.64 118 4.64 967 38.07 967 38.07
MRW
50% RIM DAMAGE
8 FLAT TYRES &
26.2
149 5.86 149 5.86 967 38.07 967 38.07
MRW
NO RIM DAMAGE
DIM C
FWD
mm
in
DIM C
AFT
mm
in
267 10.51 267 10.51
194 7.63
271 10.66
175 6.88 264 10.39
271 10.66 193 7.59
264 10.39 175 6.88
18
0.70 293 11.53
293 11.53 18
0.70
26
1.02
1.02
48
1.88 293 11.53
26
293 11.53 48
1.88
55
2.16
2.16
55
431 16.96 268 10.55
268 10.55 430 16.92
7
0.27
7
0.27
39
1.53
39
1.53
P_AC_021402_1_0030001_01_00
Main Landing Gear Jacking Point Heights
FIGURE-2-14-2-991-003-A01
2-14-2
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0
General Information
**ON A/C A350-900
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
?C
?F
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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-0
Take-Off Weight Limitation
**ON A/C A350-900
Take-Off Weight Limitation
1.
This section provides the take-off weight limitation at ISA conditions and ISA + 15 ˚C (+59 ˚F)
conditions on a dry runway.
3-3-0
Page 1
Apr 01/15
3-3-0
MTOW
130
1 500
150
170
190
210
230
250
270
2 000
6 920
2 500
8 920
3 500
RUNWAY LENGTH (m)
3 000
RUNWAY LENGTH (ft)
10 920
14 920
4 000
4 500
0 ft
2 000 ft
4 000 ft
6 000 ft
8 000 ft
AIRPORT PRESSURE ALTITUDE
12 920
NOTE:
THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED
IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
TAKE−OFF WEIGHT (x 1 000 kg)
4 920
290
286.6
5 000
336.6
386.6
436.6
486.6
536.6
586.6
636.6
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_030300_1_0010001_01_01
ISA Conditions
FIGURE-3-3-0-991-001-A01
Page 2
Apr 01/15
TAKE−OFF WEIGHT (x 1 000 lb)
3-3-0
MTOW
130
1 500
150
170
190
210
230
250
270
2 000
6 920
2 500
8 920
3 500
RUNWAY LENGTH (m)
3 000
RUNWAY LENGTH (ft)
10 920
14 920
4 000
4 500
0 ft
2 000 ft
4 000 ft
6 000 ft
8 000 ft
AIRPORT PRESSURE ALTITUDE
12 920
NOTE:
THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED
IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
TAKE−OFF WEIGHT (x 1 000 kg)
4 920
290
286.6
5 000
336.6
386.6
436.6
486.6
536.6
586.6
636.6
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_030300_1_0020001_01_01
ISA + 15 ˚C (+59 ˚F) Conditions
FIGURE-3-3-0-991-002-A01
Page 3
Apr 01/15
TAKE−OFF WEIGHT (x 1 000 lb)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-0
Landing Field Length
**ON A/C A350-900
Landing Field Length
1.
This section provides the landing field length on a dry runway.
3-4-0
Page 1
Apr 01/15
3-4-0
1 200
130
1 400
1 600
1 800
2 000
2 200
2 400
326.6
140
150
386.6
180
LANDING WEIGHT (x 1 000 kg)
160
170
366.6
LANDING WEIGHT (x 1 000 lb)
346.6
VALID FOR ALL TEMPERATURES
306.6
426.6
446.6
190
8 000 ft
6 000 ft
4 000 ft
2 000 ft
0 ft
200
AIRFIELD ELEVATION
406.6
NOTE:
THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED
IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
REQUIRED LANDING DISTANCE (m)
286.6
2 600
210
4 280
4 780
5 280
5 780
6 280
6 780
7 280
7 780
8 280
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_030400_1_0010001_01_01
Landing Field Length
FIGURE-3-4-0-991-001-A01
Page 2
Apr 01/15
REQUIRED LANDING DISTANCE (ft)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0
Final Approach Speed
**ON A/C A350-900
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, 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 140 kt at a MLW of 205000 kg (451948 lb) and classifies the aircraft
into the Aircraft Approach Category C.
NOTE : This value is given for information only.
3-5-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-2-0
Turning Radii
**ON A/C A350-900
Turning Radii
1.
This section gives the turning radii.
4-2-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
R5
R3
R1
70° 65°
60°
R2
R4
R6
NOTE:
FOR TURNING RADII VALUES, REFER TO SHEET 2
P_AC_040200_1_0010001_01_00
Turning Radii
(Sheet 1 of 2)
FIGURE-4-2-0-991-001-A01
4-2-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A350−900 TURNING RADII
TYPE OF STEERING
EFFECTIVE
TURN ANGLE (deg) STEERING ANGLE (deg)
2
20
19.6
2
25
24.5
2
30
29.4
2
35
34.2
2
40
39.1
2
45
43.8
2
50
48.6
2
55
53.1
2
60
57.5
2
65
61.5
2
70
65.0
2
72 (MAX)
66.1
1
50
49.3
1
55
54.1
1
60
58.7
1
65
63.2
1
70
67.5
1
72 (MAX)
69.2
R1
R2
RMLG LMLG
R3
NLG
R4
WING
R5
NOSE
R6
TAIL
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
76.3
250
58.7
193
46.7
153
38.0
125
31.1
102
25.7
84
21.1
69
17.4
57
14.1
46
11.4
37
9.2
30
8.5
28
86.9
285
69.3
227
57.3
188
48.6
159
41.7
137
36.3
119
31.7
104
28.0
92
24.7
81
22.0
72
19.8
65
19.1
63
86.0
282
69.6
228
58.9
193
51.5
169
45.9
151
41.8
137
38.6
127
36.2
119
34.3
113
32.9
108
31.9
105
31.6
104
113.6
373
96.2
316
84.3
277
75.7
248
68.9
226
63.7
209
59.2
194
55.5
182
52.4
172
49.8
163
47.7
156
47.0
154
87.1
286
71.2
233
60.8
199
53.7
176
48.5
159
44.7
147
41.8
137
39.6
130
38.0
125
36.7
121
35.9
118
35.6
117
96.0
315
79.7
262
69.0
226
61.5
202
55.9
183
51.7
170
48.3
158
45.7
150
43.5
143
41.9
137
40.6
133
40.2
132
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
20.5
67
16.6
54
13.3
43
10.3
34
7.7
25
6.7
22
31.1
102
27.2
89
23.9
78
20.9
69
18.3
60
17.3
57
38.2
125
35.7
117
33.8
111
32.4
106
31.2
103
30.9
101
58.6
192
54.8
180
51.6
169
48.7
160
46.2
152
45.3
149
41.4
136
39.2
129
37.6
123
36.3
119
35.3
116
35.0
115
47.8
157
45.1
148
43.0
141
41.2
135
39.8
130
39.2
129
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.
P_AC_040200_1_0010001_02_00
Turning Radii
(Sheet 2 of 2)
FIGURE-4-2-0-991-001-A01
4-2-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0
Minimum Turning Radii
**ON A/C A350-900
Minimum Turning Radii
1.
This section gives the minimum turning radii.
4-3-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
R5
R3
X
Y
R4
A
(MINIMUM TURNING WIDTH)
R6
NOTE:
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
A350−900 MINIMUM TURNING RADII
TYPE OF STEERING
EFFECTIVE
TURN ANGLE (deg) STEERING ANGLE (deg)
1
72 (MAX)
69.2
2
72 (MAX)
66.1
m
ft
m
ft
X
Y
A
R3
NLG
R4
WING
R5
NOSE
R6
TAIL
28.7
94
28.7
94
10.9
36
12.7
42
48.5
159
51.1
168
30.9
101
31.6
104
45.3
149
47.0
154
35.0
115
35.6
117
39.2
129
40.2
132
NOTE:
IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1
BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
P_AC_040300_1_0010001_01_00
Minimum Turning Radii
FIGURE-4-3-0-991-001-A01
4-3-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0
Visibility from Cockpit in Static Position
**ON A/C A350-900
Visibility from Cockpit in Static Position
1.
This section gives the visibility from cockpit in static position.
4-4-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
NOT TO BE USED FOR
LANDING APPROACH VISIBILITY
DIMENSIONS ARE APPROXIMATE
27°
VISUAL ANGLES IN VERTICAL
PLANE THROUGH PILOT
EYE POSITION.
20°
3.04 m
(9.97 ft)
14.20 m
(46.59 ft)
105.5°
120°
FIRST OFFICER
FIELD OF VIEW
4.63 m
(15.19 ft)
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
105.5°
120°
0.53 m
(1 ft 8.88 in)
VISUAL ANGLES IN PLANE
PERPENDICULAR TO
LONGITUDINAL AXIS.
32°
32°
15°
15°
NOTE:
PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
ZONE THAT CANNOT BE SEEN
P_AC_040400_1_0010001_01_00
Visibility from Cockpit in Static Position
FIGURE-4-4-0-991-001-A01
4-4-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0
Runway and Taxiway Turn Paths
**ON A/C A350-900
Introduction
1.
This section gives the runway and taxiway turnpaths for the following configurations:
- 90˚ Turn --- Runway to Taxiway
- 135˚ Turn --- Runway to Taxiway
- 180˚ U-Turn on Runway
- 90˚ Turn --- Taxiway to Taxiway
- 135˚ Turn --- Taxiway to Taxiway
The turnpaths Runway to Taxiway and Taxiway to Taxiway are defined using 2 methods:
- Oversteering method,
- Cockpit over centerline method.
The 180 U-Turn on runway is defined using the following method:
- U-Turn using edge of runway method.
4-5-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1
90˚ Turn - Runway to Taxiway
**ON A/C A350-900
90˚ Turn - Runway to Taxiway
1.
This section gives the 90˚ turn - runway to taxiway.
4-5-1
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX 10.9 m
(36 ft)
23 m
(75 ft)
APPROX 13.3 m
(44 ft)
TAXIWAY
CENTERLINE
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
NLG PATH
MLG PATH
RUNWAY CENTERLINE
45 m
(150 ft)
P_AC_040501_1_0010001_01_02
90˚ Turn - Runway to Taxiway
Oversteering Method (Sheet 1 of 2)
FIGURE-4-5-1-991-001-A01
4-5-1
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX 5 m
(16 ft)
23 m
(75 ft)
TAXIWAY CENTERLINE
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
NLG PATH
MLG PATH
RUNWAY CENTERLINE
45 m
(150 ft)
P_AC_040501_1_0010001_02_02
90˚ Turn - Runway to Taxiway
Cockpit over Centerline Method (Sheet 2 of 2)
FIGURE-4-5-1-991-001-A01
4-5-1
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2
135˚ Turn - Runway to Taxiway
**ON A/C A350-900
135˚ Turn - Runway to Taxiway
1.
This section gives the 135˚ turn - runway to taxiway.
4-5-2
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
APPROX 5.8 m
(19 ft)
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX 7.6 m
(25 ft)
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
TAXIWAY
CENTERLINE
23 m
(75 ft)
NLG PATH
RUNWAY CENTERLINE
MLG PATH
45 m
(150 ft)
P_AC_040502_1_0010002_01_02
135˚ Turn - Runway to Taxiway
Oversteering Method (Sheet 1 of 2)
FIGURE-4-5-2-991-001-B01
4-5-2
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RUNWAY
CENTERLINE
TURN R = 45 m
(150 ft)
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX
1.6 m (5 ft)
FILLET R = 25.5 m
(85 ft)
ADDITIONAL FILLET TO MEET
4.5 m (15 ft) EDGE CLEARANCE
TAXIWAY
CENTERLINE
23 m
(75 ft)
NLG PATH
MLG PATH
45 m
(150 ft)
P_AC_040502_1_0010002_02_02
135˚ Turn - Runway to Taxiway
Cockpit over Centerline Method (Sheet 2 of 2)
FIGURE-4-5-2-991-001-B01
4-5-2
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3
180˚ Turn on a Runway
**ON A/C A350-900
180˚ Turn on a Runway
1.
This section gives the 180˚ turn on a runway.
4-5-3
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RUNWAY CENTERLINE
R4 = 45.3 m
(149 ft)
R3 = 30.9 m
(101 ft)
4.5 m
(15 ft)
R5 = 35 m
(115 ft)
4.5 m
(15 ft)
APPROX 48.5 m
(159.12 ft)
NLG PATH
NOSE TIP PATH
MLG PATH
WING TIP PATH
NOTE:
TYPE 1 VALUES.
IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYING DIFFERENTIAL
BRAKING DURING THE WHOLE TURN.
P_AC_040503_1_0010001_01_01
180˚ Turn on a Runway
FIGURE-4-5-3-991-001-A01
4-5-3
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4
90˚ Turn - Taxiway to Taxiway
**ON A/C A350-900
90˚ Turn - Taxiway to Taxiway
1.
This section gives the 90˚ turn - taxiway to taxiway.
