@AIRBUS
A330-700L
AIRCRAFT CHARACTERISTICS
AIRPORT AND MAINTENANCE PLANNING
AC
The content of this document is the property of Airbus.
It is supplied in confidence and commercial security on its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may
information contained in it be disclosed to unauthorized persons.
It must not be reproduced in whole or in part without permission in writing from the owners of
the copyright. Requests for reproduction of any data in this document and the media authorized
for it must be addressed to Airbus.
© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
31707 Blagnac Cedex
FRANCE
Issue: Apr 01/20
Rev: Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 2 - Jul 01/21
LOCATIONS
CHG
CODE
DESCRIPTIONS OF CHANGE
CHAPTER 2
Section 2-3
Subject 2-3-0
Ground Clearances
FIGURE Ground Clearances - Ground
Clearances for WV000 at MRW and 135
000 kg (297 624 lb)
R
R
FIGURE Ground Clearances - Ground
Clearances for Flaps Retracted with
WV000
R
FIGURE Ground Clearances - Ground
Clearances for Flaps in Intermediate
Position with WV000
R
FIGURE Ground Clearances - Ground
Clearances for Flaps Fully Extended with
WV000
R
ADDED A NOTE RELATED TO THE
GROUND CLEARANCE VALUES IN THE
TABLE ARE DEPEND ON THE CG
POSITION AND AIRCRAFT WEIGHT.
ADDED A NOTE RELATED TO THE
GROUND CLEARANCE VALUES IN THE
TABLE ARE DEPEND ON THE CG
POSITION AND AIRCRAFT WEIGHT.
ADDED A NOTE RELATED TO THE
GROUND CLEARANCE VALUES IN THE
TABLE ARE DEPEND ON THE CG
POSITION AND AIRCRAFT WEIGHT.
ADDED A NOTE RELATED TO THE
GROUND CLEARANCE VALUES IN THE
TABLE ARE DEPEND ON THE CG
POSITION AND AIRCRAFT WEIGHT.
Section 2-14
Subject 2-14-0
FIGURE Jacking for Maintenance Ground Clearance on Jacks
R
HIGHLIGHTS
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 2 - Jul 01/21
CONTENT
CHG
CODE
LAST REVISION
DATE
CHAPTER 1
Subject 1-1-0
Introduction
Apr 01/20
Subject 1-2-1
Glossary
Apr 01/20
CHAPTER 2
Subject 2-1-1
General Aircraft Characteristics Data
Apr 01/20
Subject 2-2-0
General Aircraft Dimensions
Apr 01/20
FIGURE General Aircraft Dimensions
Apr 01/20
Subject 2-3-0
Ground Clearances
R
Jul 01/21
FIGURE Ground Clearances - Ground Clearances for WV000 at MRW
and 135 000 kg (297 624 lb)
R
Jul 01/21
R
Jul 01/21
R
Jul 01/21
R
Jul 01/21
FIGURE Ground Clearances - Ground Clearances for Flaps Retracted
with WV000
FIGURE Ground Clearances - Ground Clearances for Flaps in
Intermediate Position with WV000
FIGURE Ground Clearances - Ground Clearances for Flaps Fully
Extended with WV000
Subject 2-4-1
Interior Arrangements - Plan View
Apr 01/20
FIGURE Interior Arrangements - Plan View
Apr 01/20
Subject 2-6-1
Lower Deck Cargo Compartments
Apr 01/20
FIGURE Lower Deck Cargo Compartments - Location and Dimensions
Apr 01/20
Subject 2-6-2
L.E.C.
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
Main Deck Cargo Compartment
FIGURE Main-Deck Cargo Compartment - Location and Dimensions
CHG
CODE
LAST REVISION
DATE
Apr 01/20
Apr 01/20
Subject 2-6-3
Main and Lower Deck Cross-sections
Apr 01/20
FIGURE Lower-Deck Cargo Cross-sections
Apr 01/20
FIGURE Main-Deck-Cargo Arrangement Cross-sections
Apr 01/20
Subject 2-7-0
Door Clearances
Apr 01/20
FIGURE Lateral Position of Doors from Aircraft Nose
Apr 01/20
FIGURE Radome
Apr 01/20
FIGURE Aft Cargo-Compartment Door
Apr 01/20
FIGURE Bulk Cargo-Compartment Door
Apr 01/20
FIGURE MLG Doors
Apr 01/20
Subject 2-9-0
Landing Gear
Apr 01/20
FIGURE Landing Gear Position
Apr 01/20
FIGURE Main Landing Gear
Apr 01/20
FIGURE Nose Landing Gear
Apr 01/20
FIGURE Tow Truck Power - NLG Servicing 3
Apr 01/20
Subject 2-10-0
Exterior Lighting
Apr 01/20
FIGURE Exterior Lighting - Lights General Layout
Apr 01/20
Subject 2-11-0
Antennas and Probes Location
Apr 01/20
FIGURE Antennas and Probes - Location
Jun 01/20
Subject 2-12-0
Engine and Nacelle
Apr 01/20
FIGURE Engine and Nacelle - Engine Dimensions - RR TRENT 700
Apr 01/20
FIGURE Engine and Nacelle - Nacelle Dimensions - RR TRENT 700
Apr 01/20
L.E.C.
