@AIRBUS A /-600 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING

Transcription

1 @AIRBUS A /-600 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus. AIRBUS S.A.S All rights reserved. AIRBUS S.A.S. Customer Services Technical Data Support and Services Blagnac Cedex FRANCE Issue: Apr 01/01 Rev:

2 HIGHLIGHTS Revision No LOCATIONS CHG CODE DESCRIPTIONS OF CHANGE CHAPTER 2 Section 2-1 R Subject General Airplane Characteristics R Subject D Section 2-3 Subject Ground Clearances R NOTE AMENDED FIGURE Ground Clearances R ILLUSTRATION REVISED FIGURE Ground Clearances R ILLUSTRATION REVISED Section 2-6 Subject Lower Deck Cargo Compartments R CONTAINERIZED VOLUME UPDATED CONTAINERIZED VOLUME UPDATED CHAPTER 5 Section 5-2 Subject Subject Section 5-3 Subject Subject Section 5-4 Subject Fuel System FIGURE Overpressure Protector and NACA Flame arrestor Section 5-5 Subject Engine Starting Pneumatic Requirements R R R R R R R N N NEW ILLUSTRATION ADDED ILLUSTRATION ADDED HIGHLIGHTS Page 1

3 LOCATIONS FIGURE Engine Starting Pneumatic Requirements Subject CHG CODE N DESCRIPTIONS OF CHANGE ILLUSTRATION ADDED R Low Ambient Temperatures R DESCRIPTION TITLE UPDATED FIGURE Engine Starting Pneumatic Requirements - Low Ambient Temperature -40 C (-40 F) -- RB 211 TRENT 500 series engine R Subject R Medium Ambient Temperatures R DESCRIPTION TITLE UPDATED FIGURE Engine Starting Pneumatic R Requirements - Medium Ambient Temperature +15 C (+59 F) -- RB 211 TRENT 500 series engine Subject R High Ambient Temperatures R DESCRIPTION TITLE UPDATED FIGURE Engine Starting Pneumatic Requirements - High Ambient Temperature +50 C (+122 F) -- RB 211 TRENT 500 series engine R CHAPTER 7 Section Section Section Section Section Section Section 7-8 Subject Subject Section R D D D D D D R D D D HIGHLIGHTS Page 2

4 LIST OF EFFECTIVE CONTENT CONTENT Revision No CHG CODE LAST REVISION DATE CHAPTER 1 Subject Purpose May 01/07 Subject Introduction May 01/07 CHAPTER 2 Subject General Airplane Characteristics R Subject General Airplane Dimensions May 01/07 FIGURE General Airplane Dimensions May 01/07 FIGURE General Airplane Dimensions May 01/07 Subject Ground Clearances R FIGURE Ground Clearances R FIGURE Ground Clearances R Subject Interior Arrangements May 01/07 Subject Typical Configuration May 01/07 FIGURE Typical Configuration May 01/07 FIGURE Typical Configuration May 01/07 Subject Passenger Compartment Cross-section May 01/07 FIGURE Passenger Compartment Cross-section May 01/07 FIGURE Passenger Compartment Cross-section May 01/07 L.E.C. Page 1

5 CONTENT CHG CODE LAST REVISION DATE FIGURE Passenger Compartment Cross-section May 01/07 Subject Cargo Compartment May 01/07 Subject Lower Deck Cargo Compartments R FIGURE Lower Deck Cargo Compartments May 01/07 FIGURE Loading Combinations May 01/07 Subject Doors Clearances May 01/07 Subject Forward Passenger / Crew Door May 01/07 FIGURE Forward Passenger / Crew Doors May 01/07 Subject Mid Passenger / Crew Door May 01/07 FIGURE Mid Passenger / Crew Door May 01/07 FIGURE Mid Passenger / Crew Door May 01/07 Subject Emergency Exits May 01/07 FIGURE Emergency Exits May 01/07 FIGURE Emergency Exits May 01/07 Subject Aft Passenger / Crew Doors May 01/07 FIGURE Aft Passenger / Crew Doors May 01/07 Subject Forward Cargo Compartment Doors May 01/07 FIGURE Forward Cargo Compartment Doors May 01/07 Subject Aft Cargo Compartment Doors May 01/07 FIGURE Aft Cargo Compartment Doors May 01/07 L.E.C. Page 2

6 CONTENT CHG CODE LAST REVISION DATE Subject Bulk Cargo Compartment Doors May 01/07 FIGURE Bulk Cargo Compartment Doors May 01/07 Subject Main Landing Gear Doors May 01/07 FIGURE Main and Center Landing Gear Doors May 01/07 Subject Radome May 01/07 FIGURE Radome May 01/07 Subject APU and Nose Landing Gear Doors May 01/07 FIGURE APU and Nose Landing Gear Doors May 01/07 FIGURE APU and Nose Landing Gear Doors May 01/07 CHAPTER 3 Subject General Information May 01/07 Subject Payload / Range May 01/07 Subject ISA Conditions May 01/07 FIGURE PAYLOAD / RANGE - RB 211 TRENT 556 engine May 01/07 FIGURE PAYLOAD / RANGE - RB 211 TRENT 553 engine May 01/07 Subject FAR / JAR Takeoff Weight Limitation May 01/07 Subject FAR / JAR Takeoff Weight Limitation May 01/07 FIGURE FAR / JAR Takeoff Weight Limitation - ISA Conditions -- RB 211 TRENT 556 engine May 01/07 L.E.C. Page 3

7 CONTENT FIGURE FAR / JAR Takeoff Weight Limitation - ISA Conditions -- RB 211 TRENT 553 engine Subject CHG CODE LAST REVISION DATE May 01/07 ISA +15 C (ISA +27 F) Conditions May 01/07 FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15 C (ISA +27 F) Conditions -- RB 211 TRENT 556 engine FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15 C (ISA +27 F) Conditions -- RB 211 TRENT 553 engine May 01/07 May 01/07 Subject Landing Field Length May 01/07 Subject ISA Conditions All series engine May 01/07 FIGURE FAR / JAR Landing Field Length - ISA Conditions -- RB 211 TRENT 556 engine FIGURE FAR / JAR Landing Field Length - ISA Conditions -- RB 211 TRENT 553 engine May 01/07 May 01/07 Subject Final Approach Speed May 01/07 Subject Final Approach Speed May 01/07 FIGURE Final Approach Speed - RB 211 TRENT 556 engine May 01/07 FIGURE Final Approach Speed - RB 211 TRENT 553 engine May 01/07 CHAPTER 4 Subject General Information May 01/07 Subject Turning Radii Jan 01/11 FIGURE Turning Radii Jan 01/11 FIGURE Turning Radii Jan 01/11 FIGURE Turning Radii - Steady State Turning Radii Jan 01/11 L.E.C. Page 4