4-5-4
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX 10.5 m
(34 ft)
23 m
(75 ft)
APPROX 12.9 m
(42 ft)
TAXIWAY
CENTERLINE
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
NLG PATH
TAXIWAY CENTERLINE
MLG PATH
23 m
(75 ft)
P_AC_040504_1_0010001_01_02
90˚ Turn - Taxiway to Taxiway
Oversteering Method (Sheet 1 of 2)
FIGURE-4-5-4-991-001-A01
4-5-4
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX 3.9 m
(13 ft)
23 m
(75 ft)
ADDITIONAL FILLET TO MEET
4.5 m (15 ft) EDGE CLEARANCE
TAXIWAY
CENTERLINE
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
TAXIWAY CENTERLINE
NLG PATH
MLG PATH
23 m
(75 ft)
P_AC_040504_1_0010001_02_02
90˚ Turn - Taxiway to Taxiway
Cockpit over Centerline Method (Sheet 2 of 2)
FIGURE-4-5-4-991-001-A01
4-5-4
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5
135˚ Turn - Taxiway to Taxiway
**ON A/C A350-900
135˚ Turn - Taxiway to Taxiway
1.
This section gives the 135˚ turn - taxiway to taxiway.
4-5-5
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
APPROX 6.9 m
(23 ft)
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX 8.8 m
(29 ft)
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
TAXIWAY
CENTERLINE
TAXIWAY CENTERLINE
23 m
(75 ft)
NLG PATH
MLG PATH
23 m
(75 ft)
P_AC_040505_1_0010002_01_02
135˚ Turn - Taxiway to Taxiway
Oversteering Method (Sheet 1 of 2)
FIGURE-4-5-5-991-001-B01
4-5-5
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
TURN R = 45 m
(150 ft)
FAA LEAD−IN FILLET
L=75 m (250 ft)
APPROX
2.5 m (8 ft)
FILLET R = 25.5 m
(85 ft)
ADDITIONAL FILLET TO MEET
4.5 m (15 ft) EDGE CLEARANCE
TAXIWAY
CENTERLINE
TAXIWAY CENTERLINE
23 m
(75 ft)
NLG PATH
MLG PATH
23 m
(75 ft)
P_AC_040505_1_0010002_02_02
135˚ Turn - Taxiway to Taxiway
Cockpit over Centerline Method (Sheet 2 of 2)
FIGURE-4-5-5-991-001-B01
4-5-5
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0
Runway Holding Bay (Apron)
**ON A/C A350-900
Runway Holding Bay (Apron)
1.
This section gives the runway holding bay (Apron).
4-6-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
6.1 m
(20 ft)
MAIN LANDING
GEAR PATH
90 m
(300 ft)
102 m
(335 ft)
12.2 m
(40 ft)
6.1 m
(20 ft)
HOLDING
POINT
190 m
(625 ft)
TAXIWAY
CENTERLINE
RUNWAY
CENTERLINE
23 m
(75 ft)
45 m
(150 ft)
NOTE:
COORDINATE WITH USING AIRCRAFT FOR SPECIFIC PLANNED OPERATING PROCEDURES.
P_AC_040600_1_0010001_01_00
Runway Holding Bay (Apron)
FIGURE-4-6-0-991-001-A01
4-6-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0
Minimum Line-Up Distance Corrections
**ON A/C A350-900
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 4.5 m (15 ft.) from the taxiway edge, and finishes with the aircraft aligned on the
centerline of the runway.
During the turn, all the clearances must meet the minimum value of 4.5 m (15 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 4.5 m (15 ft.) from the pavement edge, and it
finishes with the aircraft aligned on the centerline of the runway.
During the turn, all the clearances must meet the minimum value of 4.5 m (15 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 (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.
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 4.5 m (15 ft.) for this category
of aircraft as recommended in ICAO Annex 14.
4-7-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
4.5 m
(15 ft)
TODA
TAXIWAY
CENTERLINE
ASDA
> 4.5 m
(15 ft)
RUNWAY CENTERLINE
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
90° TURN ON RUNWAY ENTRY
MAX
AIRCRAFT
STEERING
TYPE
ANGLE
A350−900
72°
60 m (200 ft)
WIDE RUNWAY
45 m (150 ft)
WIDE RUNWAY
MINIMUM LINE−UP
MINIMUM LINE−UP
DISTANCE CORRECTION
DISTANCE CORRECTION
ON TODA
ON ASDA
ON TODA
ON ASDA
25.7 m 84 ft 54.3 m 178 ft 21.8 m 72 ft 50.5 m 166 ft
P_AC_040700_1_0010001_01_01
90˚ Turn on Runway Entry
FIGURE-4-7-0-991-001-A01
4-7-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
MINIMUM PAVEMENT WIDTH
4.5 m
(15 ft)
TODA
> 4.5 m
(15 ft)
4.5 m
(15 ft)
ASDA
RUNWAY CENTERLINE
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
180° TURN ON RUNWAY TURN PAD
MAX
AIRCRAFT
STEERING
TYPE
ANGLE
A350−900
72°
45 m (150 ft)
WIDE RUNWAY
60 m (200 ft)
WIDE RUNWAY
MINIMUM LINE−UP
MINIMUM LINE−UP
DISTANCE CORRECTION
DISTANCE CORRECTION
ON TODA
ON ASDA
ON TODA
ON ASDA
37.2 m 122 ft 65.9 m 216 ft 35.7 m 117 ft 64.4 m 211 ft
REQUIRED MINIMUM
PAVEMENT WIDTH
62.9 m
206 ft
P_AC_040700_1_0020001_01_01
180˚ Turn on Runway Turn Pad
FIGURE-4-7-0-991-002-A01
4-7-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
4.5 m
(15 ft)
> 4.5 m
(15 ft)
TODA
ASDA
4.5 m
(15 ft)
25°
RUNWAY CENTERLINE
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
180° TURN ON RUNWAY WIDTH
MAX
AIRCRAFT
STEERING
TYPE
ANGLE
A350−900
72°
60 m (200 ft)
WIDE RUNWAY
45 m (150 ft)
WIDE RUNWAY
MINIMUM LINE−UP
MINIMUM LINE−UP
DISTANCE CORRECTION
DISTANCE CORRECTION
ON TODA
ON ASDA
ON TODA
ON ASDA
47.5 m 156 ft 76.2 m 250 ft
NOT POSSIBLE
P_AC_040700_1_0030001_01_01
180˚ Turn on Runway Width
FIGURE-4-7-0-991-003-A01
4-7-0
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-8-0
Aircraft Mooring
**ON A/C A350-900
Aircraft Mooring
1.
This section provides information on aircraft mooring.
4-8-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
TOWING FITTING
STRAP
A
QUICK RELEASE
PIN
MOORING KIT
TENSIONER
SAFETY LEVER
WARNING FLAG
HOOK
MOORING POINT
A
P_AC_040800_1_0010001_01_01
Aircraft Mooring
FIGURE-4-8-0-991-001-A01
4-8-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-1-0
Aircraft Servicing Arrangements
**ON A/C A350-900
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 the positioning and operation on the ramp.
This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC AIR CONDITIONING UNIT
AS AIR START UNIT
BULK BULK TRAIN
CAT CATERING TRUCK
CB CONVEYOR BELT
CLEAN CLEANING TRUCK
FUEL FUEL HYDRANT DISPENSER or TANKER
GPU GROUND POWER UNIT
LDCL LOWER DECK CARGO LOADER
LV LAVATORY VEHICLE
PBB PASSENGER BOARDING BRIDGE
PS PASSENGER STAIRS
TOW TOW TRACTOR
ULD ULD TRAIN
WV POTABLE WATER VEHICLE
5-1-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-1
Typical Ramp Layout (Open Apron)
**ON A/C A350-900
Typical Ramp Layout (Open Apron)
1.
This section provides the typical ramp layout (open apron).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (25 ft.) from
the aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel
chocks in position on landing gears).
5-1-1
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
TOW
AS
GPU
PS
CAT
ULD
AC
LDCL
CAT
PS
FUEL
LDCL
BULK
CLEAN
STAND SAFETY LINE
ULD
CB
WV
CAT
LV
FEET
0 10 20 30 40 50 60
0
4
8
12 16
METERS
20
P_AC_050101_1_0010001_01_02
Typical Ramp Layout (Open Apron)
FIGURE-5-1-1-991-001-A01
5-1-1
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2
Typical Ramp Layout (Gate)
**ON A/C A350-900
Typical Ramp Layout (Gate)
1.
This section provides the baseline ramp layout (gate).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (25 ft.) 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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
TOW
AS
GPU
PBB
CAT
ULD
AC
LDCL
CAT
PBB
FUEL
LDCL
BULK
CLEAN
STAND SAFETY LINE
ULD
CB
WV
CAT
LV
FEET
0 10 20 30 40 50 60
0
4
8
12 16
METERS
20
P_AC_050102_1_0010001_01_02
Typical Ramp Layout (Gate)
FIGURE-5-1-2-991-001-A01
5-1-2
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0
Terminal Operations - Full Servicing Turn Round Time
**ON A/C A350-900
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
315 pax: 48 B/C + 267 Y/C.
All passengers deplane and board the aircraft.
2 Passenger Boarding Bridges (PBB) used at doors L1 and L2.
Equipment positioning + opening door = +3 min.
Closing door + equipment removal = +3 min.
No Passenger with Reduced Mobility (PRM) on board.
Deplaning:
- 158 pax at door L1
- 157 pax at door L2
- Deplaning rate = 25 pax/min per door
- Priority deplaning for premium passengers.
Boarding:
- 158 pax at door L1
- 157 pax at door L2
- Boarding rate = 15 pax/min per door
- Last Pax Seated allowance (LPS) + headcounting = +4 min.
B.
CARGO
2 cargo loaders + 1 belt loader.
Opening door + equipment positioning = +2.5 min.
Equipment removal + closing door = +2.5 min.
100% cargo exchange:
- FWD cargo compartment: 8 containers/4 pallets
- AFT cargo compartment: 4 containers/4 pallets
- Bulk compartment: 1000 kg (2205 lb).
Container unloading/loading times:
- Unloading = 1.2 min/container
- Loading = 1.4 min/container.
Bulk unloading/loading times:
5-2-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Unloading = 110 kg/min (243 lb/min)
- Loading = 95 kg/min (209 lb/min).
Pallet unloading/loading times:
- Unloading = 2.4 min/pallet
- Loading = 2.8 min/pallet.
C.
REFUELLING
100000 L (26418 USgal), 4 hoses, 40 psig (2.76 bars-rel).
Dispenser positioning + connection = +8 min.
Disconnection + dispenser removal = +8 min.
D.
CLEANING
Cleaning is performed in available time.
E.
CATERING
3 catering trucks for servicing galleys simultaneously at doors R1, R2 and R4.
Equipment positioning + opening door = +5 min.
Closing door + equipment removal = +3 min.
Full Size Trolley Equivalent (FSTE) to unload and load: 40 FSTE
- 10 FSTE at door R1
- 7 FSTE at door R2
- 23 FSTE at door R4.
Time for trolley exchange = 1.5 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 2 × 90 kVA.
Air Conditioning: up to 2 hoses.
Potable water servicing: 100% uplift, 1060 L (280 USgal).
Waste water servicing: draining + rinsing.
5-2-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
TRT: 61 min
0
10
20
30
40
50
60
70
DEPLANING/BOARDING AT L1
DEPLANING/BOARDING AT L2
HEADCOUNTING
CATERING AT R1
CATERING AT R2
CATERING AT R4
CLEANING
AVAILABLE TIME
CARGO FWD CC
CARGO AFT CC
BULK
REFUELING
POTABLE WATER SERVICING
WASTE WATER SERVICING
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
P_AC_050200_1_0010001_01_02
Full Servicing Turn Round Time Chart
FIGURE-5-2-0-991-001-A01
5-2-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0
Terminal Operations - Transit Turn Round Time
**ON A/C A350-900
Terminal Operations - Transit 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 transit turn round time chart
A.
PASSENGER HANDLING
315 pax: 48 B/C + 267 Y/C.
50% passengers deplane and board the aircraft.
1 Passenger Boarding Bridge (PBB) used at door L1.
Equipment positioning + opening door = +3 min.
Closing door + equipment removal = +3 min.
No Passenger with Reduced Mobility (PRM) on board.
Deplaning:
- 158 pax at door L1
- Deplaning rate = 25 pax/min per door.
Boarding:
- 158 pax at door L1
- Boarding rate = 15 pax/min per door
- Last Pax Seated allowance (LPS) + headcounting = + 4 min.
B.
CARGO
1 cargo loader + 1 belt loader.
Opening door + equipment positioning = +2.5 min.
Equipment removal + closing door = +2.5 min.
50% cargo exchange:
- AFT cargo compartment: 2 containers/2 pallets
- Bulk compartment: 500 kg (1102 lb).
Container unloading/loading times:
- Unloading = 1.2 min/container
- Loading = 1.4 min/container.
Bulk unloading/loading times:
- Unloading = 110 kg/min (243 lb/min)
- Loading = 95 kg/min (209 lb/min).
Pallet unloading/loading times:
- Unloading = 2.4 min/pallet
5-3-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
-
Loading = 2.6 min/pallet.
C.
REFUELING
No refueling.
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: t0 = 0
- Other equipment: t = t0 + 1 min.
Ground Power Unit (GPU): up to 2 × 90 kVA.
Air conditioning: up to 2 hoses.
No potable water servicing.
No waste water servicing.
5-3-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
TRT: 30 min
0
5
10
15
20
25
30
35
DEPLANING/BOARDING AT L1
HEADCOUNTING
CATERING
AVAILABLE TIME
CLEANING
AVAILABLE TIME
CARGO AFT CC
BULK
ACTIVITY
GSE POSITIONING/REMOVAL
P_AC_050300_1_0010002_01_02
Transit Turn Round Time Chart
FIGURE-5-3-0-991-001-B01
5-3-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-0
Ground Service Connections Layout
**ON A/C A350-900
Ground Service Connections Layout
1.