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
FIGURE Engine and Nacelle - Fan Cowls - RR TRENT 700
FIGURE Engine and Nacelle - Thrust Reverser Cowls - RR TRENT
700
Subject 2-12-1
LAST REVISION
DATE
Apr 01/20
Apr 01/20
Auxiliary Power Unit
Apr 01/20
FIGURE Auxiliary Power Unit - Access Doors
Apr 01/20
Subject 2-13-0
Leveling and Symmetry
Jun 01/20
FIGURE Location of Leveling Points
Apr 01/20
Subject 2-14-0
Jacking for Maintenance
Apr 01/20
FIGURE Jacking for Maintenance - Jacking Points Layout and
Maximum Jacking Force
Apr 01/20
FIGURE Jacking for Maintenance - Ground Clearance on Jacks
FIGURE Jacking for Maintenance - Jacking Point Adaptors
R
Jul 01/21
Apr 01/20
Subject 2-14-1
Jacking of the Landing Gear
Apr 01/20
FIGURE Jacking of the Landing Gear - Jacking of the Landing Gear
Apr 01/20
FIGURE Jacking of the Landing Gear
Apr 01/20
CHAPTER 4
Subject 4-1-0
General Information
Apr 01/20
Subject 4-2-0
Turning Radii
Apr 01/20
FIGURE Turning Radii - (Sheet 1)
Apr 01/20
FIGURE Turning Radii - (Sheet 2)
Apr 01/20
Subject 4-3-0
Minimum Turning Radii
Apr 01/20
FIGURE Minimum Turning Radii
Apr 01/20
L.E.C.
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
LAST REVISION
DATE
Subject 4-4-0
Visibility from Cockpit in Static Position
Apr 01/20
FIGURE Visibility from Cockpit in Static Position
Apr 01/20
FIGURE Binocular Visibility Through Windows from Captain Eye
Position
Subject 4-5-0
Runway and Taxiway Turn Paths
Apr 01/20
Apr 01/20
Subject 4-5-1
135˚ Turn - Runway to Taxiway
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental Oversteer
Method
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over Centerline
Method
Subject 4-5-2
90˚ Turn - Runway to Taxiway
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental Oversteer
Method
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over Centerline
Method
Subject 4-5-3
Apr 01/20
Apr 01/20
Apr 01/20
Apr 01/20
Apr 01/20
Apr 01/20
180˚ Turn on a Runway
Apr 01/20
FIGURE 180˚ Turn on a Runway
Apr 01/20
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway
FIGURE 135˚ Turn - Taxiway to Taxiway - Judgemental Oversteer
Method
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline
Method
Subject 4-5-5
Apr 01/20
Apr 01/20
Apr 01/20
90˚ Turn - Taxiway to Taxiway
Apr 01/20
FIGURE 90˚ Turn - Taxiway to Taxiway - Judgemental Oversteer
Method
Apr 01/20
L.E.C.
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline
Method
Subject 4-6-0
CHG
CODE
LAST REVISION
DATE
Apr 01/20
Runway Holding Bay (Apron)
Apr 01/20
FIGURE Runway Holding Bay (Apron)
Apr 01/20
Subject 4-7-0
Minimum Line-Up Distance Corrections
Apr 01/20
FIGURE Minimum Line-Up Distance Corrections - 90˚ Turn on
Runway Entry
Apr 01/20
FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn on
Runway Turn Pad
Apr 01/20
FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn on
Runway Width
Apr 01/20
Subject 4-8-0
Aircraft Mooring
Apr 01/20
FIGURE Aircraft Mooring
Apr 01/20
CHAPTER 5
Subject 5-1-2
05-01-02 Typical Ramp Layout
Jun 01/20
FIGURE Typical Ramp Layout
Jun 01/20
Subject 5-4-1
Ground Service Connections Layout
Apr 01/20
FIGURE Ground Service Connections Layout
Apr 01/20
Subject 5-4-2
Grounding (Earthing) Points
Apr 01/20
FIGURE Ground Service Connections - Grounding (Earthing) Points
Apr 01/20
FIGURE Ground Service Connections - Grounding (Earthing) Points
Apr 01/20
FIGURE Ground Service Connections - Grounding (Earthing) Points
Apr 01/20
Subject 5-4-3
Hydraulic System
Apr 01/20
L.E.C.