8 CONTENT CHG CODE LAST REVISION DATE FIGURE Turning Radii - Steady State Turning Radii Jan 01/11 Subject Minimum Turning Radii May 01/07 FIGURE Minimum Turning Radii May 01/07 FIGURE Minimum Turning Radii May 01/07 Subject Visibility from Cockpit in Static Position May 01/07 FIGURE Visibility from Cockpit in Static Position May 01/07 Subject Runway and Taxiway Turn Paths May 01/07 Subject Turn - Runway to Taxiway Jan 01/11 FIGURE 135 Turn - Runway to Taxiway - Judgemental Oversteering Jan 01/11 Method FIGURE 135 Turn - Runway to Taxiway - Cockpit Over Centerline Jan 01/11 Method FIGURE 135 Turn - Runway to Taxiway - Judgemental Oversteering Jan 01/11 Method FIGURE 135 Turn - Runway to Taxiway - Cockpit Over Centerline Jan 01/11 Method Subject Turn - Runway to Taxiway Jan 01/11 FIGURE 90 Turn - Runway to Taxiway - Judgement Oversteering Jan 01/11 Method FIGURE 90 Turn - Runway to Taxiway - Cockpit Over Centerline Jan 01/11 Method FIGURE 90 Turn - Runway to Taxiway - Judgement Oversteering Jan 01/11 Method FIGURE 90 Turn - Runway to Taxiway - Cockpit Over Centerline Jan 01/11 Method Subject Turn on a Runway May 01/07 L.E.C. Page 5

9 CONTENT CHG CODE LAST REVISION DATE FIGURE 180 Turn on a Runway - 75 Nose Wheel Steering Jan 01/11 FIGURE 180 Turn on a Runway - 70 Nose Wheel Steering Jan 01/11 Subject Turn - Taxiway to Taxiway Jan 01/11 FIGURE 135 Turn - Taxiway to Taxiway - Judgement Oversteering Jan 01/11 Method FIGURE 135 Turn - Taxiway to Taxiway - Cockpit Over Centerline Jan 01/11 Method FIGURE 135 Turn - Taxiway to Taxiway - Judgement Oversteering Jan 01/11 Method FIGURE 135 Turn - Taxiway to Taxiway - Cockpit Over Centerline Jan 01/11 Method Subject Turn - Taxiway to Taxiway Jan 01/11 FIGURE 90 Turn - Taxiway to Taxiway - Judgemental Oversteering Jan 01/11 Method FIGURE 90 Turn - Taxiway to Taxiway - Cockpit Over Centerline Jan 01/11 Method FIGURE 90 Turn - Taxiway to Taxiway - Judgemental Oversteering Jan 01/11 Method FIGURE 90 Turn - Taxiway to Taxiway - Cockpit Over Centerline Jan 01/11 Method Subject Runway Holding Bay (Apron) Jan 01/11 FIGURE Runway Holding Bay (Apron) Jan 01/11 Subject Airplane Parking May 01/07 FIGURE Airplane Parking - Steering Geometry May 01/07 FIGURE Airplane Parking - Steering Geometry May 01/07 FIGURE Airplane Parking - Minimum Parking Space Requirements May 01/07 FIGURE Airplane Parking - Steering Geometry May 01/07 FIGURE Airplane Parking - Steering Geometry May 01/07 L.E.C. Page 6

10 CONTENT CHG CODE LAST REVISION DATE FIGURE Airplane Parking - Minimum Parking Space Requirements May 01/07 CHAPTER 5 Subject TERMINAL SERVICING Jan 01/10 Subject Airplane Servicing Arrangements Jan 01/10 Subject Symbols Used on Servicing Diagrams Jan 01/10 Subject Loading (Open Apron) Jan 01/10 FIGURE Airplane Servicing Arrangements - Typical Ramp Layout (Open Apron) FIGURE Airplane Servicing Arrangements - Typical Ramp Layout (Open Apron) Jan 01/10 Jan 01/10 Subject Loading (Passenger Bridge) Jan 01/10 FIGURE Airplane Servicing Arrangements - Typical Ramp Layout (gate area) FIGURE Airplane Servicing Arrangements - Typical Ramp Layout (gate area) Jan 01/10 Jan 01/10 Subject Terminal Operations - Full Servicing Turn Round Charts Jan 01/10 Subject Full Servicing Turn Round Charts Jan 01/10 FIGURE Turn around charts - Turn Round Time 63 min. Jan 01/10 FIGURE Turn around charts - Turn Round Time 74 min. Jan 01/10 Subject Terminal Operations - Transit Turn Round Charts Jan 01/10 Subject Transit Turn Round Charts Jan 01/10 L.E.C. Page 7

11 CONTENT CHG CODE LAST REVISION DATE FIGURE Transit Turn Round Charts - Turn Round Time 40 min. Jan 01/10 FIGURE Transit Turn Round Charts - Turn Round Time 46 min. Jan 01/10 Subject Ground Service Connections May 01/07 Subject Ground Service Connections Layout May 01/07 FIGURE Ground Service Connections - Ground Service Connections Layout FIGURE Ground Service Connections - Ground Service Connections Layout May 01/07 May 01/07 Subject Grounding Points May 01/07 FIGURE Ground Service Connections - Grounding Points Jan 01/11 Subject Hydraulic System May 01/07 Subject Electrical System May 01/07 Subject Oxygen System May 01/07 Subject Fuel System R FIGURE Overpressure Protector and NACA Flame arrestor N Subject Pneumatic System May 01/07 Subject Potable Water System May 01/07 Subject Oil System May 01/07 FIGURE Ground Service Connections - Engine Oil Tank - RR TRENT 500 series engine May 01/07 L.E.C. Page 8