This section provides the ground service connections layout.
5-4-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
12 11
10
7
8
9
6
1
2
4
5
3
7
8
9
15 14
17
13
10
11
12
16
18
1 − NLG GROUNDING (EARTHING) POINT
2 − GROUND ELECTRICAL POWER CONNECTORS
3 − OXYGEN SYSTEM
4 − LOW PRESSURE AIR PRE−CONDITIONING
5 − HIGH PRESSURE AIR PRE−CONDITIONING
6 − YELLOW HYDRAULIC−SYSTEM SERVICE PANEL
7 − ENGINE OIL SERVICING
8 − STARTER OIL SERVICING
9 − VFG OIL SERVICING
10 − REFUEL/DEFUEL COUPLINGS
(OPTIONAL−LH WING)
11 − OVERPRESSURE PROTECTOR
12 − NACA FLAME ARRESTOR
13 − MLG GROUNDING (EARTHING) POINT
14 − GREEN HYDRAULIC−SYSTEM SERVICE PANEL
15 − REFUEL/DEFUEL CONTROL PANEL
16 − POTABLE WATER SERVICING PANEL
17 − WASTE WATER SERVICING PANEL
18 − APU OIL SERVICING
P_AC_050400_1_0010001_01_02
Ground Service Connections Layout
FIGURE-5-4-0-991-001-A01
5-4-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1
Grounding (Earthing) Points
**ON A/C A350-900
Grounding (Earthing) Points
1.
Grounding (Earthing) Point Locations
AFT OF NOSE
On Nose Landing
Gear leg
On left Main
Landing Gear leg
On right Main
Landing Gear leg
4.42 m
(14.5 ft.)
32.95 m
(108.1 ft.)
32.95 m
(108.1 ft.)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.07 m
(0.23 ft.)
5.59 m
(18.34 ft.)
5.59 m
(18.34 ft.)
MEAN HEIGHT
FROM GROUND
1.06 m
(3.48 ft.)
1.55 m
(5.09 ft.)
1.55 m
(5.09 ft.)
A.
The grounding (earthing) stud on each landing gear leg is designed for use with a clip-on
connector (such as an 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.
5-4-1
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
B
A
C
GROUNDING (EARTHING) POINT
B
C
P_AC_050401_1_0010001_01_00
Grounding (Earthing) Point - NLG
FIGURE-5-4-1-991-001-A01
5-4-1
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
B
A
A
A
C
LH SHOWN
RH SYMMETRICAL
GROUNDING (EARTHING) POINT
B
C
P_AC_050401_1_0020001_01_00
Grounding (Earthing) Point - MLG
FIGURE-5-4-1-991-002-A01
5-4-1
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2
Hydraulic System
**ON A/C A350-900
Hydraulic System
1.
Hydraulic System
The nominal operating pressure is 5000 psi (345 bar).
A.
Access
ACCESS
Green Hydraulic
System:
Access Door 197LB
Yellow Hydraulic
System:
Access Door 194KB
2.
AFT OF NOSE
36.37 m
(119.32 ft.)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.61 m
(2.0 ft.)
30.35 m
(99.57 ft.)
MEAN HEIGHT
FROM GROUND
2.39 m
(7.84 ft.)
1.51 m
(4.95 ft.)
B.
Reservoir Pressurization
- One 1/4 in. ISO 4570 connector.
C.
Reservoir Filling
Centralized filling capability is on the Green ground service panel.
Filling: Ground pressurized supply or hand pump.
D.
Ground Test
On each ground service panel:
- One self-sealing connector (suction)
- One self-sealing connector (delivery).
2.24 m
(7.35 ft.)
Technical Specifications
A.
The hydraulic ground equipment must be able to start with the aircraft hydraulic circuit not
pressurized.
B.
The hydraulic ground equipment must be able to permanently operate with the aircraft reservoir
pressures varying between 2.0 bar and 5.0 bar (29.0 psi and 72.51 psi).
C.
After ground equipment shutdown, no further fluid exchange must occur between the aircraft
reservoir and the ground equipment.
5-4-2
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
Z190
A
197LB
GROUND TEST PRESSURE
CONNECTION
GROUND TEST SUCTION
CONNECTION
GROUND SUPPLY
A
P_AC_050402_1_0010001_01_01
Green Ground Service Panel
FIGURE-5-4-2-991-001-A01
5-4-2
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
Z190
194KB
GROUND TEST PRESSURE
CONNECTION
GROUND TEST SUCTION
CONNECTION
A
P_AC_050402_1_0020001_01_01
Yellow Ground Service Panel
FIGURE-5-4-2-991-002-A01
5-4-2
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3
Electrical System
**ON A/C A350-900
Electrical System
1.
A/C External Power
ACCESS
AFT OF NOSE
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
A/C External
6.63 m
Power:
(21.75 ft.)
Access Door 122AR
2.
3.
0.91 m
(2.99 ft.)
MEAN HEIGHT
FROM GROUND
2.58 m
(8.46 ft.)
Technical Specifications
A.
External Power Receptacle:
- Two standard ISO 461 Style3 -- 90 kVA each.
B.
Power Supply:
- Three-phase, 115 V, 400 Hz.
C.
Electrical Connectors for Servicing:
- AC outlets: HUBBELL 5258
- DC outlets: HUBBELL 7472.
A/C Emergency Generation
ACCESS
RAT Safety-Pin
Installation:
Access Panel
198VR
AFT OF NOSE
39.48 m
(129.53 ft.)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
2.50 m
(8.2 ft.)
5-4-3
MEAN HEIGHT
FROM GROUND
2.91 m
(9.55 ft.)
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
122AR
A
ELECTRICAL POWER
RECEPTACLES
925VU
A
FWD
P_AC_050403_1_0010001_01_01
Electrical Service Panel
FIGURE-5-4-3-991-001-A01
5-4-3
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
198VR
A
198QR
B
198PR
SAFETY PIN
Z190
A
RAT RETRACTED
B
RAT EXTENDED
P_AC_050403_1_0030001_01_01
RAT
FIGURE-5-4-3-991-003-A01
5-4-3
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4
Oxygen System
**ON A/C A350-900
Oxygen System
1.
General
The crew oxygen system has two isolated subsystems:
- The left-hand side oxygen subsystem supplies oxygen to the captain and one observer.
- The right-hand side oxygen subsystem supplies oxygen to the F/O and one observer.
Each subsystem has a compartment with a HP gaseous cylinder assembly (one more cylinder
assembly for each oxygen compartment is optional).
2.
Access
Get access to the forward lower-deck cargo-compartment.
The access panel to the crew oxygen servicing point is located on the rear triangular area of the FWD
cargo door.
3.
Technical Specifications
- One 3/8 in. MIL-DTL 7891 standard service connection.
5-4-4
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FR20
A
FR30
B
Z130
FR29
A
FR28
CREW OXYGEN
FILLING PORT
CREW OXYGEN
FILLING GAGE
B
P_AC_050404_1_0010001_01_00
Oxygen System
FIGURE-5-4-4-991-001-A01
5-4-4
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FR32 FR33
FR20
C
FR21
A
B
Z130
A
OXYGEN
COMPARTMENT−CAPT
B
OXYGEN
COMPARTMENT−F/O
C
P_AC_050404_1_0020001_01_00
Crew Oxygen Storage - Location
FIGURE-5-4-4-991-002-A01
5-4-4
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5
Fuel System
**ON A/C A350-900
Fuel System
1.
Refuel/Defuel Control Panel
ACCESS
AFT OF NOSE
Refuel/Defuel
36.2 m
Control Panel:
(118.77 ft.)
Access Door 197KB
2.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
2.18 m
(7.15 ft.)
On centerline
Refuel/Defuel Connectors
ACCESS
AFT OF NOSE
Refuel/Defuel
Coupling, Left
(Optional):
Access Door 523EB
Refuel/Defuel
Coupling, Right:
Access Door 623EB
A.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
32.57 m
(106.86 ft.)
15.83 m
(51.94 ft.)
-
5.5 m
(18.04 ft.)
32.57 m
(106.86 ft.)
-
15.83 m
(51.94 ft.)
5.5 m
(18.04 ft.)
Refuel/defuel couplings:
(1) Two standard ISO 45, 2.5 in. on right wing.
(2) Two standard ISO 45, 2.5 in. on left wing (optional).
B.
Refuel pressure:
(1) Max. pressure: 3.45 bar (50 psi).
3.
Overpressure Protector and NACA Intake for Vent Tank
ACCESS
Overpressure
Protector
NACA Intake for
Vent Tank
AFT OF NOSE
38.24 m
(125.46 ft.)
38.69 m
(126.94 ft.)
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
22.33 m
22.33 m
(73.26 ft.)
(73.26 ft.)
23.07 m
23.07 m
(75.69 ft.)
(75.69 ft.)
5-4-5
MEAN HEIGHT
FROM GROUND
6.13 m
(20.11 ft.)
6.19 m
(20.31 ft.)
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
Z190
197KB
A
TYPICAL LAYOUT
11QU
A
P_AC_050405_1_0010001_01_01
Refuel/Defuel Control Panel
FIGURE-5-4-5-991-001-A01
5-4-5
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
01
A
523EB
623EB
Z500
Z600
RIB16
RIB15
REFUEL/DEFUEL COUPLING
A
NOTE:
01 LH OPTIONAL
RH SHOWN
LH SYMMETRICAL
P_AC_050405_1_0020002_01_01
Refuel/Defuel Couplings
FIGURE-5-4-5-991-002-B01
5-4-5
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
543DB (643DB)
543CB (643CB)
RIB27
Z500 (Z600)
RIB25
NACA INTAKE
NACA DUCT PANEL
TANK OVERPRESSURE
DISC
OVERPRESSURE PANEL
A
LH SHOWN
RH SYMMETRICAL
P_AC_050405_1_0030001_01_01
Overpressure Protectors and NACA Vent Intake
FIGURE-5-4-5-991-003-A01
5-4-5
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6
Pneumatic System
**ON A/C A350-900
Pneumatic System
1.
Low Pressure Connectors
ACCESS
AFT OF NOSE
Low Pressure
23.58 m
Connector:
(77.36 ft.)
Access Door 193CB
Low Pressure
23.58 m
Connector:
(77.36 ft.)
Access Door 194CR
A.
2.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
-
1.05 m
(3.44 ft.)
2.59 m
(8.5 ft.)
-
1.87 m
(6.14 ft.)
2.87 m
(9.42 ft.)
Connectors : Two standard SAE AS4262 type B, 8 in.
High Pressure Connectors
ACCESS
AFT OF NOSE
High Pressure
26.81 m
Connectors:
(87.96 ft.)
Access Door 193KB
A.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
2.06 m
(6.76 ft.)
On centerline
Connectors: Two standard ISO 2026, 3 in.
5-4-6
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
194CR
A
193CB
Z190
LP CONNECTOR
A
P_AC_050406_1_0010001_01_01
Low Pressure Ground Connectors
FIGURE-5-4-6-991-001-A01
5-4-6
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
193KB
Z190
A
HP CONNECTOR
A
P_AC_050406_1_0020001_01_01
High Pressure Ground Connectors
FIGURE-5-4-6-991-002-A01
5-4-6
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7
Oil System
**ON A/C A350-900
Engine Oil Servicing
1.
Engine Oil Servicing
ACCESS
AFT OF NOSE
24.7 m
Engine 1:
Access Door 415BR (81.04 ft.)
24.7 m
Engine 2:
Access Door 425BR (81.04 ft.)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
8.6 m
(28.22 ft.)
12.29 m
(40.32 ft.)
5-4-7
MEAN HEIGHT
FROM GROUND
3.23 m
(10.6 ft.)
3.23 m
(10.6 ft.)
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
415BR (ENGINE 1)
425BR (ENGINE 2)
A
OIL TANK
OIL LEVEL SIGHT
GLASS
OIL FILLER CAP
A
TYPICAL
P_AC_050407_1_0040001_01_00
Engine Oil Servicing
FIGURE-5-4-7-991-004-A01
5-4-7
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
VFG Oil Servicing
1.
VFG Oil Servicing
ACCESS
Engine 1:
Fan Cowl 415AL
Engine 2:
Fan Cowl 425AL
AFT OF NOSE
24.3 m
(79.72 ft.)
24.3 m
(79.72 ft.)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
11.02 m
(36.15 ft.)
9.86 m
(32.35 ft.)
5-4-7
MEAN HEIGHT
FROM GROUND
1.22 m
(4.0 ft.)
1.22 m
(4.0 ft.)
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
B
B
A
A
DISCONNECT
RESET HANDLE
PRESSURE FILL
C
DRAIN
FILTER BOWL
SIGHT GLASS
OVERFLOW/STANDPIPE
B
C
TYPICAL
P_AC_050407_1_0090001_01_00
VFG Oil Servicing
FIGURE-5-4-7-991-009-A01
5-4-7
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
Starter Oil Servicing
1.
Starter Oil Servicing
ACCESS
Engine 1:
Fan Cowl 415AL
Engine 2:
Fan Cowl 425AL
AFT OF NOSE
24.6 m
(80.71 ft.)
24.6 m
(80.71 ft.)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
10.57 m
(34.68 ft.)
10.31 m
(33.83 ft.)
5-4-7
MEAN HEIGHT
FROM GROUND
1.08 m
(3.54 ft.)
1.08 m
(3.54 ft.)