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
FIGURE
Panel
FIGURE
Panel
FIGURE
Panel
FIGURE
CHG
CODE
Ground Service Connections - Green System Ground Service
LAST REVISION
DATE
Apr 01/20
Ground Service Connections - Blue System Ground Service
Apr 01/20
Ground Service Connections - Yellow System Ground Service
Apr 01/20
Ground Service Connections - RAT
Apr 01/20
Subject 5-4-4
Electrical Servicing
Jun 01/20
FIGURE Ground Service Connections - Electrical Service Panel
Jun 01/20
FIGURE Ground Service Connections - Maintenance Bus-Switch
Location
Subject 5-4-5
Apr 01/20
Oxygen System
Apr 01/20
FIGURE Ground Service Connections - Oxygen Servicing
Apr 01/20
Subject 5-4-6
Fuel System
Apr 01/20
FIGURE Ground Service Connections - Refuel/Defuel Control Panel
Apr 01/20
FIGURE Ground Service Connections - Refuel/Defuel Coupling
Apr 01/20
FIGURE Ground Service Connections - Overpressure Protector and
NACA Flame Arrestor - Wing
Apr 01/20
Subject 5-4-7
Pneumatic System
FIGURE Ground Service Connections - LP and HP Ground
Connectors
Subject 5-4-8
Apr 01/20
Apr 01/20
Oil System
Apr 01/20
FIGURE Ground Service Connections - Engine Oil Tank - RR Trent
700 Series Engine
Apr 01/20
FIGURE Ground Service Connections - IDG Oil Tank - RR Trent 700
Series Engine
Apr 01/20
L.E.C.
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
FIGURE Ground Service Connections - Starter Oil Tank - RR Trent
700 Series Engine
APU Oil Servicing
FIGURE Ground Service Connections - APU Oil Servicing
CHG
CODE
LAST REVISION
DATE
Apr 01/20
Apr 01/20
Apr 01/20
Subject 5-4-10
Waste Water System
FIGURE Ground Service Connections - Waste-Water Ground-Service
Panels
Subject 5-4-11
Jun 01/20
Jun 01/20
Cargo Control Panels
Apr 01/20
FIGURE Lower Cargo Door Operation Panel
Apr 01/20
FIGURE MDCD Control Panel
Apr 01/20
Subject 5-5-0
Engine Starting Pneumatic Requirements
Apr 01/20
FIGURE Engine Starting Pneumatic Requirements - Rolls Royce Trent
700 Series Engine
Apr 01/20
Subject 5-8-0
Ground Towing Requirements
Jun 01/20
FIGURE Ground Towing Requirements
Apr 01/20
FIGURE Ground Towing Requirements - Location of the RAOs
Jun 01/20
Subject 5-9-0
De-Icing and External Cleaning
Apr 01/20
FIGURE De-Icing and External Cleaning
Apr 01/20
CHAPTER 6
Subject 6-1-0
Engine Exhaust Velocities and Temperatures
Apr 01/20
Subject 6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power
Apr 01/20
FIGURE Engine Exhaust Velocities - Ground Idle Power - RR Trent
700 Series Engine
Apr 01/20
L.E.C.
Page 7
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
LAST REVISION
DATE
Subject 6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power
Apr 01/20
FIGURE Engine Exhaust Temperatures - Ground Idle Power - RR
Trent 700 Series Engine
Apr 01/20
Subject 6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
Apr 01/20
FIGURE Engine Exhaust Velocities - Breakaway Power - RR Trent
700 Series Engine
Apr 01/20
Subject 6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power
Apr 01/20
FIGURE Engine Exhaust Temperatures - Breakaway Power - RR
Trent 700 Series Engine
Apr 01/20
Subject 6-1-5
Engine Exhaust Velocities Contours - Takeoff Power
Apr 01/20
FIGURE Engine Exhaust Velocities - Takeoff Power - RR Trent 700
Series Engine
Apr 01/20
Subject 6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power
Apr 01/20
FIGURE Engine Exhaust Temperatures - Takeoff Power - RR Trent
700 Series Engine
Apr 01/20
Subject 6-3-0
Danger Areas of Engines
Apr 01/20
Subject 6-3-1
Ground Idle Power
Apr 01/20
FIGURE Danger Areas of Engines - RR Trent 700 Series Engine
Apr 01/20
Subject 6-3-2
Breakaway Power
Apr 01/20
FIGURE Danger Areas of Engines - RR Trent 700 Series Engine
Apr 01/20
Subject 6-3-3
Take-Off Power
Apr 01/20
FIGURE Danger Areas of Engines - RR Trent 700 Series Engine
Apr 01/20
L.E.C.
Page 8
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
CODE
LAST REVISION
DATE
Subject 6-4-0
APU Exhaust Velocities and Temperatures
Apr 01/20
Subject 6-4-1
APU - GARRETT
FIGURE Exhaust Velocities and Temperatures - APU -- GARRETT
GTCP 331-350
Subject 6-5-0
Apr 01/20
Apr 01/20
Pilot Visibility in Approach
Jun 01/20
FIGURE Pilot Visibility in Approach - Navigation Aids
Jun 01/20
CHAPTER 7
Subject 7-1-0
General Information
Apr 01/20
Subject 7-2-0
Landing Gear Footprint
Apr 01/20
FIGURE Landing Gear Footprint
Apr 01/20
Subject 7-3-0
Maximum Pavement Loads
Apr 01/20
FIGURE Maximum Pavement Loads
Apr 01/20
Subject 7-4-0
Landing Gear Loading on Pavement
Apr 01/20
FIGURE Landing Gear Loading on Pavement - WVZCG -0.5 m, MRW
227 900 kg, CG 28.2%
Apr 01/20
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of Engineers
Design Method
Apr 01/20
FIGURE Flexible Pavement Requirements - WVZCG -0.5 m, WVZCG
-0.4 m, WVZCG 0 m, MRW 227 900 kg, CG 28.2%
Apr 01/20
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion
Apr 01/20
Subject 7-7-0
L.E.C.