12 CONTENT FIGURE Ground Service Connections - IDG Oil Tank - RR TRENT 500 series engine FIGURE Ground Service Connections - Starter Oil Tank - RR TRENT 500 series engine CHG CODE LAST REVISION DATE May 01/07 May 01/07 APU Oil System Jan 01/10 FIGURE Ground Service Connections - APU Oil Tank Jan 01/10 Subject Vacuum Toilet System May 01/07 Subject Engine Starting Pneumatic Requirements N FIGURE Engine Starting Pneumatic Requirements N Subject Low Ambient Temperatures R FIGURE Engine Starting Pneumatic Requirements - Low Ambient Temperature -40 C (-40 F) -- RB 211 TRENT 500 series engine R Subject Medium Ambient Temperatures R FIGURE Engine Starting Pneumatic Requirements - Medium Ambient Temperature +15 C (+59 F) -- RB 211 TRENT 500 series engine R Subject High Ambient Temperatures R FIGURE Engine Starting Pneumatic Requirements - High Ambient Temperature +50 C (+122 F) -- RB 211 TRENT 500 series engine R Subject Ground Pneumatic Power Requirements May 01/07 Subject Heating May 01/07 FIGURE Ground Pneumatic Power Requirements - Heating May 01/07 Subject Cooling May 01/07 L.E.C. Page 9

13 CONTENT CHG CODE LAST REVISION DATE FIGURE Ground Pneumatic Power Requirements - Cooling May 01/07 Subject Preconditioned Airflow Requirements May 01/07 FIGURE Preconditioned Airflow Requirements May 01/07 Subject Ground Towing Requirements Jan 01/11 FIGURE Ground Towing Requirements Jan 01/10 FIGURE Ground Towing Requirements - Typical tow bar configuration 1 FIGURE Ground Towing Requirements - Typical tow bar configuration 2 FIGURE Ground Towing Requirements - Maximum Extension of the NLG Shock Absorber Jan 01/10 Jan 01/10 Jan 01/10 CHAPTER 6 Subject Engine Exhaust Velocities and Temperatures May 01/07 Subject Engine Exhaust Velocities Contours - Ground Idle Power May 01/07 FIGURE Engine Exhaust Velocities - Ground Idle Power - RR TRENT 500 series engine May 01/07 Subject Engine Exhaust Temperatures Contours - Ground Idle Power May 01/07 FIGURE Engine Exhaust Temperatures - Ground Idle Power - RR TRENT 500 series engine May 01/07 Subject Engine Exhaust Velocities Contours - Breakaway Power May 01/07 FIGURE Engine Exhaust Velocities - Breakaway Power - RR TRENT 500 series engine May 01/07 Subject Engine Exhaust Temperatures Contours - Breakaway Power May 01/07 L.E.C. Page 10

14 CONTENT FIGURE Engine Exhaust Temperatures - Breakaway Power - RR TRENT 500 series engine Subject CHG CODE LAST REVISION DATE May 01/07 Engine Exhaust Velocities Contours - Takeoff Power May 01/07 FIGURE Engine Exhaust Velocities - Takeoff Power - RR TRENT 500 series engine May 01/07 Subject Engine Exhaust Temperatures Contours - Takeoff Power May 01/07 FIGURE Engine Exhaust Temperatures - Takeoff Power - RR TRENT 500 series engine May 01/07 Subject Airport and Community Noise Data May 01/07 Subject Noise Data May 01/07 FIGURE Airport and Community Noise - RR TRENT 500 series engine May 01/07 Subject Danger Areas of Engines May 01/07 Subject Ground Idle Power May 01/07 FIGURE Danger Areas of Engines - RR TRENT 500 series engine May 01/07 Subject Breakaway Power May 01/07 FIGURE Danger Areas of Engines - RR TRENT 500 series engine May 01/07 Subject Takeoff Power May 01/07 FIGURE Danger Areas of Engines - RR TRENT 500 series engine May 01/07 Subject APU Exhaust Velocities and Temperatures May 01/07 Subject L.E.C. Page 11

15 CONTENT CHG CODE LAST REVISION DATE APU - GARRETT May 01/07 FIGURE Exhaust Velocities and Temperatures - GARRETT GTCP (A) May 01/07 CHAPTER 7 Subject General Information Jan 01/11 Subject Radius of Relative Stiffness May 01/07 FIGURE Radius of relative stiffness - (Reference : Portland Cement Association) May 01/07 Subject Radius of Relative Stiffness (Other values of E and L ) Jan 01/11 Subject Radius of Relative Stiffness May 01/07 FIGURE Radius of Relative Stiffness - (Effect of E and µ on L values) May 01/07 CHAPTER 8 Subject Possible Future Derivative Airplane May 01/07 CHAPTER 9 Subject ScaledDrawing1in.=50ft. May 01/07 FIGURE Scaled Drawing - 1 in. = 50 ft. May 01/07 FIGURE Scaled Drawing - 1 in. = 50 ft. May 01/07 FIGURE Scaled Drawing - 1 in. = 50 ft. May 01/07 FIGURE Scaled Drawing - 1 in. = 50 ft. May 01/07 Subject Scaled Drawing 1 cm. = 500 cm. May 01/07 FIGURE Scaled Drawing - 1 cm. = 500 cm. May 01/07 L.E.C. Page 12

16 CONTENT CHG CODE LAST REVISION DATE FIGURE Scaled Drawing - 1 cm. = 500 cm. May 01/07 FIGURE Scaled Drawing - 1 cm. = 500 cm. May 01/07 FIGURE Scaled Drawing - 1 cm. = 500 cm. May 01/07 L.E.C. Page 13

17 TABLE OF CONTENTS 1 SCOPE Purpose Introduction 2 AIRPLANE DESCRIPTION General Airplane Characteristics General Airplane Dimensions Ground Clearances Interior Arrangements Typical Configuration Passenger Compartment Cross Section Cargo Compartments Lower Deck Cargo Compartments (Loading combinations) Door Clearances Forward Passenger / Crew Doors Mid Passenger / Crew Doors Emergency Exits Aft Passenger / Crew Doors Forward Cargo Compartment Doors Aft Cargo Compartment Doors Bulk Cargo Compartment Doors Main and Center Landing Gear Doors Radome APU and Nose Landing Gear Doors 3 AIRPLANE PERFORMANCE General Information Payload / Range ISA Conditions FAR / JAR Takeoff Weight Limitation ISA Conditions ISA +15 C (ISA +27 F) Conditions FAR / JAR Landing Field Length ISA Conditions All series engines Final Approach Speed T.O.C. Page 1