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
PRESSURE
FILL PORT
PRESSURE SPILL
PORT
OIL DRAIN PLUG/
MAGNETIC CHIP DETECTOR
A
P_AC_050407_1_0100001_01_00
Starter Oil Servicing
FIGURE-5-4-7-991-010-A01
5-4-7
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
APU Oil Servicing
1.
APU Oil Servicing
ACCESS
AFT OF NOSE
62.52 m
APU:
Access Door 316BR (205.12 ft.)
-
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.48 m
(1.57 ft.)
5-4-7
MEAN HEIGHT
FROM GROUND
6.45 m
(21.16 ft.)
Page 7
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
Z310
B
316BR
FR104
A
FILL CAP
PRESSURE
OVERFILL
PORT
C
SIGHT GLASS
PRESSURE FILL
PORT
B
C
FWD
P_AC_050407_1_0110001_01_00
APU Oil Servicing
FIGURE-5-4-7-991-011-A01
5-4-7
Page 8
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8
Potable Water System
**ON A/C A350-900
Potable Water System
1.
Potable Water System
ACCESS
AFT OF NOSE
Potable-Water
50.2 m
Ground Service
(164.7 ft.)
Panel:
Access Door 164AR
2.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
-
1.6 m
(5.25 ft.)
MEAN HEIGHT
FROM GROUND
3.3 m
(10.83 ft.)
Technical Specifications
A.
Connectors:
(1) Fill/drain nipple 3/4 in. (ISO 17775).
B.
Capacity:
(1) Standard configuration - two tanks (530 l (140 USgal) each): 1060 l (280 USgal).
(2) Optional - two tanks (750 l (198 USgal) each): 1500 l (396 USgal).
C.
Filling pressure:
(1)
Max filling pressure: 8.6 bar (125 psi).
5-4-8
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
Z160
FR71
A
164AR
FR84
FR85
FR86
POTABLE WATER
INDICATION PANEL
FILL
STOP
OVERFLOW
NIPPLE
DRAIN
A
FILL/DRAIN PORT
FWD
P_AC_050408_1_0050001_01_00
Potable-Water Ground Service Panel
FIGURE-5-4-8-991-005-A01
5-4-8
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
Z120
FR12
FR13
DRAIN PORT
A
P_AC_050408_1_0060002_01_00
Forward Drain Port
FIGURE-5-4-8-991-006-B01
5-4-8
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
Z170
POTABLE WATER TANKS
FR93
FR89
FR86
A
P_AC_050408_1_0070001_01_00
Potable-Water Tanks Location
FIGURE-5-4-8-991-007-A01
5-4-8
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9
Waste Water System
**ON A/C A350-900
Waste Water System
1.
Waste Water System
ACCESS
AFT OF NOSE
Waste-Water
52.21 m
Ground Service
(171.29 ft.)
Panel:
Access Door 171AL
2.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
3.69 m
(12.11 ft.)
On centerline
Technical Specifications
A.
Connectors:
(1)
Draining - 4 in. (ISO 17775).
(2) Flushing and Filling - 1 in. (ISO 17775).
B.
Usable waste tank capacity:
(1) Two tanks (595 l (157 USgal) each): 1190 l (314 USgal).
C.
Waste tank - Rinsing:
(1) Operating pressure: 3.45 bar (50 psi).
D.
Waste tank - Precharge:
(1) Precharge per tank (two tanks): 23 l (6 USgal).
5-4-9
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
WASTE DRAIN
CONNECTION
FILL AND RINSE
CONNECTION
CONTROL
LEVER
P_AC_050409_1_0010001_01_00
Waste-Water Ground Service Panel
FIGURE-5-4-9-991-001-A01
5-4-9
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
Z170
FR93
FR89
FR86
WASTE TANK
A
P_AC_050409_1_0020001_01_00
Waste Tanks Location
FIGURE-5-4-9-991-002-A01
5-4-9
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10
Cargo Control Panels
**ON A/C A350-900
Cargo Control Panels
1.
Cargo Control Panels
DISTANCE
ACCESS
FWD Cargo Door
Control Panel:
Access Door 132AR
FWD CLS* Panel:
Access Door 132BR
AFT Cargo Door
Control Panel:
Access Door 152AR
AFT CLS* Panel:
Access Door 152BR
AFT OF NOSE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
9.59 m
(31.46 ft.)
2.48 m
(8.14 ft.)
3.87 m
(12.7 ft.)
9.59 m
(31.46 ft.)
2.77 m
(9.09 ft.)
4.50 m
(14.76 ft.)
45.18 m
(148.23 ft.)
2.46 m
(8.07 ft.)
3.80 m
(12.47 ft.)
45.37 m
(148.85 ft.)
2.84 m
(9.32 ft.)
4.71 m
(15.45 ft.)
NOTE : * CLS - CARGO LOADING SYSTEMS
5-4-10
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
A
FR22
FR21
Z130
B
C
FWD CARGO
DOOR
PWR ON/OFF
SWITCH
SYST ON
LAMP
132BR
A
132AR
INDICATOR LIGHT
"CARGO DOOR
FULLY OPEN AND
ARRESTED"
TOGGLE SWITCH
OPEN OR CLOSE
CARGO DOOR
JOYSTICK
B
01
MANUAL
OPERATING
DEVICE
FWD
C
NOTE:
01 OUTSIDE CARGO LOADING SYSTEM CONTROL PANEL
02
02
FWD
CARGO DOOR CONTROL PANEL
P_AC_050410_1_0030001_01_00
Forward Cargo Control Panels
FIGURE-5-4-10-991-003-A01
5-4-10
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
FR77
FR76
A
AFT CARGO DOOR
B
Z150
PWR ON/OFF
SWITCH
SYST ON
LAMP
C
A
152BR
152AR
INDICATOR LIGHT
"CARGO DOOR
FULLY OPEN AND
ARRESTED"
TOGGLE SWITCH
OPEN OR CLOSE
CARGO DOOR
JOYSTICK
B
01
MANUAL
OPERATING
DEVICE
FWD
C
NOTE:
01 OUTSIDE CARGO LOADING SYSTEM CONTROL PANEL
02
02
FWD
CARGO DOOR CONTROL PANEL
P_AC_050410_1_0040001_01_00
Aft Cargo Control Panels
FIGURE-5-4-10-991-004-A01
5-4-10
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0
Engine Starting Pneumatic Requirements
**ON A/C A350-900
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 90 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 the requirements below, the configuration with two HPGC is used. Using one connector only
(for a given mass flow rate and discharge pressure from the ASU) will increase the pressure loss
in the ducts of the bleed system and therefore lower the performances at the engine starter.
C.
For a given OAT the following charts are used to determine an acceptable combination for air
data: discharge temperature, absolute discharge pressure and mass flow rate at the HPGC.
D.
This section is addressing requirements for the ASU only, and is not representative of the start
performance of the aircraft using the APU or engine cross bleed procedure.
E.
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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
ROLLS ROYCE TRENT 1000/SEA LEVEL
STARTING TIME: LESS THAN 90 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
180
390
170
AIRFLOW (kg/min)
350
150
330
140
310
130
290
120
270
110
250
230
100
ABSOLUTE PRESSURE (psia)
90
AIRFLOW (lb/min)
370
160
210
40
45
50
ABSOLUTE PRESSURE (psia)
55
55
50
45
ASU DISCHARGE TEMPERATURE:
70° C (158° F)
140° C (284° F)
260° C (500° F) MAX
40
35
−45
−35
−25 −15 −5
5
15
25
35
45
OUTSIDE AIR TEMPERATURE OAT (° C)
55
−40 −20
0
20
40
60
80
100 120
OUTSIDE AIR TEMPERATURE OAT (° F)
EXAMPLE:
FOR AN OAT OF 15° C (59° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 260° C (500° F)
AT HPGC:
− THE REQUIRED PRESSURE AT HPGC IS 41 psia
− THE REQUIRED AIRFLOW AT HPGC IS 102 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.
EXAMPLE:
FOR AN OAT OF 15° C (59° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 200° C (392° F)
AT HPGC, INTERPOLATING BETWEEN THE LINES 140° C (284° F) AND 260° C (500° F) RESULTS IN:
− A REQUIRED PRESSURE AT HPGC OF 42.5 psia
− A REQUIRED AIRFLOW AT HPGC OF 114 kg/min.
P_AC_050500_1_0010001_01_00
Example for Use of the Charts
FIGURE-5-5-0-991-001-A01
5-5-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
ROLLS ROYCE TRENT 1000/SEA LEVEL
STARTING TIME: LESS THAN 90 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
180
390
170
AIRFLOW (kg/min)
350
150
330
140
310
130
290
120
270
110
250
230
100
90
AIRFLOW (lb/min)
370
160
210
45
40
50
55
ABSOLUTE PRESSURE (psia)
ABSOLUTE PRESSURE (psia)
55
50
45
40
35
−45
−35
−25
−15
−5
5
15
25
35
45
55
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
120
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
70° C (158° F)
140° C (284° F)
260° C (500° F) MAX
P_AC_050500_1_0020001_01_00
Engine Starting Pneumatic Requirements
FIGURE-5-5-0-991-002-A01
5-5-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0
Ground Pneumatic Power Requirements
**ON A/C A350-900
Ground Pneumatic Power Requirements
1.
General
This section describes the required performance for the ground equipment to maintain the cabin
temperature at 27 deg.C (80.6 deg.F) for the cooling or 21 deg.C (69.8 deg.F) for the heating cases
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
GC
GSE
IFE
LP
OAT
PCA
A.
DEFINITION
Aircraft
Aircraft Handling Manual
Ground Connection
Ground Service Equipment
In-Flight Entertainment
Low Pressure
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.
B.
The air flow rates and temperature requirements for the GSE are given for the A/C in the
configuration ”2 LP ducts connected”.
NOTE : The maximum air flow is driven by Pressure limitation at ground connection.
C.
2.
For temperature at ground connection below 2 deg.C (35.6 deg.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:
5-6-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
-
Heating (pull up) the cabin, initially at OAT, up to 21 deg.C (69.8 deg.F) (FIGURE
5-6-0-991-001-A --- Sheet 1).
Cooling (pull down) the cabin, initially at OAT, down to 27 deg.C (80.6 deg.F) (FIGURE
5-6-0-991-001-A --- Sheet 2).
5-6-0
Page 2
Apr 01/15
AIR FLOW AT GC (kg/s)
2.5
2.7
2.9
3.1
3.3
3.5
3.7
3.9
4.1
4.3
4.5
5-6-0
35
40
45
50
55
TIME TO HEAT CABIN TO +21°C (+69.8°F) ON GROUND (min)
60
65
PU1 "ISA −38°C (−36.4°F )"
PU2 "ISA −45°C (−49°F )"
PU1: OAT ISA −38°C (−36.4°F); GC OUTLET +70°C (+158°F); A/C EMPTY; IFE OFF; NO SOLAR LOAD; LIGHTS ON;
RECIRCULATION FANS ON
PU2: OAT ISA −45°C (−49°F); GC OUTLET +70°C (+158°F); A/C EMPTY; IFE OFF; NO SOLAR LOAD; LIGHTS ON;
RECIRCULATION FANS ON
PULL UP CASES:
30
MAX AIR FLOW
PULL UP PERFORMANCE (+70°C (+158°F) GC OUTLET)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_050600_1_0010001_01_02
Ground Pneumatic Power Requirements
Heating (Sheet 1 of 2)
FIGURE-5-6-0-991-001-A01
Page 3
Apr 01/15
AIR FLOW AT GC (kg/s)
2.5
2.7
2.9
3.1
3.3
3.5
3.7
3.9
4.1
4.3
4.5
20
5-6-0
30
40
50
60
70
TIME TO COOL CABIN TO +27°C (+80.6°F) ON GROUND (min)
PD1 "ISA +23°C (+73.4°F) / GC OUTLET +2°C (+35.6°F)"
PD2 "ISA +23°C (+73.4°F) / GC OUTLET −10°C (+14°F)"
PD3 "ISA +23°C (+73.4°F) / GC OUTLET −20°C (−4°F)"
PD1: OAT ISA +23°C (+73.4°F); GC OUTLET + 2°C (+35.6°F); A/C EMPTY; IFE OFF; SOLAR LOAD; LIGHTS ON;
RECIRCULATION FANS ON
PD2: OAT ISA +23°C (+73.4°F); GC OUTLET −10°C (+14°F); A/C EMPTY; IFE OFF; SOLAR LOAD; LIGHTS ON;
RECIRCULATION FANS ON
PD3: OAT ISA +23°C (+73.4°F); GC OUTLET −20°C (−4°F); A/C EMPTY; IFE OFF; SOLAR LOAD; LIGHTS ON;
RECIRCULATION FANS ON
PULL DOWN CASES:
10
MAX AIR FLOW
PULL DOWN PERFORMANCE
80
90
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_050600_1_0010001_02_01
Ground Pneumatic Power Requirements
Cooling (Sheet 2 of 2)
FIGURE-5-6-0-991-001-A01
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0
Preconditioned Airflow Requirements
**ON A/C A350-900
Preconditioned Airflow Requirements
1.
This section provides the necessary information for the design of a ground unit; it gives the air flow
rate and temperature combinations needed to maintain the cabin temperature at 27 deg.C (80.6
deg.F).
These settings are not intended to be used for operation (they don’t substitute to the settings given
in the AMM):
They are issued from theoretical simulations and give the picture of a real steady state.