Page 9
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
Rigid Pavement Requirements - Portland Cement Association Design
Method
FIGURE Rigid Pavement Requirements - WVZCG -0.5 m, WVZCG
-0.4 m, WVZCG 0 m, MRW 227 900 kg, CG 28.2%
CHG
CODE
LAST REVISION
DATE
Apr 01/20
Apr 01/20
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion
Apr 01/20
Subject 7-9-0
Aircraft Classification Number - Flexible and Rigid Pavements
Apr 01/20
FIGURE Aircraft Classification Number - ACN Table
Apr 01/20
FIGURE Aircraft Classification Number - Flexible Pavement - WVZCG
-0.5 m, WVZCG -0.4 m, WVZCG 0 m, MRW 227 900 kg, CG 28.2%
Apr 01/20
FIGURE Aircraft Classification Number - Flexible Pavement - WVZCG
0.4 m, MRW 227 900 kg, CG 26%
Apr 01/20
FIGURE Aircraft Classification Number - Flexible Pavement - WVZCG
0.6 m, MRW 202 300 kg, CG 28.2%
Apr 01/20
CHAPTER 8
Subject 8-0-0
Scaled Drawings
Apr 01/20
FIGURE Scaled Drawing
Apr 01/20
CHAPTER 10
Subject 10-0-0
Aircraft Rescue and Fire Fighting
Jun 01/20
FIGURE Front Page
Apr 01/20
FIGURE Highly Flammable and Hazardous Materials and Components
Jun 01/20
FIGURE Batteries Location and Access
Apr 01/20
FIGURE Wheel/Brake Overheat - Wheel Safety Area
Jun 01/20
FIGURE Ground Lock Safety-Devices
Apr 01/20
FIGURE Emergency Evacuation Devices
Jun 01/20
FIGURE Sliding Windows Evacuation
Jun 01/20
FIGURE Belly-Door Exterior Control-Handle
Jun 01/20
L.E.C.
Page 10
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
FIGURE Belly-Door Interior Control-Handle
CHG
CODE
LAST REVISION
DATE
Jun 01/20
FIGURE Pressure Bulkhead Door
Jun 01/20
FIGURE Main-Deck Access Door
Jun 01/20
FIGURE Aft-Cargo-Compartment Door Controls
Apr 01/20
FIGURE Main-Deck Cargo Door-Control
Jun 01/20
FIGURE Control Panels
Jun 01/20
FIGURE APU Air Intake
Jun 01/20
FIGURE Ground Clearances
Apr 01/20
FIGURE Structural Break-in Points
Jun 01/20
L.E.C.
Page 11
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TABLE OF CONTENTS
1
1-1-0
1-2-1
SCOPE
Purpose
Glossary
2
AIRCRAFT DESCRIPTION
2-1-1
General Aircraft Characteristics Data
2-2-0
General Aircraft Dimensions
2-3-0
Ground Clearances
2-4-1
Interior Arrangements - Plan View
2-6-1
Lower Deck Cargo Compartments
2-6-2
Main Deck Cargo Compartments
2-6-3
Main and Lower Deck Cross-sections
2-7-0
Door Clearances
2-9-0
Landing Gear
2-10-0
Exterior Lighting
2-11-0
Antennas and Probes Location
2-12-0
Engine and Nacelle
2-12-1
Auxiliary Power Unit
2-13-0
Levelling, symmetry and Alignment
2-14-0
Jacking for Maintenance
2-14-1
Jacking of the Landing Gear
4
4-1-0
4-2-0
4-3-0
4-4-0
4-5-0
4-5-1
4-5-2
4-5-3
4-5-4
4-5-5
4-6-0
4-7-0
GROUND MANEUVERING
General Information
Turning Radii
Minimum Turning Radii
Visibility from Cockpit in Static Position
Runway and Taxiway Turn Paths
135˚ Turn - Runway to Taxiway
90˚ Turn - Runway to Taxiway
180˚ Turn on a Runway
135˚ Turn - Taxiway to Taxiway
90˚ Turn - Taxiway to Taxiway
Runway Holding Bay (Apron)
Minimum Line-Up Distance Corrections
T.O.C.
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-8-0
Aircraft Mooring
5
TERMINAL SERVICING
5-1-2
Typical Ramp Layout - Open Apron
5-4-1
Ground Service Connections Layout
5-4-2
Grounding Points
5-4-3
Hydraulic System
5-4-4
Electrical System
5-4-5
Oxygen System
5-4-6
Fuel System
5-4-7
Pneumatic System
5-4-8
Oil System
5-4-10
Waste Water System
5-4-11
Cargo Control Panels
5-5-0
Engine Starting Pneumatic 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
6-1-6
6-3-0
6-3-1
6-3-2
6-3-3
6-4-0
6-4-1
6-5-0
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
Danger Areas of Engines
Ground Idle Power
Breakaway Power
Takeoff Power
APU Exhaust Velocities and Temperatures
APU
Pilot Visibility in Approach
7
7-1-0
7-2-0
7-3-0
PAVEMENT DATA
General Information
Landing Gear Footprint
Maximum Pavement Loads
T.O.C.