18 3-5-1 Final Approach Speed 4 GROUND MANEUVERING General Information Turning Radii Minimum Turning Radii Visibility from Cockpit in Static Position Runway and Taxiway Turn Paths Turn - Runway to Taxiway Turn - Runway to Taxiway Turn on a Runway Turn - Taxiway to Taxiway Turn - Taxiway to Taxiway Runway Holding Bay (Apron) Airplane Parking 5 TERMINAL SERVICING TERMINAL SERVICING Airplane Servicing Arrangements Symbols Used on Servicing Diagrams Loading (Open Apron) Loading (Passenger Bridge) Terminal Operations Type A and Type B Turn around Charts Terminal Operation - en route station Type C Turn around Chart Ground Service Connections Ground Service Connections Layout Grounding Points Hydraulic System Electrical System Oxygen System Fuel System Pneumatic System Potable Water System Oil System Vacuum Toilet System Engine Starting Pneumatic Requirements T.O.C. Page 2

19 5-5-1 Low Ambient Temperatures Medium Ambient Temperatures High Ambient Temperatures Ground Pneumatic Power Requirements Heating Cooling Preconditioned Airflow Requirements Ground Towing Requirements 6 OPERATING CONDITIONS Engine Exhaust Velocities and Temperatures Engine Exhaust Velocities Contours - Ground Idle Power Engine Exhaust Temperatures Contours - Ground Idle Power Engine Exhaust Velocities Contours - Breakaway Power Engine Exhaust Temperatures Contours - Breakaway Power Engine Exhaust Velocities Contours - Takeoff Power Engine Exhaust Temperatures Contours - Takeoff Power Airport and Community Noise Noise Data Danger Areas of Engines Ground Idle Power Breakaway Power Takeoff Power APU Exhaust Velocities and Temperatures APU 7 PAVEMENT DATA General Information Radius of Relative Stiffness Radius of Relative Stiffness (Other values of E and L) Radius of Relative Stiffness 8 DERIVATIVE AIRPLANES Possible Future Derivative Airplane 9 SCALED DRAWINGS Scaled Drawing 1 in. = 500 ft Scaled Drawing 1 cm. = 500 cm. T.O.C. Page 3

20 T.O.C. Page 4

21 SCOPE Purpose Purpose 1. General The A /-600 AIRPLANE CHARACTERISTICS (AC) manual is issued for the A , A basic versions to provide the necessary data needed by airport operators and airlines for the planning of airport facilities. This document conforms to NAS CORRESPONDENCE Correspondence concerning this publication should be directed to : AIRBUS S.A.S. Customer Services Technical Data Support and Services 1 Rond Point Maurice BELLONTE BLAGNAC CEDEX FRANCE Page 1

22 1-2-0 Introduction Introduction 1. General This manual comprises 9 chapters with a List of Effective Pages (LEP) and a Table Of Content (TOC) at the beginning of the manual. Chapter 1 : SCOPE Chapter 2 : AIRPLANE DESCRIPTION This chapter contains general dimensional and other basic aircraft data. It covers : - aircraft dimensions and ground clearances, - passenger and cargo compartments arrangement. Chapter 3 : AIRPLANE PERFORMANCE This chapter indicates the aircraft performance. It covers : - payload range, - takeoff and landing runway requirements, - landing approach speed. Chapter 4 : GROUND MANEUVERING This chapter provides the aircraft turning capability and maneuvering characteristics on the ground. It includes : - turning radii and visibility from the cockpit, - runway and taxiway turn path. Chapter 5 : TERMINAL SERVICING This chapter provides information for the arrangement of ground handling and servicing equipment. It covers : - location and connections of ground servicing equipment, Page 1

23 - engines starting pneumatic and preconditioned airflow requirements. Chapter 6 : OPERATING CONDITIONS This chapter contains data and safety/environmental precautions related to engine and APU operation on the ground. It covers : - contour size and shape of the jet engine exhaust velocities and temperatures, - noise data. Chapter 7 : PAVEMENT DATA This chapter contains the pavement data helpful for airport planning. It gives : - landing gear foot print and static load, - charts for flexible pavements with Load Classification Number (LCN), - charts for rigid pavements with LCN, - Aircraft Classification Number (ACN), Pavement Classification Number (PCN), reporting system for flexible and rigid pavements. Chapter 8 : DERIVATIVE AIRPLANES This chapter gives relevant data of possible new version with the associated size change. Chapter 9 : SCALED DRAWINGS This chapter contains different airplane scaled drawings Page 2

24 2-1-0 General Airplane Characteristics AIRPLANE DESCRIPTION General Airplane Characteristics 1. General Airplane Characteristics The weight terms used throughout this manual are given below together with their respective definitions. Maximum Taxi Weight (MTW) : Maximum weight for ground maneuver as limited by aircraft strength and airworthiness requirements. (It includes weight of run-up and taxi fuel). It is also called Maximum Ramp Weight (MRW). Maximum Landing Weight (MLW) : Maximum weight for landing as limited by aircraft strength and airworthiness requirements. Maximum Takeoff Weight (MTOW) : Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (This is the maximum weight at start of the takeoff run). Maximum Zero Fuel Weight (MZFW) : Maximum operational weight of the aircraft without usable fuel. Standard Seating Capacity : Number of passengers specifically certified or anticipated for certification. Usable Volume : Usable volume available for cargo, pressurized fuselage, passenger compartment and cockpit. Usable Fuel Capacity: Fuel available for aircraft propulsion. Water Volume : Volume of cargo compartment Page 1

25 2-2-0 General Airplane Dimensions General Airplane Dimensions 1. This section provides General Airplane Dimensions Page 1

26 **ON A/C A m ( ft) m ( ft) NOTE: FOR DOOR DIMENSIONS AND LOCATIONS, SEE CHAPTER 2 7. SCALE FEET SCALE METER m (89.64 ft) m (93.79 ft) m ( ft) m (21.57 ft) m ( ft) MLG m ( ft) CLG m ( ft) m ( ft) m ( ft) m (74.12 ft) SEE CHAPTER m (18.50 ft) m (35.05 ft) m (61.48 ft) m ( ft) F_AC_020200_1_ _01_00 General Airplane Dimensions FIGURE A Page 2