For the air conditioning operation, Airlines will refer to the AMM that details the procedure and the
PCA settings to maintain the cabin temperature below 27 deg.C (80.6 deg.F) during boarding
(therefore it is not a steady state).
5-7-0
Page 1
Apr 01/15
5-7-0
−10
C2
C1
−5
C3
0
5
10
MAX AIR FLOW
15
20
25
30
GC OUTLET TEMPERATURE (°C)
35
40
H1
45
H2
50
OAT ISA−38°C (−36.4°F); A/C EMPTY; IFE OFF; NO SOLAR LOAD; LIGHTS ON; RECIRCULATION FANS ON
OAT ISA−45°C (−49°F); A/C EMPTY; IFE OFF; NO SOLAR LOAD; LIGHTS ON; RECIRCULATION FANS ON
OAT ISA−55°C (−67°F); A/C EMPTY; IFE OFF; NO SOLAR LOAD; LIGHTS ON; RECIRCULATION FANS ON
OAT ISA+30°C (86°F); 446 PASSENGERS AND CREW; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON
OAT ISA+23°C (73.4°F); 446 PASSENGERS AND CREW; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON
OAT ISA; 446 PASSENGERS AND CREW; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON
1,8
2,3
2,8
3,3
3,8
4,3
COOLING/HEATING PERFORMANCE
EXAMPLE:
COOLING CAPACITY CALCULATION:
FOR THE CONDITIONS C3, THE COOLING CAPACITY OF 4.25 kg/s x 1kJ/(kg.°C) X (27−2) = 106 kW IS NEEDED
TO MAINTAIN THE CABIN TEMPERATURE BELOW 27°C (86°F) (4.25 kg/s AT GC OUTLET OF 2°C (35.6°F)).
AIRFLOW FROM GC (kg/s)
4,8
H3
55
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_050700_1_0010001_01_01
Preconditioned Airflow Requirements
FIGURE-5-7-0-991-001-A01
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0
Ground Towing Requirements
**ON A/C A350-900
Ground Towing Requirements
1.
This section provides information on aircraft towing.
The A350 is designed with means for conventional or towbarless towing. Information/procedures can
be found in chapter 9 of the Aircraft Maintenance Manual.
Status on towbarless towing equipment qualification can be found in ISI 09.11.00001.
It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idle
thrust, using a towbar attached to the NLG.
One towbar fitting is installed at the front of the leg (optional towing fitting for towing from the rear
of the NLG available).
The main landing gears have attachment points for towing or debogging (for details, ARM 7).
This section shows the chart to determine the drawbar pull and tow tractor mass requirements as a
function of the following physical characteristics:
- Aircraft weight,
- Number of engines at idle,
- Slope.
2.
Towbar design guidelines
The A350 towbar requirements are identical to the towbar requirements of the long range aircraft.
- ISO 8267-1, ”Aircraft - Towbar Attachment Fitting - Interface Requirements - Part 1: Main Line
Aircraft”,
- ISO 9667, ”Aircraft Ground Support Equipment - Towbars”,
- 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 NLG against jerks) and with towing shear pins:
- A traction shear pin calibrated at 28 620 daN (64 340 lbf),
- A torsion pin calibrated at 3 130 m.daN (27 7028 lbf.in).
The towing head is designed according to ISO 8267--1, cat. III.
5-8-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
DRAWBAR PULL ( x 1000 kg )
25
=0
.8
BREAKWAY RESISTANCE 4%
# OF ENGINES ON FOR PB: 1
ENGINE THRUST 811 daN
17.0
15
D
AR
280
2% SLOPE
1 ENGINE ON
250
255
230
205
.2
=0
180
155
W
O
SN
130
H
WE
10
DR
YC
ON
CR
ETE
TC
ON
CR
ET
E
=0
.57
20
A/C WEIGHT ( x 1000 kg )
5
ICE
= 0.05
29.8
0
0
10
20
30
40
50
60
70
80
TOTAL TRACTION WHEEL LOAD ( x 1000 kg )
0
1
2
No. OF ENGINES
AT IDLE
0
0.5
1.0
1.5
2.0
SLOPE ( % )
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A350 AT 250 000 kg, AT 2% SLOPE,
1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
−
−
−
−
−
−
−
ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (250 000 kg),
FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (2%),
FROM THIS POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 2,
FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER 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 (17 000 kg),
SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE.
THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (29 800 kg).
P_AC_050800_1_0010001_01_00
Ground Towing Requirements
FIGURE-5-8-0-991-001-A01
5-8-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0
De-icing and External cleaning
**ON A/C A350-900
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 17 m (56 ft.).
2.
De-Icing
Wing Top Surface
(Both Sides)
AIRCRAFT TYPE
354 m2
(3810 ft.2)
A350--900
AIRCRAFT TYPE
A350--900
Wingtip Devices
HTP Top Surface
(Both Inside and
(Both Sides)
(Outside Surfaces)
(Both Sides)
25 m2
69 m2
(269 ft.2)
(743 ft.2)
Fuselage Top Surface
(Top Third - 120? Arc)
357 m2
(3843 ft.2)
VTP
(Both Sides)
102 m2
(1098 ft.2)
Nacelle and Pylon
Total De-Iced Area
(Top Third - 120? Arc)
(All Engines)
56 m2
962 m2
(603 ft.2)
(10355 ft.2)
NOTE : Dimensions are approximate
3.
External Cleaning
Wing Top
Surface
(Both Sides)
AIRCRAFT
TYPE
A350--900
354 m2
(3810 ft.2)
AIRCRAFT TYPE
A350--900
Wing Lower
Wingtip Devices
HTP Top
Surface
(Both Inside
Surface
(Including Flap
and
(Both Sides)
Track Fairing)
(Outside
(Both Sides)
Surfaces)
(Both Sides)
384 m2
25 m2
69 m2
(4133 ft.2)
(269 ft.2)
(743 ft.2)
VTP
(Both Sides)
102 m2
(1098 ft.2)
Fuselage and
Belly Fairing
1073 m2
(11550 ft.2)
HTP Lower
Surface
(Both Sides)
69 m2
(743 ft.2)
Nacelle and Pylon Total Cleaned Area
(All Engines)
166 m2
2242 m2
(1787 ft.2)
(24133 ft.2)
NOTE : Dimensions are approximate
5-9-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0
Engine Exhaust Velocities and Temperatures
**ON A/C A350-900
Engine Exhaust Velocities and Temperatures
1.
General
This section provides the estimated engine exhaust-efflux velocity and temperature contours for
Maximum Take-Off (MTO), Breakaway 11% MTO, Breakaway 22% MTO and Ground Idle
conditions for the A350 engines.
The contours are available for the Rolls-Royce Trent XWB-84 engine.
The Maximum Take-Off data are presented at the maximum thrust rating.
The Breakaway data are presented at a rating that corresponds to the minimum thrust level
necessary to start the movement of the A350-900 at its maximum ramp weight, from a static
position or when on an uphill surface with a slope of 1.5%. Breakaway thrust corresponds to 11%
MTO when applied on both engines and 22% MTO when applied on a single engine (Idle thrust on
the other engine).
The Idle data are directly provided by the engine manufacturer.
In the charts, the longitudinal distances are measured from the inboard engine core-nozzle exit
section. The lateral distances are measured from the aircraft fuselage centerline.
The estimated efflux data are shown at ISA +15K (+15˚C), Sea Level Static and no headwind
conditions.
The analysis assumes that the core and the bypass streams are fully mixed by the nozzle exit plane.
The effects of on-wing installation or ground proximity are not taken into account and the ambient
air is assumed to be still.
The velocity contours are presented at 50 ft/s (15 m/s), 100 ft/s (30 m/s) and 150 ft/s (46 m/s).
The temperature contours are shown at ambient temperature +10K (+10˚C), ambient temperature
+20K (+20˚C) and ambient temperature +30K (+30˚C).
In the case of the velocity contours for the Maximum Take-Off operating condition, there is some
coalescence of the jet plumes from the port and starboard engines, hence the contours are presented
with both a plan view and a side view for twin-engine operation.
An axisymmetric view is also provided for this case, to be applied only for single engine operation. For
the other figures, there is no interference between the two engine plumes in the operating conditions
studied and hence the efflux can be adequately described by the axisymmetric contours of a single
plume.
6-1-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1
Engine Exhaust Velocities - Ground Idle Power
**ON A/C A350-900
Engine Exhaust Velocities - Ground Idle Power
1.
This section provides engine exhaust velocities at ground idle power.
6-1-1
Page 1
Apr 01/15
RADIAL CO−ORDINATE (ft)
−100
−80
−60
−40
−20
0
20
40
0
6-1-1
40
60
80
100
120
AXIAL CO−ORDINATE (ft)
140
160
180
200
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX VELOCITY CONTOURS
AT GROUND IDLE AXISYMMETRIC VIEW
20
ICN−TRENTXWB−A−710000−R−K0680−02140−A−001−01
220
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060101_1_0020001_01_00
Ground Idle Power - TRENT XWB Engine
FIGURE-6-1-1-991-002-A01
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2
Engine Exhaust Temperatures - Ground Idle Power
**ON A/C A350-900
Engine Exhaust Temperatures - Ground Idle Power
1.
This section provides engine exhaust temperatures at ground idle power.
6-1-2
Page 1
Apr 01/15
−40
0
40
6-1-2
20
40
60
100
120
AXIAL CO−ORDINATE (ft)
80
Tamb +10K
140
160
180
200
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS
AT GROUND IDLE SIDE VIEW
0
Tamb +30K Tamb +20K
ICN−TRENTXWB−A−710000−R−K0680−02294−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060102_1_0010001_01_00
Ground Idle Power - TRENT XWB-84 Engine
(Sheet 1 of 2)
FIGURE-6-1-2-991-001-A01
Page 2
Apr 01/15
VERTICAL CO−ORDINATE (ft)
RADIAL CO−ORDINATE (ft)
6-1-2
0
20
40
80
100
AXIAL CO−ORDINATE (ft)
60
ICN−TRENTXWB−A−710000−R−K0680−02141−A−001−01
120
140
160
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS
AT GROUND IDLE AXISYMMETRIC VIEW
−100
−80
−60
−40
−20
0
20
40
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060102_1_0010001_02_00
Ground Idle Power - TRENT XWB-84 Engine
(Sheet 2 of 2)
FIGURE-6-1-2-991-001-A01
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3
Engine Exhaust Velocities - Breakaway Power
**ON A/C A350-900
Engine Exhaust Velocities - Breakaway Power
1.
This section provides engine exhaust velocities at breakaway power.
6-1-3
Page 1
Apr 01/15
−100
−80
−60
−40
−20
0
20
40
6-1-3
20
40
60
50 ft/sec
AXIAL CO−ORDINATE (ft)
80 100 120 140 160 180 200 220 240 260 280 300 320 340 360 380 400
100 ft/sec
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX VELOCITY CONTOURS
AT 11% MTO THRUST AXISYMMETRIC VIEW
0
150 ft/sec
ICN−TRENTXWB−A−710000−R−K0680−02138−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060103_1_0010001_01_00
Breakaway Power (11% MTO Thrust) - TRENT XWB-84 Engine
FIGURE-6-1-3-991-001-A01
Page 2
Apr 01/15
RADIAL CO−ORDINATE (ft)
−100
−80
−60
−40
−20
0
20
40
0
200
100 ft/sec
300
AXIAL CO−ORDINATE (ft)
50 ft/sec
400
500
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX VELOCITY CONTOURS AT
22% MTO THRUST AXISYMMETRIC VIEW
100
150 ft/sec
ICN−TRENTXWB−A−710000−R−K0680−02136−A−001−01
600
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060103_1_0020001_01_00
Breakaway Power (22% MTO Thrust) - TRENT XWB-84 Engine
FIGURE-6-1-3-991-002-A01
6-1-3
Page 3
Apr 01/15
RADIAL CO−ORDINATE (ft)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4
Engine Exhaust Temperatures - Breakaway Power
**ON A/C A350-900
Engine Exhaust Temperatures - Breakaway Power
1.
This section provides engine exhaust temperatures at breakaway power.
6-1-4
Page 1
Apr 01/15
6-1-4
−40
0
40
20
40
60
100
120
AXIAL CO−ORDINATE (ft)
80
Tamb +10K
140
160
180
200
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS
AT 11% MTO THRUST SIDE VIEW
0
Tamb +30K Tamb +20K
ICN−TRENTXWB−A−710000−R−K0680−02292−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060104_1_0010001_01_00
Breakaway Power (11% MTO Thrust) - TRENT XWB-84 Engine
(Sheet 1 of 2)
FIGURE-6-1-4-991-001-A01
Page 2
Apr 01/15
VERTICAL CO−ORDINATE (ft)
RADIAL CO−ORDINATE (ft)
−100
−80
−60
−40
−20
0
20
40
6-1-4
20
40
60
100
120
AXIAL CO−ORDINATE (ft)
80
Tamb +10K
140
160
180
200
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS
AT 11% MTO THRUST AXISYMMETRIC VIEW
0
Tamb +30K Tamb +20K
ICN−TRENTXWB−A−710000−R−K0680−02139−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060104_1_0010001_02_00
Breakaway Power (11% MTO Thrust) - TRENT XWB-84 Engine
(Sheet 2 of 2)
FIGURE-6-1-4-991-001-A01
Page 3
Apr 01/15
−40
0
40
6-1-4
20
40
60
100
120
AXIAL CO−ORDINATE (ft)
80
Tamb +10K
140
160
180
200
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS
AT 22% MTO THRUST SIDE VIEW
0
Tamb +30K Tamb +20K
ICN−TRENTXWB−A−710000−R−K0680−02290−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060104_1_0020001_01_00
Breakaway Power (22% MTO Thrust) - TRENT XWB-84 Engine
(Sheet 1 of 2)
FIGURE-6-1-4-991-002-A01
Page 4
Apr 01/15
VERTICAL CO−ORDINATE (ft)
RADIAL CO−ORDINATE (ft)
−100
−80
−60
−40
−20
0
20
40
6-1-4
20
40
60
100
120
AXIAL CO−ORDINATE (ft)
80
Tamb +10K
140
160
180
200
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS
AT 22% MTO THRUST AXISYMMETRIC VIEW
0
Tamb +30K Tamb +20K
ICN−TRENTXWB−A−710000−R−K0680−02137−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_060104_1_0020001_02_00
Breakaway Power (22% MTO Thrust) - TRENT XWB-84 Engine
(Sheet 2 of 2)
FIGURE-6-1-4-991-002-A01
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5
Engine Exhaust Velocities - Max Take-Off Power
**ON A/C A350-900
Engine Exhaust Velocities - Max Take-Off Power
1.