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0
7-5-0
7-6-0
7-7-0
7-8-0
7-9-0
8
8-0-0
Landing Gear Loading on Pavement
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
Flexible Pavement Requirements - LCN Conversion
Rigid Pavement Requirements - Portland Cement Association Design Method
Rigid Pavement Requirements - LCN Conversion
ACN/PCN Reporting System - Flexible and Rigid Pavements
SCALED DRAWINGS
SCALED DRAWINGS
10
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0
AIRCRAFT RESCUE AND FIRE FIGHTING
T.O.C.
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0
Purpose
**ON A/C A330-700L
Introduction
1.
The A330-700L AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(AC) manual is issued for the A330-700L to give necessary data to airport operators, airlines and
Maintenance/Repair Organizations (MRO) for airport and maintenance facilities planning.
The A330-700L is designed to replace the existing A300-600ST known as Beluga, to modernize and
improve Airbus aircraft parts transportation. The A330-700L will offer a large volume in its main
deck cargo compartment, which can carry a pair of A350 wings.
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
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1-2-1
Glossary
**ON A/C A330-700L
Glossary
1. List of Abbreviations
A/C
AC
ACN
AMM
APU
C/L
CBR
CC
CG
CKPT
E
ELEC
ESWL
FAA
FDL
FR
FSTE
FWD
GPU
GSE
HYD
ICAO
IDG
ISA
L
LCN
LD
LD
LDG
LH
LMLG
MAC
MAX
Aircraft
Aircraft Characteristics manual
Aircraft Classification Number
Aircraft Maintenance Manual
Auxiliary Power Unit
Center Line
California Bearing Ratio
Cargo Compartment
Center of Gravity
Cockpit
Young’s Modulus
Electric, Electrical, Electricity
Equivalent Single Wheel Load
Federal Aviation Administration
Fuselage Datum Line
Frame
Full Size Trolley Equivalent
Forward
Ground Power Unit
Ground Support Equipment
Hydraulic
International Civil Aviation Organisation
Integrated Drive Generator
International Standard Atmosphere
Radius of relative stiffness
Load Classification Number
Load Device
Lower Deck
Landing Gear
Left Hand
Left Main Landing Gear
Mean Aerodynamic Chord
Maximum
1-2-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
MD
MDCC
MIN
MLG
NLG
OAT
PCA
PCN
RH
RMLG
ULD
WV
2.
Main Deck
Main Deck Cargo Compartment
Minimum
Main Landing Gear
Nose Landing Gear
Outside Air Temperature
Portland Cement Association
Pavement Classification Number
Right Hand
Right Main Landing Gear
Unit Load Device
Weight Variant
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 Take-Off Weight (MTOW):
Maximum weight for take-off 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.
- 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.
1-2-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-1
General Aircraft Characteristics Data
**ON A/C A330-700L
General Aircraft Characteristics Data
1.
The following table gives characteristics of A330-700L model, these data are specific to each weight
variant:
Aircraft Characteristics
WV000
WV001
227 900 kg
205 900 kg
Maximum Ramp Weight (MRW)
(502 433 lb)
(453 932 lb)
227 000 kg
205 000 kg
Maximum Take-Off Weight
(500 449 lb)
(451 948 lb)
(MTOW)
Maximum Landing Weight
187 000 kg
187 000 kg
(MLW)
(412 264 lb)
(412 264 lb)
Maximum Zero Fuel Weight
178 000 kg
178 000 kg
(MZFW)
(392 423 lb)
(392 423 lb)
50 500 kg
50 500 kg
Estimated Maximum Payload
(111 333 lb)
(111 333 lb)
127 500 kg
127 500 kg
Operating Weight Empty (OWE)
(281 089 lb)
(281 089 lb)
2.
The following table gives characteristics of A330-700L model, these data are common to each weight
variant:
Aircraft Characteristics
4
Seats in courier area
73 000 kg
Usable Fuel Capacity
(160 937 lb)
(density = 0.785 kg/l)
Pressurized Fuselage Volume
87.4 m3
(3087 ft3)
Cockpit Volume
5.75 m3
(203 ft3)
Main-Deck Cargo-Compartment Water Volume
2 209 m3
(78 010 ft3)
Usable Volume, AFT CC
60.7 m3
(2 144 ft3)
Usable Volume, Bulk CC
19.7 m3
(696 ft3)
2-1-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics
85.7 m3
(3 026 ft3)
22.7 m3
(802 ft3)
Water Volume, AFT CC
Water Volume, Bulk CC
2-1-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0
General Aircraft Dimensions
**ON A/C A330-700L
General Aircraft Dimensions
1.
This section gives general aircraft dimensions.