27 **ON A/C A m ( ft) NOTE: FOR DOOR DIMENSIONS AND LOCATIONS, SEE CHAPTER m (94.00 ft) SCALE FEET SCALE METER m (72.25 ft) m (76.40 ft) m ( ft) m (21.57 ft) m ( ft) MLG m ( ft) CLG m ( ft) m ( ft) m ( ft) m (74.12 ft) SEE CHAPTER m (18.50 ft) m (35.05 ft) m (61.48 ft) m ( ft) F_AC_020200_1_ _01_00 General Airplane Dimensions FIGURE A Page 3

28 2-3-0 Ground Clearances Ground Clearances 1. This section gives the height of various points of the aircraft, above the ground, for different aircraft configurations. Dimensions in the tables are approximate and will vary with tire type, W&B an others special conditions. The dimensions are given for: - the basic aircraft OWE with a mid CG, - the MRW for the lightest weight variant with a FWD CG and a AFT CG, - the MRW for the heaviest weight variant with a FWD CG and a AFT CG, - aircraft on jacks, FDL at 7.2 m (23.62 ft). NOTE : Passenger and cargo door clearances are measured from the center of the door sill and from floor level Page 1

29 **ON A/C A M X L C2Y K E3 J H E2 D C1 B E1 A Z P N V U T S F R O Q OWE 354.6t MTW 350t AIRCRAFT A/C MID CG CG: 16% FWD CG CG: 38% ON JACKS CONFIGURATION m ft m ft m ft m ft m ft A B FR 37.9 C FR 74 C D FR 23 E FR 37.9 E FR 56.4 E F FR 40.4 H J K L M N O P Q R S T U V FR 99 X Y Z NOTE: PASSENGER AND CARGO DOOR CLEARANCES ARE MEASURED FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL. F_AC_020300_1_ _01_01 Ground Clearances FIGURE A Page 2

30 **ON A/C A M X L C2 Y K E3 J H D C1 E2 A B E1 Z P N V U T S F R O Q OWE 349.2t MTW MTW A/C MID CG CG: 22% FWD CG AFT CG CONFIGURATION m ft m ft m ft m ft m A B FR 37.9 C FR 74 C D FR 23 E FR 37.9 E FR 53.6 E AIRCRAFT ON JACKS ft F FR 40.4 FR 99 H J K L M N O P Q R S T U V X Y Z NOTE: PASSENGER AND CARGO DOOR CLEARANCES ARE MEASURED FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL. F_AC_020300_1_ _01_01 Ground Clearances FIGURE A Page 3

31 2-4-0 Interior Arrangements Interior Arrangements 1. This section gives the standard interior arrangements configuration Page 1

32 2-4-1 Typical Configuration Typical Configuration 1. This section gives the typical configuration for A and A Page 1

33 **ON A/C A G VCC PASSENGER SEATS (380 TOTAL) 12 FIRST CLASS 54 BUSINESS CLASS 314 TOURIST CLASS A A G G A A A G C G C L L L L L A L C ITEM DESIGNATION A ATTENDANT SEAT (12) C COAT STOWAGE (3) G GALLEY (10) L LAVATORY (11) S STOWAGE (3) VCC VCC VIDEO (1) L L L L L A A G G G S A A G A G A S S F_AC_020401_1_ _01_00 Typical Configuration FIGURE A Page 2

34 **ON A/C A G VCC A L G C A A A L L A G C A L PASSENGER SEATS (313 TOTAL) 12 FIRST CLASS 36 BUSINESS CLASS 265 TOURIST CLASS A G L L G L A G L ITEM DESIGNATION A ATTENDANTS SEAT (12) C COAT STOWAGE (2) G GALLEY (11) L LAVATORY (10) S STOWAGE (3) VCC VCC VIDEO (1) L L G G G S A A G A A G S S F_AC_020401_1_ _01_00 Typical Configuration FIGURE A Page 3

35 2-5-0 Passenger Compartment Cross Section Passenger Compartment Cross-section 1. This section gives the typical passenger compartment cross-section configuration of A /-600 models Page 1

36 mm (54.00 in) mm (21.00 in) mm (54.00 in) 1650 mm (64.96 in) 1827 mm (71.92 in) mm (5.07 in) 1006 mm (39.61 in) 1006 mm (39.61 in) 2462 mm (96.93 in) 5287 mm ( in) 450 mm (17.72 in) 2402 mm (94.56 in) 2222 mm (87.48 in) F_AC_020500_1_ _01_00 Passenger Compartment Cross-section FIGURE A Page 2

37 mm (54.00 in) mm (21.00 in) mm (54.00 in) 1650 mm (64.96 in) 1827 mm (71.92 in) mm (5.07 in) 1006 mm (39.61 in) 1006 mm (39.61 in) 2462 mm (96.93 in) 5287 mm ( in) 450 mm (17.72 in) 2401 mm (94.52 in) 1783 mm (70.20 in) F_AC_020500_1_ _01_00 Passenger Compartment Cross-section FIGURE A Page 3

38 mm (41.50 in) mm (19.00 in) mm (41.50 in) 1650 mm (64.96 in) 1827 mm (71.92 in) 503 mm (19.80 in) mm (5.32 in) 1006 mm (39.61 in) 503 mm (19.80 in) 2462 mm (96.93 in) 5287 mm ( in) 450 mm (17.72 in) 2401 mm (94.52 in) 1783 mm (70.20 in) F_AC_020500_1_ _01_00 Passenger Compartment Cross-section FIGURE A Page 4

39 2-6-0 Cargo Compartments Cargo Compartment 1. This section gives the cargo compartments location and dimensions Page 1