This section provides engine exhaust velocities at max take-off power.
6-1-5
Page 1
Apr 01/15
−100
0
100
0
400
100 ft/sec
800
AXIAL CO−ORDINATE (ft)
600
50 ft/sec
1000
1200
1400
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX VELOCITY CONTOURS AT MTO
AXISYMMETRIC VIEW FOR SINGLE ENGINE OPERATION
200
150 ft/sec
ICN−TRENTXWB−A−710000−R−K0680−02134−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RADIAL CO−ORDINATE (ft)
P_AC_060105_1_0030001_01_00
Max Take-Off Power - TRENT XWB-84 Engine (Single)
FIGURE-6-1-5-991-003-A01
6-1-5
Page 2
Apr 01/15
−40
0
40
0
400
100 ft/sec
800
AXIAL CO−ORDINATE (ft)
600
50 ft/sec
1000
1200
1400
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX VELOCITY CONTOURS AT MTO
SIDE VIEW FOR TWIN−ENGINE OPERATION
200
150 ft/sec
ICN−TRENTXWB−A−710000−R−K0680−02133−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
6-1-5
VERTICAL CO−ORDINATE (ft)
P_AC_060105_1_0040001_01_00
Max Take-Off Power - TRENT XWB-84 Engine (Twin)
(Sheet 1 of 2)
FIGURE-6-1-5-991-004-A01
Page 3
Apr 01/15
−100
0
100
0
400
800
AXIAL CO−ORDINATE (ft)
600
1000
1200
1400
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX VELOCITY CONTOURS AT MTO
PLAN VIEW FOR TWIN − ENGINE OPERATION
200
ICN−TRENTXWB−A−710000−R−K0680−02132−A−001−01
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
LATERAL CO−ORDINATE (ft)
P_AC_060105_1_0040001_02_00
Max Take-Off Power - TRENT XWB-84 Engine (Twin)
(Sheet 2 of 2)
FIGURE-6-1-5-991-004-A01
6-1-5
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6
Engine Exhaust Temperatures - Max Take-Off Power
**ON A/C A350-900
Engine Exhaust Temperatures - Max Take-Off Power
1.
This section provides engine exhaust temperatures at max take-off power.
6-1-6
Page 1
Apr 01/15
−40
0
40
0
6-1-6
300
AXIAL CO−ORDINATE (ft)
200
Tamb +10K
400
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS AT MTO
SIDE VIEW
100
Tamb +30K Tamb +20K
ICN−TRENTXWB−A−710000−R−K0680−02288−A−001−01
500
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
VERTICAL CO−ORDINATE (ft)
P_AC_060106_1_0030001_01_00
Max Take-Off Power - TRENT XWB-84 Engine
(Sheet 1 of 2)
FIGURE-6-1-6-991-003-A01
Page 2
Apr 01/15
−100
−80
−60
−40
−20
0
20
40
0
6-1-6
300
AXIAL CO−ORDINATE (ft)
200
Tamb +10K
400
TRENT XWB 84000 lbf THRUST ENGINE − ESTIMATED EXHAUST EFFLUX TEMPERATURE CONTOURS AT MTO
AXISYMMETRIC VIEW
100
Tamb +30K Tamb +20K
ICN−TRENTXWB−A−710000−R−K0680−02135−A−001−01
500
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
RADIAL CO−ORDINATE (ft)
P_AC_060106_1_0030001_02_00
Max Take-Off Power - TRENT XWB-84 Engine
(Sheet 2 of 2)
FIGURE-6-1-6-991-003-A01
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1
Danger Areas of the Engines - Ground Idle Power
**ON A/C A350-900
Danger Areas of the Engines - Ground Idle Power
1.
This section provides danger areas of the engines at ground idle power conditions.
6-3-1
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
R 4.6 m
(15 ft)
1.6 m
(5 ft)
45°
UPTO 67 m (220 ft) AFT OF EXHAUST NOZZLES
30°
INTAKE SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST DANGER AREA
P_AC_060301_1_0010001_01_00
Ground Idle Power - TRENT XWB-84 Engine
FIGURE-6-3-1-991-001-A01
6-3-1
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-3
Danger Areas of the Engines - Max Take-Off Power
**ON A/C A350-900
Danger Areas of the Engines - Max Take-Off Power
1.
This section provides danger areas of the engines at max take-off power conditions.
6-3-3
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
R 9.1 m
(30 ft)
UPTO 442 m (1 450 ft) AFT OF EXHAUST NOZZLES
30°
INTAKE SUCTION DANGER AREA
EXHAUST DANGER AREA
P_AC_060303_1_0010001_01_00
Max Take-Off Power - TRENT XWB-84 Engine
FIGURE-6-3-3-991-001-A01
6-3-3
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0
APU Exhaust Velocities and Temperatures
**ON A/C A350-900
APU Exhaust Velocities and Temperatures
1.
This section gives APU exhaust velocities and temperatures.
6-4-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
[m]
[ft]
40
15 m/s
10
46 m/s 30.5 m/s
61 m/s
30
20
FD
5
10
[m]
[ft]
0
0
5
0
10
10
20
30
15
40
50
0
20
60
[m]
[ft]
40
93°C
427°C
FD
10
315.5°C
204°C
20
149°C
5
260°C
[m]
[ft]
10
0
0
0
5
10
10
20
30
30
15
40
50
0
20
60
P_AC_060400_1_0010001_01_00
APU Exhaust Velocities and Temperatures
FIGURE-6-4-0-991-001-A01
6-4-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0
General Information
**ON A/C A350-900
General Information
1.
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 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 7-2-0 presents basic data on the landing gear footprint configuration, MRW and tire sizes and
pressures.
Maximum Pavement Loads:
Section 7-3-0 shows maximum vertical and horizontal pavement loads for certain critical conditions at
the tire-ground interfaces.
Landing Gear Loading on Pavement:
Section 7-4-0 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 7-5-0 uses the procedures in Instruction Report No S-77-1 ”Procedures for Development of
CBR Design Curves”, dated June 1977 and 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 the 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 Aircraft Classification Number (ACN).
Flexible Pavement Requirements - LCN Conversion Method:
7-1-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The Load Classification Number (LCN) curves are no longer provided in section 7-6-0 since the LCN
system for reporting pavement strength is obsolete, having been replaced by the ICAO recommended
ACN/PCN system in 1983.
For questions regarding the LCN system, contact Airbus.
Rigid Pavement Requirements - PCA (Portland Cement Association) Design Method:
Section 7-7-0 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:
The Load Classification Number (LCN) curves are no longer provided in section 7-8-0 since the LCN
system for reporting pavement strength is obsolete, having been replaced by the ICAO recommended
ACN/PCN system in 1983.
For questions regarding the LCN system, contact Airbus.
ACN/PCN Reporting System:
Section 7-9-0 provides ACN data prepared according to the ACN/PCN system as referred to 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 with 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.
Computationally, the ACN/PCN system uses the 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
SUBGRADE
TIRE PRESSURE
EVALUATION
PAVEMENT TYPE
CATEGORY
CATEGORY
METHOD
R - Rigid
A - High
W - No pressure limit
T - Technical
F - Flexible
B - Medium
X - High pressure limited U - Using Aircraft
to 1.75 MPa (254 psi)
7-1-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PCN
PAVEMENT TYPE
SUBGRADE
CATEGORY
C - Low
D - Ultra Low
TIRE PRESSURE
CATEGORY
Y - Medium pressure
limited to 1.25 MPa (181
psi)
Z - Low pressure limited
to 0.5 MPa (73 psi)
EVALUATION
METHOD
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
k
k
k
=
=
=
=
150 MN/m 3 (550 pci)
80 MN/m 3 (300 pci)
40 MN/m 3 (150 pci)
20 MN/m 3 (75 pci)
7-1-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0
Landing Gear Footprint
**ON A/C A350-900
Landing Gear Footprint
1.
This section provides data about the landing gear footprint in relation with 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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
28.665 m
(94.045 ft)
10.600 m
(34.777 ft)
0.748 m
(2.454 ft)
1.735 m
(5.692 ft)
2.040 m
(6.693 ft)
WEIGHT
VARIANT
MAXIMUM
RAMP
WEIGHT
A350−900 268 900 kg
(592 825 lb)
WV000
A350−900 275 900 kg
(608 250 lb)
WV001
A350−900 272 900 kg
(601 650 lb)
WV002
PERCENTAGE
OF WEIGHT
ON MAIN
GEAR GROUP
NOSE GEAR TIRE
SIZE
NOSE GEAR
TIRE
PRESSURE
WING GEAR TIRE
SIZE
WING GEAR
TIRE
PRESSURE
93.7%
1050x395R16 28PR
12.2 bar
(177 psi)
1400x530R23 42PR
16.6 bar
(241 psi)
93.7%
1050x395R16 28PR
12.2 bar
(177 psi)
1400x530R23 42PR
16.8 bar
(244 psi)
94.8%
1050x395R16 28PR
12.2 bar
(177 psi)
1400x530R23 42PR
16.6 bar
(241 psi)
P_AC_070200_1_0010001_01_02
Landing Gear Footprint
FIGURE-7-2-0-991-001-A01
7-2-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0
Maximum Pavement Loads
**ON A/C A350-900
Maximum Pavement Loads
1.
This section provides 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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
H
V
V
(MG)
(NG)
V
(NG)
MAXIMUM VERTICAL NOSE GEAR GROUND LOAD AT FORWARD CG
V
MAXIMUM VERTICAL MAIN GEAR GROUND LOAD AT AFT CG
(MG)
H
1
MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING
2
3
4
V
(NG)
MAXIMUM
WEIGHT
RAMP
VARIANT WEIGHT
STATIC LOAD
AT
FWD CG
STATIC
BRAKING
AT 10 ft/s²
DECELERATION
5
V
(MG)
(PER STRUT)
STATIC LOAD
AT
AFT CG
6
H (PER STRUT)
AT
STEADY
BRAKING
INSTANTANEOUS
AT 10 ft/s²
BRAKING
DECELERATION COEFFICIENT = 0.8
23.4 %
A350−900 268 900 kg 23 450 kg MAC
WV000 (592 825 lb) (51 700 lb) (b)
37 500 kg
(82 675 lb)
125 960 kg 33 %
MAC
(277 700 lb) (a)
41 790 kg
(c)
(92 125 lb)
100 770 kg
(c)
(222 150 lb)
23.4 %
A350−900 275 900 kg 23 450 kg MAC
WV001 (608 250 lb) (51 700 lb) (b)
37 500 kg
(82 675 lb)
129 330 kg 33.2 % 42 880 kg
MAC
(c)
(285 125 lb) (a)
(94 525 lb)
103 460 kg
(c)
(228 100 lb)
%
A350−900 272 900 kg 23 450 kg 23.4
MAC
WV002 (601 650 lb) (51 700 lb) (b)
37 500 kg
(82 675 lb)
129 310 kg 36.39 % 42 410 kg
MAC
(c)
(285 075 lb) (a)
(93 500 lb)
103 450 kg
(c)
(228 075 lb)
NOTE:
(a) LOADS CALCULATED USING AIRCRAFT AT MRW
(b) LOADS CALCULATED USING AIRCRAFT AT 250 200 kg (551 600 lb)
(c) BRAKED MAIN GEAR
P_AC_070300_1_0010001_01_02
Maximum Pavement Loads
FIGURE-7-3-0-991-001-A01
7-3-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0
Landing Gear Loading on Pavement
**ON A/C A350-900
Landing Gear Loading on Pavement
1.
This section provides 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 and standard tire pressure) the lowest ACN (and LCN) and the highest ACN
(and LCN) for each type of aircraft.
Example, see FIGURE 7-4-0-991-001-A, calculation of the total weight on the MLG for:
- An aircraft with a MRW of 268 900 kg (592 825 lb),
- The aircraft gross weight is 210 000 kg (462 975 lb),
- A percentage of weight on the MLG of 93.68 % (percentage of weight on the MLG at MRW and
maximum aft CG).
The total weight on the MLG group is 196 730 kg (433 725 lb).
NOTE : The CG in the figure title is the CG used for ACN/LCN calculation.