2-2-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
11.1 m
(36.42 ft)
19.4 m
(63.65 ft)
30.2 m
(99.08 ft)
16.4 m
(53.81 ft)
29 m
(95.14 ft)
21.1 m
(69.23 ft)
2.5 m
(8.20 ft)
62.5 m
(205.05 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
F_AC_020200_1_0130101_01_00
General Aircraft Dimensions
(Sheet 1 of 2)
FIGURE-2-2-0-991-013-A01
2-2-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
62.5 m
(205.05 ft)
8.2 m
(26.90 ft)
22.2 m
(72.83 ft)
13.8 m
(45.28 ft)
10.5 m
(34.45 ft)
3.1 m
(10.17 ft)
61.2 m
(200.79 ft)
63.1 m
(207.02 ft)
60.3 m
(197.83 ft)
7.7 m
(25.26 ft)
19.4 m
(63.65 ft)
58 m
(190.29 ft)
8.8 m
(28.87 ft)
10.7 m
(35.10 ft)
18.7 m
(61.35 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
F_AC_020200_1_0130102_01_00
General Aircraft Dimensions
(Sheet 2 of 2)
FIGURE-2-2-0-991-013-A01
2-2-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0
Ground Clearances
**ON A/C A330-700L
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 can change with tire type, weight and balance and other special conditions.
NOTE : Tire pressure and shock absorbers are fixed in the standard condition.
The dimensions are given for the weight variant WV000:
- A light weight 135 000 kg (297 624 lb), with a FWD CG and an AFT CG,
- An aircraft at MRW 227 000 kg (500 449 lb) with a FWD CG and an AFT CG,
- A minimum weight at Operating Weight Empty (OWE) 127 500 kg (281 089 lb) with aligned
CG,
- Aircraft on jacks, FDL at 6.515 m (21.37 ft).
NOTE : Cargo door ground clearances are measured from the floor level.
2-3-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
VT AP HT
W1 W2
C2 C1
F2
BF3
BF2
MRW 227 000 kg (500 450 lb)
A/C CONFIGURATION
FWD CG (20.5%) AFT CG (28%)
FOR WV000
m
m
ft
ft
12.90
42.32
12.94 42.45
F2
1.20
3.94
1.27
4.17
F1
17.10
56.10
17.18 56.36
D1
12.28
40.29
12.35 40.52
D2
FUSELAGE
5.09
16.70
5.01
16.44
D3
3.69
12.11
3.76
12.34
CP1
1.94
6.36
1.95
6.40
BF1
1.93
6.33
1.93
6.33
BF2
1.95
6.40
1.94
6.36
BF3
6.84
22.44
6.74
22.11
HT
7.39
24.25
7.28
23.88
AP
18.89
61.98
18.79 61.65
VT
3.03
9.94
3.07
10.07
C1
DOORS
3.10
10.17
3.05
10.01
C2
7.94
26.05
7.91
25.95
W1
WINGS
6.58
21.59
6.54
21.46
W2
0.88
2.89
0.89
2.92
ENGINE
N1
N1 BF1
D3
D2 D1
F1
CP1
135 000 kg (297 625 lb)
FWD CG (18%)
m
ft
13.02
42.72
1.28
4.20
17.18
56.36
12.37
40.58
16.70
5.09
3.77
12.37
2.11
6.92
2.11
6.92
2.15
7.05
7.16
23.49
7.71
25.30
19.21
63.02
10.86
3.31
3.36
11.02
8.18
26.84
6.81
22.34
1.04
3.41
NOTE:
CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM FLOOR LEVEL.
THE VALUES GIVEN IN THE TABLE DEPEND ON THE POSITION OF
THE CENTER OF GRAVITY (CG) AND ON THE AIRCRAFT WEIGHT.
AFT CG (25%)
m
ft
13.06 42.85
1.35
4.43
17.25 56.59
12.43 40.78
5.16
16.93
3.84
12.60
2.12
6.96
2.11
6.92
2.14
7.02
7.06
23.16
7.60
24.93
19.10 62.66
3.27
10.73
3.30
10.83
8.14
26.71
6.77
22.21
1.05
3.44
F_AC_020300_1_0450101_01_01
Ground Clearances
Ground Clearances for WV000 at MRW and 135 000 kg (297 624 lb) (Sheet 1 of 2)
FIGURE-2-3-0-991-045-A01
2-3-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
OWE 127 500 kg (281 089 lb)
CG (23.5%)
A/C CONFIGURATION
FUSELAGE
DOORS
WINGS
ENGINE
F2
F1
D1
D2
D3
CP1
BF1
BF2
BF3
HT
AP
VT
C1
C2
W1
W2
N1
m
ft
13.04
1.34
17.24
12.43
5.16
3.83
2.13
2.13
2.17
7.14
7.66
19.17
3.27
3.31
8.19
6.84
1.06
42.78
4.40
56.56
40.78
16.93
12.57
6.99
6.99
7.12
23.43
25.13
62.89
10.73
10.86
26.87
22.44
3.48
NOTE:
CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM FLOOR LEVEL.
THE VALUES GIVEN IN THE TABLE DEPEND ON THE POSITION OF
THE CENTER OF GRAVITY (CG) AND ON THE AIRCRAFT WEIGHT.