40 2-6-1 Lower Deck Cargo Compartments (Loading combinations) Lower Deck Cargo Compartments **ON A/C A This table gives cargo compartments loading combinations. Cargo Compartment Palletized volume Containerized volume Forward Door size (h w) 3256 ft 3 ( m 3 ) 3672 ft 3 ( m 3 ) in (1.699 m) x in (2.701 m) basedon96in 125 in pallets loaded to height of 64 in (1.626 m) basedonld3(iataenas K2C) container volume Aft Door size (h w) 2442 ft 3 ( m 3 ) 2754 ft 3 ( m 3 ) 66.3 in (1.684 m) x in (2.720 m) Bulk Door size (h w) 37.4 in (0.950 m) x 37.4 in (0.950 m) basedon96in 125 in pallets loaded to height of 64 in (1.626 m) 695 ft 3 ( m 3 ) basedonld3(iataenas K2C) container volume **ON A/C A This table gives cargo compartments loading combinations. Cargo Compartment Palletized volume Containerized volume Forward Door size (h w) 2442 ft 3 ( m 3 ) 2754 ft 3 ( m 3 ) in (1.699 m) x in (2.701 m) basedon96in 125 in pallets loaded to height of 64 in (1.626 m) basedonld3(iataenas K2C) container volume Aft Door size (h w) 1628 ft 3 ( m 3 ) 1836 ft 3 ( m 3 ) 66.3 in (1.684 m) x in (2.720 m) Bulk Door size (h w) 37.4 in (0.950 m) x 37.4 in (0.950 m) basedon96in 125 in pallets loaded to height of 64 in (1.626 m) 695 ft 3 ( m 3 ) basedonld3(iataenas K2C) container volume Page 1

41 TYPICAL SECTIONS FR20 TO FR39.2 AND FR53.2 TO FR65 TOP OF CARGO COMPT CARGO COMPT FLOOR 3.18 m (125.0 in) 4.15 m (163.4 in) m (222.0 in) FWD : 1.75 m (68.9 in) AFT : 1.71 m (67.3 in) 2.70 m (106.3 in) 2.72 m (107.1 in) 0.95 m (37.4 in) 600: 500: m m (66.6 ft) (50.1 ft) m m (49.2 ft) (34.0 ft) 4.04 m (159.1 in) 4.04 m (159.1 in) FWD CARGO COMPTARTMENT AFT CARGO COMPARTMENT BULK CARGO COMPARTMENT F_AC_020601_1_ _01_00 Lower Deck Cargo Compartments FIGURE A Page 2

42 FWD CARGO COMPT AFT CARGO COMPT CARGO FLEXIBILITY LOADING COMBINATIONS TYPICAL LOADING COMBINATIONS STANDARD AIRCRAFT HALF SIZE CONTAINERS NAS K2C AS PER IATA CONTOUR E OR 60.4 in X 61.5 in PALLETS NAS K3P LIMITED TO MAX GROSS WEIGHT 3500 lb (1587kg) EACH A A FWD AFT FWD AFT HALF SIZE CONTAINERS NAS K2C AS PER IATA CONTOUR C LIMITED TO MAX GROSS WEIGHT 3500 lb (1587kg) EACH FULL SIZE CONTAINERS NAS L2C AS PER IATA CONTOUR F OR 60.4 in X 61.5 in PALLETS NAS K3P,2L4P LIMITED TO MAX GROSS WIGHT 3500 lb (3174kg) EACH 96 in X 125 in PALLETS NAS MIP,2P,3P LIMITED TO MAX GROSS WEIGHT lb (4626kg) EACH (WITH POTENTIAL FOR EXTENSION TO lb (5103 kg) F_AC_020601_1_ _01_00 Loading Combinations FIGURE A Page 3

43 2-7-0 Door Clearances Doors Clearances 1. This section gives doors clearances Page 1

44 2-7-1 Forward Passenger / Crew Doors Forward Passenger / Crew Door 1. This section gives forward passenger / crew doors clearances Page 1

45 2.43 m (7 ft 11 in) 1.07 m (3 ft 6 in) 0.64 m (2 ft 1 in) C L 0.75 m (2 ft 5 in) 3.30 m (10 ft 9 in) CRITICAL CLEARANCE LIMIT 5.85 m (19 ft 2 in) 3.00 m (9 ft 10 in) 1.93 m (6 ft 3 in) C L m (1.77 in) SEE CHAPTER 2 3 C L F_AC_020701_1_ _01_01 Forward Passenger / Crew Doors FIGURE A Page 2

46 2-7-2 Mid Passenger / Crew Doors Mid Passenger / Crew Door 1. This section gives mid passenger / crew doors clearances Page 1

47 **ON A/C A C L 0.75 m (2 ft 5 in) 0.75 m (2 ft 5 in) 2.43 m 1.07 m (3 ft 6 in) (7 ft 11 in) 3.40 m (11 ft 1 in) 1.07 m (3 ft 6 in) 2.43 m (7 ft 11 in) 4.85 m (15 ft 10 in) A (FROM NOSE) 23.91m (78 ft 10 in) A (FROM NOSE) m (155 ft 8 in) C L m (1.77 in) A A SEE CHAPTER m (11 ft 1 in) 3.41 m (11 ft 2 in) 4.85 m (15 ft 10 in) C L 1.93 m (6 ft 3 in) 0.64 m (2 ft 1 in) (TOP OF FLOOR) A A F_AC_020702_1_ _01_02 Mid Passenger / Crew Door FIGURE A Page 2

48 C L 0.75 m (2 ft 5 in) 2.43 m (7 ft 11 in) 1.07 m (3 ft 6 in) 3.40 m (11 ft 1 in) (FROM NOSE): m (61 ft 7 in) A C L m (1.77 in) A 3.40 m (11 ft 1 in) SEE CHAPTER m (11 ft 2 in) 1.93 m (6 ft 3 in) C L 0.64 m (2 ft 1 in) (TOP OF FLOOR) A A F_AC_020702_1_ _01_02 Mid Passenger / Crew Door FIGURE A Page 3

49 2-7-3 Emergency Exits Emergency Exits 1. This section gives emergency exits doors clearances Page 1

50 **ON A/C A C L 0.53 m (1 ft 8 in) LINING 0.5 m (1 ft 7 in) 1.47 m (4 ft 9 in) 0.61 m (2 ft) DOOR (FROM NOSE) m (111 ft 10 in) A C L 0.1 m (3.93 in) SEE CHAPTER m (10 ft 6 in) A C L 1.46 m (4 ft 9 in) LINING 1.66 m (5 ft 5 in) DOOR 0.38 m (1 ft 2 in) A A Emergency Exits FIGURE A01 F_AC_020703_1_ _01_ Page 2

51 **ON A/C A C L 0.52 m (1 ft 8 in) 1.46 m (4 ft 9 in) 0.61 m (2 ft) DOOR (FROM NOSE) m (123 ft 6 in) A C L m (1.25 in) SEE CHAPTER m (10 ft 7 in) A C L 1.66 m (5 ft 5 in) DOOR 0.42 m (1 ft 4 in) A A F_AC_020703_1_ _01_00 Emergency Exits FIGURE A Page 3