7-4-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
300
300
MTOW − 268 000 kg
290
25.46% MAC
280
270
260
260
250
250
240
240
230
230
MLW
210
200
200
190
190
180
180
170
170
160
160
450
400
350
150
MZFW
TAKE OFF
140
500
220
210
150
550
(x 1 000 lb)
220
600
AIRCRAFT GROSS WEIGHT
270
(x 1 000 kg)
280
WEIGHT ON MAIN LANDING GEAR (x 1 000 kg)
650
CG FOR ACN/LCN
CALCULATION
33% MAC
290
140
300
LANDING
130
130
120
120
84
86
88
90
92
94
96
98
PERCENTAGE OF WEIGHT ON MAIN GEAR
100
P_AC_070400_1_0010001_01_01
Landing Gear Loading on Pavement
WV000, MRW 268 900 kg, CG 33%
FIGURE-7-4-0-991-001-A01
7-4-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
300
300
MTOW − 275 000 kg
290
26.2% MAC
280
270
260
260
250
250
240
240
230
230
MLW
550
500
220
210
210
200
200
190
190
180
180
170
170
160
160
MZFW
150
450
(x 1 000 lb)
220
600
AIRCRAFT GROSS WEIGHT
270
(x 1 000 kg)
280
WEIGHT ON MAIN LANDING GEAR (x 1 000 kg)
650
CG FOR ACN/LCN
CALCULATION
33.2% MAC
290
400
350
150
TAKE OFF
140
140
300
LANDING
130
130
120
120
84
86
88
90
92
94
96
98
PERCENTAGE OF WEIGHT ON MAIN GEAR
100
P_AC_070400_1_0020001_01_00
Landing Gear Loading on Pavement
WV001, MRW 275 900 kg, CG 33.2%
FIGURE-7-4-0-991-002-A01
7-4-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
**ON A/C A350-900
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
1.
This section provides data about the flexible pavement requirements.
The MLG loading on pavement graphs are given for the weight variants that produce (at the MRW
and maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN 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 7-5-0-991-001-A, calculation of the thickness of the flexible pavement for:
- An aircraft with a MRW of 268 900 kg (592 825 lb),
- A ”CBR” value of 10,
- An annual departure level of 3 000,
- The load on one MLG of 110 000 kg (242 500 lb).
The required flexible pavement thickness is 711 mm (28 in.).
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-5-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
SUBGRADE STRENGTH − CBR
3
6
10
15
20
30
40
60
80
WEIGHT ON ONE MAIN
LANDING GEAR
125 960 kg (277 700 lb)
110 000 kg (242 500 lb)
100 000 kg (220 450 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
MAXIMUM POSSIBLE
MAIN GEAR LOAD
AT MAXIMUM RAMP
WEIGHT AND AFT CG
10 000 COVERAGES USED
FOR ACN CALCULATIONS
ALPHA FACTOR = 0.8
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
60
80
100 120 150 180
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.6 bar (241 psi)
P_AC_070500_1_0010001_01_02
Flexible Pavement Requirements
WV000, MRW 268 900 kg, CG 33%
FIGURE-7-5-0-991-001-A01
7-5-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
SUBGRADE STRENGTH − CBR
3
6
10
15
20
30
40
60
80
WEIGHT ON ONE MAIN
LANDING GEAR
129 330 kg (285 125 lb)
110 000 kg (242 500 lb)
100 000 kg (220 450 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
MAXIMUM POSSIBLE
MAIN GEAR LOAD
AT MAXIMUM RAMP
WEIGHT AND AFT CG
10 000 COVERAGES USED
FOR ACN CALCULATIONS
ALPHA FACTOR = 0.8
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
60
80
100 120 150 180
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.8 bar (244 psi)
P_AC_070500_1_0020001_01_00
Flexible Pavement Requirements
WV001, MRW 275 900 kg, CG 33.2%
FIGURE-7-5-0-991-002-A01
7-5-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0
Flexible Pavement Requirements - LCN Conversion
**ON A/C A350-900
Flexible Pavement Requirements - LCN Conversion
1.
The Load Classification Number (LCN) curves are no longer provided in section 7-6-0 since the LCN
system for reporting pavement strength is obsolete, having been replaced by the ICAO recommended
ACN/PCN system in 1983.
For questions regarding the LCN system, contact Airbus.
7-6-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0
Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A350-900
Rigid Pavement Requirements - Portland Cement Association Design Method
1.
This section provides data about the rigid pavement requirements for the PCA (Portland Cement
Association) design method.
The MLG loading on pavement graphs are given for the weight variants that produce (at the MRW
and maximum aft CG and standards tire pressure) the lowest ACN and the highest ACN for each
type of aircraft.
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 weight on the MLG are made based on the curve for
k = 80 MN/m3 , already shown on the graph.
Example, see FIGURE 7-7-0-991-001-A, calculation of the thickness of the rigid pavement for:
- An aircraft with a MRW of 268 900 kg (592 825 lb),
- A k value of 80 MN/m3 (300 lbf/in3),
- A permitted working stress of 35.15 kg/cm2 (500 lb/in2),
- The load on one MLG of 110 000 kg (242 500 lb).
The required rigid pavement thickness is 290 mm (11 in.).
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-7-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.6 bar (241 psi)
1000
15
38
70
MAXIMUM POSSIBLE MAIN
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
36
14
k = 20 MN/m³
65
900
k = 40 MN/m³
34
60
k = 80 MN/m³
13
k = 150 MN/m³
800
55
50
700
30
28
26
11
600
10
500
9
400
24
18
40
35
30
22
20
(lb/in²)
45
(kg/cm²)
ALLOWABLE WORKING STRESS
12
(in)
RIGID PAVEMENT THICKNESS
(cm)
32
8
WEIGHT ON ONE MAIN
LANDING GEAR
125 960 kg (277 700 lb)
110 000 kg (242 500 lb)
100 000 kg (220 450 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
7
25
300
200
20
15
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.
P_AC_070700_1_0010001_01_01
Rigid Pavement Requirements
WV000, MRW 268 900 kg, CG 33%
FIGURE-7-7-0-991-001-A01
7-7-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.8 bar (244 psi)
1000
15
38
70
MAXIMUM POSSIBLE MAIN
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
36
14
k = 20 MN/m³
65
900
k = 40 MN/m³
34
60
k = 80 MN/m³
13
k = 150 MN/m³
800
55
50
700
30
28
26
11
600
10
500
9
400
24
18
40
35
30
22
20
(lb/in²)
45
(kg/cm²)
ALLOWABLE WORKING STRESS
12
(in)
RIGID PAVEMENT THICKNESS
(cm)
32
8
WEIGHT ON ONE MAIN
LANDING GEAR
129 310 kg (285 075 lb)
110 000 kg (242 500 lb)
100 000 kg (220 450 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
7
25
300
200
20
15
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.
P_AC_070700_1_0020001_01_00
Rigid Pavement Requirements
WV001, MRW 275 900 kg, CG 33.2%
FIGURE-7-7-0-991-002-A01
7-7-0
Page 3
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-0
Rigid Pavement Requirements - LCN Conversion
**ON A/C A350-900
Rigid Pavement Requirements - LCN Conversion
1.
The Load Classification Number (LCN) curves are no longer provided in section 7-8-0 since the LCN
system for reporting pavement strength is obsolete, having been replaced by the ICAO recommended
ACN/PCN system in 1983.
For questions regarding the LCN system, contact Airbus.
7-8-0
Page 1
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0
ACN/PCN Reporting System - Flexible and Rigid Pavements
**ON A/C A350-900
ACN/PCN Reporting System - Flexible and Rigid Pavements
1.
This section provides 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 MLG loading on pavement graphs are given for the weight variants that produce (at the MRW
and maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN 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).
For example, see FIGURE 7-9-0-991-001-A (sheet 1), calculation of the ACN for flexible pavement
for:
- An aircraft with a MRW of 268 900 kg (592 825 lb)
- An aircraft gross weight of 210 000 kg (462 975 lb)
- A medium subgrade strength (code B).
The ACN for flexible pavement is 51.
For example, see FIGURE 7-9-0-991-001-A (sheet 2), calculation of the ACN for rigid pavement for:
- An aircraft with a MRW of 268 900 kg (592 825 lb)
- An aircraft gross weight of 210 000 kg (462 975 lb)
- A medium subgrade strength (code B).
The ACN for rigid pavement is 52.
2.
Aircraft Classification Number - ACN Table
The table (FIGURE 7-9-0-991-003-A) provides ACN data in tabular format similar to the one used by
ICAO in the ”Aerodrome Design Manual Part 3, Pavements - Edition 1983” for all the operational
weight variants of the aircraft.
As an approximation, use a linear interpolation in order to get the ACN at the required operating
weight using the following equation:
- ACN = ACN min + (ACN max -- ACN min) x (Operating Weight - 142 000 kg)/(MRW - 142
000 kg)
As an approximation, also use a linear interpolation in order to get the aircraft weight at the
pavement PCN using the following equation:
- Operating Weight = 142 000 kg + (MRW -- 142 000 kg) x (PCN -- ACN min)/(ACN max -ACN min)
With ACN max: ACN calculated at the MRW in the table and with ACN min: ACN calculated at 142
000 kg.
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-9-0
Page 1
Apr 01/15
7-9-0
20
120
30
40
50
60
70
80
90
100
110
120
130
140
150
160
170
SUBGRADE STRENGTH
D − CBR 3 (ULTRA LOW)
C − CBR 6 (LOW)
B − CBR 10 (MEDIUM)
A − CBR 15 (HIGH)
ALPHA FACTOR = 0.8
300
190
200
(x 1 000 kg)
(x 1 000 lb)
210
220
230
500
240
250
260
270
600
280
ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME
DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983.
AIRCRAFT GROSS WEIGHT
180
400
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.6 bar (241 psi)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
AIRCRAFT CLASSIFICATION NUMBER (ACN)
P_AC_070900_1_0010001_01_01
ACN/PCN Reporting System - WV000, MRW 268 900 kg, CG 33%
Flexible Pavement (Sheet 1 of 2)
FIGURE-7-9-0-991-001-A01
Page 2
Apr 01/15
7-9-0
20
120
30
40
50
60
70
80
90
100
110
120
130
140
150
160
170
400
190
200
(x 1 000 kg)
(x 1 000 lb)
210
220
230
500
240
250
260
270
600
280
ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME
DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983.
AIRCRAFT GROSS WEIGHT
180
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)
300
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.6 bar (241 psi)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
AIRCRAFT CLASSIFICATION NUMBER (ACN)
P_AC_070900_1_0010001_02_00
ACN/PCN Reporting System - WV000, MRW 268 900 kg, CG 33%
Rigid Pavement (Sheet 2 of 2)
FIGURE-7-9-0-991-001-A01
Page 3
Apr 01/15
7-9-0
20
120
30
40
50
60
70
80
90
100
110
120
130
140
150
160
170
SUBGRADE STRENGTH
D − CBR 3 (ULTRA LOW)
C − CBR 6 (LOW)
B − CBR 10 (MEDIUM)
A − CBR 15 (HIGH)
ALPHA FACTOR = 0.8
300
190
200
(x 1 000 kg)
(x 1 000 lb)
210
220
230
500
240
250
260
270
600
280
ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME
DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983.
AIRCRAFT GROSS WEIGHT
180
400
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.8 bar (244 psi)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
AIRCRAFT CLASSIFICATION NUMBER (ACN)
P_AC_070900_1_0020001_01_00
ACN/PCN Reporting System - WV001, MRW 275 900 kg, CG 33.2%
Flexible Pavement (Sheet 1 of 2)
FIGURE-7-9-0-991-002-A01
Page 4
Apr 01/15
7-9-0
20
120
30
40
50
60
70
80
90
100
110
120
130
140
150
160
170
400
190
200
(x 1 000 kg)
(x 1 000 lb)
210
220
230
500
240
250
260
270
600
280
ACN WAS DETERMINED AS REFERENCED IN ICAO AERODROME
DESIGN MANUAL PART 3 CHAPTER 1. SECOND EDITION 1983.
AIRCRAFT GROSS WEIGHT
180
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)
300
1400x530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.8 bar (244 psi)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
AIRCRAFT CLASSIFICATION NUMBER (ACN)
P_AC_070900_1_0020001_02_00
ACN/PCN Reporting System - WV001, MRW 275 900 kg, CG 33.2%
Rigid Pavement (Sheet 2 of 2)
FIGURE-7-9-0-991-002-A01
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
ACN FOR
ACN FOR
LOAD
RIGID PAVEMENT
FLEXIBLE PAVEMENT
ALL UP ON ONE
TIRE
SUBGRADES − MN/m³
SUBGRADES − CBR
WEIGHT MASS
MAIN PRESSURE
VARIANT
(kg)
(MPa)
GEAR
HIGH MEDIUM LOW ULTRA−LOW HIGH MEDIUM LOW ULTRA−LOW
LEG (%)
80
10
150
40
20
15
6
3
A350−900
WV000
A350−900
WV001
A350−900
WV002
268 900
46.8
142 000
275 900
46.9
272 900
142 000
70
82
95
65
69
79
109
32
33
36
41
31
32
34
41
65
73
85
98
68
72
82
113
32
33
36
41
31
32
34
41
65
73
85
98
67
72
82
113
33
33
36
41
31
32
34
42
1.68
142 000
47.4
63
1.66
1.66
P_AC_070900_1_0030001_01_00
ACN Table
FIGURE-7-9-0-991-003-A01
7-9-0
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0
Scaled Drawings
**ON A/C A350-900
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
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
0
0
10
4
20
FEET
30 40
8
12
METERS
50
16
60
20
0
0
10
4
20
FEET
30 40
8
12
METERS
50
16
60
20
NOTE:
WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
P_AC_080000_1_0010001_01_00
Scaled Drawings
FIGURE-8-0-0-991-001-A01
8-0-0
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0
Aircraft Rescue and Fire Fighting
**ON A/C A350-900
Aircraft Rescue and Fire Fighting
1.