F_AC_020300_1_0450102_01_01
Ground Clearances
Ground Clearances for WV000 at 127 500 kg (281 089 lbs) (Sheet 2 of 2)
FIGURE-2-3-0-991-045-A01
2-3-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
D
C
B
A
FLAP TRACKS RETRACTED
AIRCRAFT
TYPE
MRW
CG 20.5%
DESCRIPTION
m
MRW
CG 28%
ft
m
ft
FLAP TRACK 2 A
3.75
12.30
3.74
12.27
FLAP TRACK 3 B
4.26
13.98
4.25
13.94
FLAP TRACK 4 C
4.51
14.80
4.49
14.73
FLAP TRACK 5 D
4.88
16.01
4.85
15.91
A330−700L
NOTE:
THE VALUES GIVEN IN THE TABLE DEPEND ON THE POSITION OF
THE CENTER OF GRAVITY (CG) AND ON THE AIRCRAFT WEIGHT.
F_AC_020300_1_0470101_01_01
Ground Clearances
Ground Clearances for Flaps Retracted with WV000
FIGURE-2-3-0-991-047-A01
2-3-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
D
C
B
A
FLAP TRACKS 1+F
AIRCRAFT
TYPE
MRW
CG 20.5%
DESCRIPTION
m
MRW
CG 28%
ft
m
ft
FLAP TRACK 2 A
3.48
11.42
3.37
11.06
FLAP TRACK 3 B
3.99
13.09
3.88
12.73
FLAP TRACK 4 C
4.24
13.91
4.12
13.52
FLAP TRACK 5 D
4.61
15.12
4.48
14.70
A330−700L
NOTE:
THE VALUES GIVEN IN THE TABLE DEPEND ON THE POSITION OF
THE CENTER OF GRAVITY (CG) AND ON THE AIRCRAFT WEIGHT.
F_AC_020300_1_0480101_01_01
Ground Clearances
Ground Clearances for Flaps in Intermediate Position with WV000
FIGURE-2-3-0-991-048-A01
2-3-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
D
C
B
A
FLAP TRACKS EXTENDED
AIRCRAFT
TYPE
MRW
CG 20.5%
DESCRIPTION
MRW
CG 28%
m
ft
m
ft
FLAP TRACK 2 A
2.82
9.25
2.81
9.22
FLAP TRACK 3 B
3.33
10.93
3.32
10.89
FLAP TRACK 4 C
3.58
11.75
3.56
11.68
FLAP TRACK 5 D
3.95
12.96
3.92
12.86
A330−700L
NOTE:
THE VALUES GIVEN IN THE TABLE DEPEND ON THE POSITION OF
THE CENTER OF GRAVITY (CG) AND ON THE AIRCRAFT WEIGHT.
F_AC_020300_1_0490101_01_01
Ground Clearances
Ground Clearances for Flaps Fully Extended with WV000
FIGURE-2-3-0-991-049-A01
2-3-0
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1
Interior Arrangements - Plan View
**ON A/C A330-700L
Interior Arrangements - Plan View
1.
This section gives the interior configuration of courier area showing the width of passway.
2-4-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
EXIT
0.610 m
(2.00 ft)
0.470 m
(1.54 ft)
0.508 m
(1.67 ft)
EXIT
EXIT
0.200 m
(0.66 ft)
FWD
NOTE:
SEAT
LAVATORY
COURIER AREA
F_AC_020401_1_0100101_01_00
Interior Arrangements - Plan View
FIGURE-2-4-1-991-010-A01
2-4-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-1
Lower Deck Cargo Compartments
**ON A/C A330-700L
Lower Deck Cargo Compartments
1.
This section gives the following data about lower deck cargo compartments:
- Location and dimensions
- Loading combinations.
2-6-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FR53.2
FR65
LOWER DECK
AFT CARGO
COMPARTMENT
FR73
LOWER DECK
BULK CARGO
COMPARTMENT
0.95 m
(3.12 ft)
2.78 m
(9.12 ft)
12.32 m
(40.42 ft)
4.04 m
(13.25 ft)
F_AC_020601_1_0130101_01_00
Lower Deck Cargo Compartments
Location and Dimensions (Sheet 1 of 2)
FIGURE-2-6-1-991-013-A01
2-6-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
14 LD3 60.4 in X 61.5 in
5 PALLETS 88 in X 125 in
4 PALLETS 96 in X 125 in
F_AC_020601_1_0130102_01_00
Lower Deck Cargo Compartments
Loading Combinations (Sheet 2 of 2)
FIGURE-2-6-1-991-013-A01
2-6-1
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-2
Main Deck Cargo Compartments
**ON A/C A330-700L
Main Deck Cargo Compartment
1.
This section gives the following data about the main-deck cargo compartment:
- Location and dimensions.