52 2-7-4 Aft Passenger / Crew Doors Aft Passenger / Crew Doors 1. This section gives Aft passenger / crew doors clearances Page 1

53 2.43 m (8 ft) 1.07 m (3 ft 6 in) C L CRITICAL CLEARANCE LIMIT 0.75 m (2 ft 5 in) 3.00 m (9 ft 10 in) (FROM NOSE) A : m (200 ft 0.2 in) A : m (177 ft 7 in) A 1.99 m (6 ft 6 in) C L C L m (1.8 in) 0.64 m (2 ft 1 in) C L A SEE CHAPTER 2 3 A A F_AC_020704_1_ _01_00 Aft Passenger / Crew Doors FIGURE A Page 2

54 2-7-5 Forward Cargo Compartment Doors Forward Cargo Compartment Doors 1. This section gives forward cargo compartment doors clearances Page 1

55 C L m (FROM NOSE) (31 ft 3 in) A C L 2.7 m (8 ft 10 in) SEE CHAPTER 2 3 A C L C L 2.04 m (6 ft 8 in) 1.70 m (5 ft 6 in) 5.27 m (17 ft 3 in) A A F_AC_020705_1_ _01_00 Forward Cargo Compartment Doors FIGURE A Page 2

56 2-7-6 Aft Cargo Compartment Doors Aft Cargo Compartment Doors 1. This section gives Aft cargo compartment doors clearances Page 1

57 C L A : m(180 ft 4 in) A : m(155 ft 11 in) (FROM NOSE) AFT PASSENGER/CREW DOOR A C L BULK CARGO COMPARTMENT DOOR AFT CARGO COMPARTMENT DOOR A 2.72m (8 ft 11 in) C L SEE CHAPTER 2 3 C L 1.92 m (6 ft 3 in) 1.68 m (5 ft 6 in) 5.19 m (17 ft) A A F_AC_020706_1_ _01_00 Aft Cargo Compartment Doors FIGURE A Page 2

58 2-7-7 Bulk Cargo Compartment Doors Bulk Cargo Compartment Doors 1. This section gives the bulk cargo compartment doors clearances Page 1

59 C L A : m (190 ft 1 in) A : m (165 ft 9 in) (FROM NOSE) AFT PASSENGER/CREW DOOR A (REF) C L BULK CARGO COMPARTMENT DOOR AFT CARGO COMPARTMENT DOOR SEE CHAPTER m (3 ft 1 in) 1.1 m (3 ft 7 in) A C L C L 1.07 m (3 ft 6 in) 1.41 m (4 ft 7 in) A A F_AC_020707_1_ _01_00 Bulk Cargo Compartment Doors FIGURE A Page 2

60 2-7-8 Main and Center Landing Gear Doors Main Landing Gear Doors 1. This section gives the main landing gear doors clearances Page 1

61 A A : m (120 ft 5 in) A : m (102 ft 8 in) 3.96 m (13 ft) A/C C L m (10 ft 4 in) 1.02 m (3 ft 4 in) m (7 ft 6 in) m (1 in) 1.1 m (3 ft 7 in) 2.58 m (8 ft 5 in) MAX m (1 ft 2 in) * MIN m (6 in) GROUND LINE * DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT A F_AC_020708_1_ _01_00 Main and Center Landing Gear Doors FIGURE A Page 2

62 2-7-9 Radome Radome 1. This section gives the radome clearances Page 1

63 STA FR1 C L 1.25 m (4 ft 1 in) m (4 ft 4 in) m (5 ft 4 in) F_AC_020709_1_ _01_00 Radome FIGURE A Page 2

64 APU and Nose Landing Gear Doors APU and Nose Landing Gear Doors 1. This section gives APU and Nose Landing Gear doors clearances Page 1

65 **ON A/C A FR94 FR98 FUSELAGE DATUM LINE MAX m (19 ft 9 in) * * MAX m (22 ft 4 in) MIN m (18 ft 8 in) MIN m (21 ft 3 in) MAX. 2.2 m (7 ft 2 in) MIN m (6 ft 5 in) * * MAX m (5 ft 5 in) MIN m (4 ft 5 in) * DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT APU and Nose Landing Gear Doors FIGURE A01 F_AC_020710_1_ _01_ Page 2

66 **ON A/C A FR94 FR98 FUSELAGE DATUM LINE MAX m (2 ft 0.4 in) * * MAX m (22 ft 8 in) MIN m (19 ft 1 in) MIN m (21 ft 8 in) MAX m (7 ft 1 in) MIN m (6 ft 3 in) * * MAX m (5 ft 4 in) MIN m (4 ft 7 in) * DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT APU and Nose Landing Gear Doors FIGURE A01 F_AC_020710_1_ _01_ Page 3

67 3-1-0 General Information General Information 1. This section gives standard day temperatures. AIRPLANE PERFORMANCE Section 3-2 indicates payload range information at specific altitudes recommended for long range cruise with a given fuel reserve condition. Section 3-3 represents FAR takeoff runway length requirements at ISA and ISA +15 C (+27 F) for RB 211 TRENT 500 series engine conditions for FAA certification. Section 3-4 represents FAR landing runway length requirements for FAA certification. Section 3-5 indicates final approach speeds. Standard day temperatures for the altitude shown are tabulated below: Standard day temperatures for the altitude Altitude Standard Day Temperature FEET METERS F C Page 1

68 3-2-0 Payload / Range Payload / Range 1. Payload / Range Page 1

69 3-2-1 ISA Conditions ISA Conditions 1. This section gives the payload / range at ISA conditions Page 1

70 **ON A/C A ZFW (1000 kg) PAYLOAD (1000 kg) NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. MAX STRUCTURAL PAYLOAD MAX PASSENGER PAYLOAD CRUISE CONDITIONS ISA ft M = RANGE (nm) RANGE (km) F_AC_030201_1_ _01_00 PAYLOAD / RANGE RB 211 TRENT 556 engine FIGURE A Page 2

71 **ON A/C A NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. ZFW (1000 kg) PAYLOAD (1000 kg) MAX STRUCTURAL PAYLOAD MAX PASSENGER PAYLOAD CRUISE CONDITIONS ISA ft M = RANGE (nm) RANGE (km) F_AC_030201_1_ _01_00 PAYLOAD / RANGE RB 211 TRENT 553 engine FIGURE A Page 3