This sections provides 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
Apr 01/15
10-0-0
REVISION DATE: APRIL 2015
REFERENCE
: P_RF_000000_1_A350900
SHEET 1/2
AIRBUS S.A.S. 2012 . All rights reserved.
AIRBUS S.A.S
CUSTOMER SERVICES
TECHNICAL DATA SUPPORT AND SERVICES
31707 BLAGNAC CEDEX
FRANCE
THIS CHART GIVES THE GENERAL LAYOUT OF THE A350−900 STANDARD VERSION.
THE NUMBER AND ARRANGEMENT OF THE INDIVIDUAL ITEMS VARY WITH THE CUSTOMERS.
FIGURES CONTAINED IN THIS POSTER ARE AVAILABLE SEPARATELY IN THE CHAPTER 10 OF THE
"AIRCRAFT CHARACTERISTICS − AIRPORT AND MAINTENANCE PLANNING" DOCUMENT.
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0010001_01_03
Front Page
FIGURE-10-0-0-991-001-A01
Page 2
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0030001_01_02
Highly Flammable and Hazardous Materials and Components
FIGURE-10-0-0-991-003-A01
10-0-0
Page 3
Apr 01/15
10-0-0
EMERGENCY EXIT
ACCESS DOOR
NOTE:
THE CREW REST COMPARTMENT INSTALLATION IS OPTIONAL AND RELATED TO AIRCRAFT CONFIGURATION.
ACCESS DOOR
EMERGENCY EXIT
FLIGHT CREW
REST COMPARTMENT
CABIN CREW
REST COMPARTMENT
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0040001_01_01
Crew Rest Compartments Location
FIGURE-10-0-0-991-004-A01
Page 4
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0050001_01_00
Wheel/Brake Overheat
Wheel Safety Area (Sheet 1 of 2)
FIGURE-10-0-0-991-005-A01
10-0-0
Page 5
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0050001_02_00
Wheel/Brake Overheat
Recommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-005-A01
10-0-0
Page 6
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TITANIUM
QUARTZ, GLASS
CFRP SANDWICH
CFRP MONOLITHIC
COMPOSITE MATERIALS
ALU ALLOY
**ON A/C A350-900
P_AC_100000_1_0060001_01_00
Composite Materials Location
FIGURE-10-0-0-991-006-A01
10-0-0
Page 7
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOSE LANDING GEAR
MAIN LANDING GEAR
TYPICAL INSTALLATION
**ON A/C A350-900
P_AC_100000_1_0070001_01_00
Ground Lock Safety Devices
FIGURE-10-0-0-991-007-A01
10-0-0
Page 8
Apr 01/15
10-0-0
COCKPIT
ESCAPE ROPE
GRID EQUALS 1 m (3.28 ft) IN REALITY
CABIN SINGLE−LANE
SLIDE/RAFT
10.25 m (33.63 ft)
EMERGENCY DESCENT THROUGH THE ESCAPE HATCH WITH THE ESCAPE ROPE
NOTE:
− RH SHOWN, LH SYMMETRICAL.
− DIMENSIONS ARE APPROXIMATE.
0
3
6
9
12
15
CABIN DUAL−LANE
SLIDE/RAFT
9.38 m (30.77 ft)
CABIN DUAL−LANE
SLIDE/RAFT
9.43 m (30.94 ft)
CABIN DUAL−LANE
SLIDE/RAFT
9.35 m (30.68 ft)
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0080001_01_02
Emergency Evacuation Devices
FIGURE-10-0-0-991-008-A01
Page 9
Apr 01/15
10-0-0
MECHANICAL
DOOR−LOCKING INDICATORS
TO OPEN:
1 − MAKE SURE THAT RESIDUAL CABIN−PRESSURE WARNING LIGHTS DOES NOT FLASH.
2 − PUSH FLAP TO GRASP HANDLE.
3 − LIFT HANDLE FULLY UP TO HORIZONTAL POSITION (GREEN LINE).
4 − PULL THE DOOR OUT AND MOVE IT FORWARD.
OUTER HANDLE
SLIDE ARMED WARNING−LIGHT AND BUZZER
(SLIDE WILL BE DISARMED AUTOMATICALLY IF
DOOR IS OPEN FROM OUTSIDE)
RESIDUAL
CABIN−PRESSURE
WARNING−LIGHT
PASSENGER/CREW DOORS AND EMERGENCY EXITS
EXTERIOR CONTROL HANDLES
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0090001_01_00
Pax/Crew Doors and Emergency Exits
FIGURE-10-0-0-991-009-A01
Page 10
Apr 01/15
10-0-0
TO OPEN:
1 − PUSH ON THE HANDLE. THE HANDLE IS EJECTED FROM ITS HOUSING.
2 − TURN THE HANDLE COUNTERCLOCKWISE TO DESENGAGE THE LATCHES.
3 − PUSH ON THE ESCAPE HATCH. IT OPENS INSIDE THE COCKPIT.
NOTE:
THE ESCAPE HATCH IS THE COCKPIT EMERGENCY EXIT.
MAKE SURE THAT NO PERSON IN THE COCKPIT IS BELOW THE ESCAPE HATCH.
ESCAPE ROPE
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0100001_01_00
Cockpit Emergency Exit
FIGURE-10-0-0-991-010-A01
Page 11
Apr 01/15
INDICATOR WINDOWS
MANUAL OPERATION
TWO OPERATORS ARE NECESSARY FOR THIS OPERATION.
1 − DO OPERATIONS 1 AND 2 OF THE "NORMAL OPERATION" PROCEDURE.
2 − ON THE YELLOW GROUND SERVICE−PANEL, DO STEP (A) OR (B):
(A) CONNECT A DRILLING MACHINE (WITH SOCKET DIA 1/2 in (12.7 mm)).
(B) ATTACH THE HYDRAULIC AUXILIARY−PUMP GEARBOX TO THE
HYDRAULIC AUXILIARY PUMP. CONNECT THE HANDLE (STORED ON
194KB ) AND THE EXTENSION HANDLE (STORED ON 197LB) WITH
THE HYDRAULIC AUXILIARY−PUMP GEARBOX.
3 − OPERATE THE HYDRAULIC AUXILIARY−PUMP GEARBOX
(AT NOT MORE THAN 100 RPM).
4 − TURN THE MANUAL OPERATING DEVICE TO THE "OPEN" POSITION
(CLOCKWISE) AND HOLD IT UNTIL THE GREEN INDICATOR LIGHT
COMES ON (CARGO DOOR FULLY OPEN AND LOCKED).
5 − RELEASE THE MANUAL OPERATING DEVICE.
6 − STOP THE OPERATION OF THE HYDRAULIC AUXILIARY PUMP.
NOTE:
WARNING: MAKE SURE THAT THE RESIDUAL PRESSURE
WARNING−LIGHT DOES NOT FLASH.
WARNING: ENSURE THAT ALL PERSONNEL AND EQUIPMENT ARE
CLEAR OF CARGO DOOR AREA.
LATCH HANDLE
HANDLE
EXTENSION
HANDLE
YELLOW
GROUND
SERVICE−PANEL
NORMAL OPERATION
HYDRAULIC
AUXILIARY−PUMP
GEARBOX
DRILLING
MACHINE
194KB
1 − PUSH THE LOCK HANDLE FLAP IN AND PULL THE LOCK
HANDLE TO THE "UNLOCKED" POSITION (OUT AND UP).
2 − QUICKLY AND FULLY PULL THE LATCH HANDLE DOWN WITH
A CONTINUOUS MOVEMENT (OUT AND DOWN).
3 − MAKE SURE THAT THE INDICATOR FLAG COMES OUT AND
YOU CAN SEE THE RED INDICATION THROUGH THE EIGHT
INDICATOR WINDOWS.
4 − PUSH THE TOGGLE SWITCH ON THE DOOR OPERATION
PANEL TO THE "OPEN" POSITION AND HOLD IT UNTIL
THE GREEN INDICATOR LIGHT COMES ON (CARGO DOOR
FULLY OPEN AND LOCKED).
5 − RELEASE THE TOGGLE SWITCH.
MANUAL
OPERATING
DEVICE
HYDRAULIC
AUXILIARY
PUMP
197LB
CARGO COMPARTMENT DOOR
TOGGLE SWITCH
GREEN
INDICATOR
LIGHT
194KB
INDICATOR FLAG
LOCK
HANDLE
FLAP
LOCK HANDLE
FWD AND AFT CARGO−COMPARTMENT DOOR−CONTROLS
RESIDUAL
PRESSURE
WARNING−LIGHT
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0110001_01_01
FWD and AFT Lower Deck Cargo Doors
FIGURE-10-0-0-991-011-A01
10-0-0
Page 12
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
INSTALLED ON NLG
**ON A/C A350-900
P_AC_100000_1_0120001_01_00
Control Panels
FIGURE-10-0-0-991-012-A01
10-0-0
Page 13
Apr 01/15
10-0-0
316AR
HOOK LATCH
PIN LATCH
315AL
SAFETY LEVER
A
316BR
1 − OPEN THE OVERPRESSURE DOOR 316BR TO RELEASE UNWANTED AIR PRESSURE.
2 − TURN THE SAFETY LEVER AND BLOCK IT.
3 − RELEASE THE HOOK LATCHES ON RIGHT ACCESS DOOR 316AR.
4 − OPERATE PIN LATCHES (FORWARD AND AFT).
5 − OPEN RIGHT ACCESS DOOR 316AR AND LOCK MANUALLY THE FIXED ROD WHEN DOOR IS FULLY OPEN.
6 − OPERATE PIN LATCHES (FORWARD AND AFT) ON LEFT ACCESS DOOR 315AL .
7 − OPEN LEFT ACCESS DOOR 315AL AND LOCK MANUALLY THE FIXED ROD WHEN DOOR IS FULLY OPEN.
OPERATION:
A
FIXED ROD
FIXED ROD
APU ACCESS DOORS
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0150001_01_01
APU Compartment Access
FIGURE-10-0-0-991-015-A01
Page 14
Apr 01/15
10-0-0
FT3
WL1
FT1
D3
BF3
RAT
BF2
BF1
N1
D2
HT
F3 C1
D1 D5
F1
AP
BF1
BF2
BF3
C1
C2
C3
CP1
D1
D2
D3
D4
D5
m
6.52
2.66
2.08
2.59
3.37
3.29
3.26
6.20
5.37
5.33
5.27
5.21
7.61
ft
21.39
8.73
6.82
8.50
11.06
10.79
10.70
20.34
17.62
17.49
17.29
17.09
24.97
A/C
(142 000 kg)
CONFIGURATION AFT CG (40%)
F1
F2
F3
F4
FT1
FT2
FT3
HT
N1
RAT
RD1
VT
WL1
WL2
m
2.70
2.58
8.78
8.45
3.84
4.64
5.27
7.56
0.93
1.25
4.34
17.07
9.44
7.04
ft
8.86
8.46
28.81
27.72
12.60
15.22
17.29
24.80
3.05
4.10
14.24
56.00
30.97
23.10
A/C
(142 000 kg)
CONFIGURATION AFT CG (40%)
DIMENSIONS ARE RELATED TO AIRCRAFT WEIGHT AND CG CONFIGURATION
FT2
D4 C3 C2 F2 F4
AP
NOTE: PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED
FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
VT
WL2
RD1 CP1
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0160001_01_01
Aircraft Ground Clearances
FIGURE-10-0-0-991-016-A01
Page 15
Apr 01/15
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
=
=
=
=
CUT HERE IN EMERGENCY
NOT MARKED
ON ALL AIRCRAFT
COLORED
**ON A/C A350-900
P_AC_100000_1_0170001_01_01
Structural Break-in Points
FIGURE-10-0-0-991-017-A01
10-0-0
Page 16
Apr 01/15
10-0-0
Z120
BAT 1
A
ELT
BAT
EMER 1
ACCESS VIA FWD
CARGO COMPARTMENT DOOR
FR19
ACCESS VIA
ACCESS DOOR 811
A
C
FR87
B
C
B
ELT ANTENNA
FR88
NOTE:
MAIN BATTERIES:
THE BATTERY CASE AND THE EXHAUST SYSTEM CAN CONTAIN AND ISOLATE AN INTERNAL BATTERY EVENT. IF THERE IS
A BATTERY CELL VENTING EVENT, THE GASES WILL BE RELEASED OUT OF THE AIRCRAFT THROUGH A PIPE CONNECTED
TO THE AIRCRAFT SKIN AND CLOSED BY A BURST DISK. WHEN A CELL VENTING EVENT OCCURS, THE GROUND PERSONNEL
MUST STAY AWAY FROM THE E/E BAY AND THE EXHAUSTED GASES. YOU MUST NOT DISCONNECT THE POWER CONNECTOR
OR CUT OFF THE BATTERY POWER WIRES TO DISCONNECT THE BATTERIES FROM THE ELECTRICAL NETWORK.
BAT 2
BAT EMER 2
FR0
@A350-900
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A350-900
P_AC_100000_1_0180001_01_01
Batteries Location and Access
FIGURE-10-0-0-991-018-A01
Page 17
Apr 01/15