72 3-3-0 FAR / JAR Takeoff Weight Limitation FAR / JAR Takeoff Weight Limitation 1. FAR / JAR Takeoff Weight Limitation Page 1

73 3-3-1 ISA Conditions FAR / JAR Takeoff Weight Limitation 1. This section gives the takeoff weight limitation at ISA conditions Page 1

74 **ON A/C A 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 1000 lb 1000 kg AIRPORT PRESSURE ALTITUDE (1000 ft) BRAKE ENERGY LIMITATION V.M.C RUNWAY LENGTH (1000 m) RUNWAY LENGTH (1000 ft) FAR/JARTakeoffWeightLimitation ISA Conditions -- RB 211 TRENT 556 engine FIGURE A01 F_AC_030301_1_ _01_ Page 2

75 **ON A/C A 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 1000 lb 1000 kg AIRPORT PRESSURE ALTITUDE (1000 ft) BRAKE ENERGY LIMITATION V.M.C RUNWAY LENGTH (1000 m) RUNWAY LENGTH (1000 ft) FAR/JARTakeoffWeightLimitation ISA Conditions -- RB 211 TRENT 553 engine FIGURE A01 F_AC_030301_1_ _01_ Page 3

76 3-3-2 ISA +15 C (ISA +27 F) Conditions ISA +15 C (ISA +27 F) Conditions 1. This section gives the takeoff weight limitation at ISA +15 C (ISA +27 F) conditions Page 1

77 **ON A/C A TAKE OFF WEIGHT 1000 lb 1000 kg NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT AIRPORT PRESSURE ALTITUDE (1000 ft) BRAKE ENERGY LIMITATION V.M.C RUNWAY LENGTH (1000 m) RUNWAY LENGTH (1000 ft) FAR/JARTakeoffWeightLimitation ISA +15 C (ISA +27 F) Conditions -- RB 211 TRENT 556 engine FIGURE A01 F_AC_030302_1_ _01_ Page 2

78 **ON A/C A 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 1000 lb 1000 kg AIRPORT PRESSURE ALTITUDE (1000 ft) BRAKE ENERGY LIMITATION V.M.C RUNWAY LENGTH (1000 m) RUNWAY LENGTH (1000 ft) FAR/JARTakeoffWeightLimitation ISA +15 C (ISA +27 F) Conditions -- RB 211 TRENT 553 engine FIGURE A01 F_AC_030302_1_ _01_ Page 3

79 3-4-0 FAR / JAR Landing Field Length Landing Field Length 1. Landing Field Length Page 1

80 3-4-1 ISA Conditions All series engines ISA Conditions All series engine 1. This section gives the landing field length Page 1

81 **ON A/C A LANDING FIELD LENGTH (1000 ft) (1000 m) 12 NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. AIRFIELD ELEVATION (1000 ft) VALID FOR ALL TEMPERATURES GROSS WEIGHT (1000 kg) GROSS WEIGHT (1000 lb) FAR / JAR Landing Field Length ISA Conditions -- RB 211 TRENT 556 engine FIGURE A01 F_AC_030401_1_ _01_ Page 2

82 **ON A/C A LANDING FIELD LENGTH (1000 ft) (1000 m) NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. AIRFIELD ELEVATION (1000 ft) VALID FOR ALL TEMPERATURES GROSS WEIGHT (1000 kg) GROSS WEIGHT (1000 lb) FAR / JAR Landing Field Length ISA Conditions -- RB 211 TRENT 553 engine FIGURE A01 F_AC_030401_1_ _01_ Page 3

83 3-5-0 Final Approach Speed Final Approach Speed 1. Final Approach Speed Page 1

84 3-5-1 Final Approach Speed Final Approach Speed 1. This section gives the final approach speed Page 1

85 **ON A/C A NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. C.A.S (Kts) LANDING GEAR DOWN FULL POSITION GROSS WEIGHT (1000 kg) GROSS WEIGHT (1000 lb) Final Approach Speed RB 211 TRENT 556 engine FIGURE A01 F_AC_030501_1_ _01_ Page 2

86 **ON A/C A NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY. THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT. C.A.S (Kts) LANDING GEAR DOWN FULL POSITION GROSS WEIGHT (1000 kg) GROSS WEIGHT (1000 lb) Final Approach Speed RB 211 TRENT 553 engine FIGURE A01 F_AC_030501_1_ _01_ Page 3

87 4-1-0 General Information GROUND MANEUVERING General Information 1. This section provides airplane turning capability and maneuvering characteristics. For ease of presentation, this data has been determined from the theoretical limits imposed by the geometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such, it reflects the turning capability of the aircraft in favorable operating circumstances. This data should only be used as guidelines for the method of determination of such parameters and for the maneuvering characteristics of this aircraft type. In the ground operating mode, varying airline practices may demand that more conservative turning procedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airline operating techniques will vary in the level of performance, over a wide range of operating circumstances throughout the world. Variations from standard aircraft operating patterns may be necessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limited area or high risk of jet blast damage. For these reasons, ground maneuvering requirements should be coordinated with the using airlines prior to layout planning Page 1

88 4-2-0 Turning Radii Turning Radii 1. This section gives the turning radii Page 1

89 **ON A/C A R5 R3 R6 R4 F_AC_040200_1_ _01_01 Turning Radii FIGURE A Page 2

90 **ON A/C A R5 R3 R6 R4 F_AC_040200_1_ _01_01 Turning Radii FIGURE A Page 3

91 **ON A/C A STEERING ANGLE A TURNING RADII EFFECTIVE STEERING ANGLE m ft m ft m ft m ft m ft m ft m ft m ft m ft m ft m ft m ft R3 R4 R5 NLG WING NOSE TURNING RADII TABLE R6 TAIL NOTE: SYMMETRIC THRUST NO BRAKING F_AC_040200_1_ _01_00 Turning Radii Steady State Turning Radii FIGURE A Page 4

92 **ON A/C A STEERING ANGLE A TURNING RADII EFFECTIVE STEERING ANGLE m ft m ft m ft m ft m ft m ft m ft m ft m ft m ft m ft R3 R4 R5 NLG WING NOSE R6 TAIL TURNING RADII TABLE NOTE: SYMMETRIC THRUST NO BRAKING F_AC_040200_1_ _01_00 Turning Radii Steady State Turning Radii FIGURE A Page 5