2-6-2
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
51.34 m
(168.44 ft)
46.56 m
(152.76 ft)
45.56 m
(149.48 ft)
43.09 m
(141.37 ft)
PLU−01
5.79 m
(19.00 ft)
START OF
ROLLERTRACK
37.10 m
(121.72 ft)
PLU−36
39.56 m
(129.79 ft)
41.16 m
(135.04 ft)
MAIN DECK
CARGO COMPARTMENT
END OF ROLLERTRACK
F_AC_020602_1_0070101_01_00
Main-Deck Cargo Compartment
Location and Dimensions
FIGURE-2-6-2-991-007-A01
2-6-2
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-3
Main and Lower Deck Cross-sections
**ON A/C A330-700L
Main and Lower Deck Cross-sections
1.
This section gives main and lower deck cross-sections for cargo version.
2-6-3
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
REFERENCE CARGO CONFIGURATION LAYOUT
AMF
96" x 125"
LD9
88" x 125"
OPTIONAL CARGO CONFIGURATIONS
LD6 / AAF
CONTAINER
AKE
AKE
ALF / AAF / AMF
CONTAINER
LD3
LD3
88" x 125"
PALLET
F_AC_020603_1_0020101_01_00
Lower-Deck Cargo Cross-sections
FIGURE-2-6-3-991-002-A01
2-6-3
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
CLEARANCE ENVELOPE
A350 FUSELAGE
PAIR OF A350 WINGS
F_AC_020603_1_0030101_01_00
Main-Deck-Cargo Arrangement Cross-sections
FIGURE-2-6-3-991-003-A01
2-6-3
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0
Door Clearances
**ON A/C A330-700L
Door Clearances
1.
This section gives door location, identification and clearances.
2-7-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
MAIN DECK
COMPARTMENT DOOR
CARGO
ACCESS DOOR
COCKPIT
SLIDING
WINDOWS
BULK CARGO
COMPARTMENT DOOR
BELLY DOOR
AFT CARGO
COMPARTMENT DOOR
PRESSURE
BULKHEAD DOOR
42.67 m
(139.99 ft)
11.52 m
(37.80 ft)
45.65 m
(149.77 ft)
11.67 m
(38.29 ft)
3.27 m
(10.73 ft)
0.51 m
(1.67 ft)
60?
7.85 m
(25.75 ft)
F_AC_020700_1_0550101_01_00
Lateral Position of Doors from Aircraft Nose
FIGURE-2-7-0-991-055-A01
2-7-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
2.30 m
(7.55 ft)
2.02 m
(6.63 ft)
10.80 m
(35.43 ft)
12.30 m
(40.35 ft)
FLIGHT DATUM LINE
2.221 m
(7.29 ft)
FR1
1.32 m
(4.33 ft)
1.25 m
(4.10 ft)
67?
1.65 m
(5.41 ft)
F_AC_020700_1_0560101_01_00
Radome
FIGURE-2-7-0-991-056-A01
2-7-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A330−700L: 42.7 m (140.09 ft)
(FROM NOSE)
A
2.78 m
(9.12 ft)
SEE 02−03−00
A
2.03 m
(6.66 ft)
1.68 m
(5.51 ft)
5.19 m
(17.03 ft)
A A
F_AC_020700_1_0570101_01_00
Aft Cargo-Compartment Door
FIGURE-2-7-0-991-057-A01
2-7-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A330−700L: 45.65 m (149.77 ft)
(FROM NOSE)
A
SEE 02−03−00
0.95 m
(3.12 ft)
1.11 m
(3.64 ft)
A
FWD
1.41 m
(4.63 ft)
1.07 m
(3.51 ft)
A A
F_AC_020700_1_0580101_01_00
Bulk Cargo-Compartment Door
FIGURE-2-7-0-991-058-A01
2-7-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
A/C C
L
1.56 m
(5.12 ft)
Z−2.00 m (6.56 ft)
3.03 m
(9.94 ft)
81?
2.34 m
(7.68 ft)
1.10 m
(3.61 ft)
2.70 m
(8.86 ft)
SEE 02−03−00 01
GROUND LINE
A
RH SHOWN
LH SYMMETRICAL
NOTE:
01 DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.
F_AC_020700_1_0590101_01_00
MLG Doors
FIGURE-2-7-0-991-059-A01
2-7-0
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0
Landing Gear
**ON A/C A330-700L
Landing Gear
1.
General
All dimensions shown are minimum dimensions with zero clearances.
Dimensions for elevators and related mechanisms must be added to the following figures.
A.
Elevators
These can be either mechanical or hydraulic. Elevators are used to:
- Let easy movement of persons and equipment around the main landing gears
- Lift and remove the 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. Jacks must be
installed and engaged with all the jacking points (Ref. Section 2-14 for Jacking).
Jacks must support the total aircraft weight i.e. when the landing gears do not touch the
elevators on retraction/extension tests.
When tripod support jacks are used, the tripod-base circle radius must be small because the
locations required for positioning the jacks are close to the sides of the pits.
2-9-0
Page 1
Jul 01/21
2-9-0
32.62 m
(107.02 ft)
NOTE:
ENVELOPES SHOWN WITH ZERO CLEARANCE TO OUTSIDE EDGE OF TIRES.
FRONT OF NOSE
6.31 m
(20.70 ft)
AIRCRAFT CENTER LINE
22.15 m
(72.67 ft)
3.65 m
(11.98 ft)
3.89 m
(12.76 ft)
5.34 m
(17.52 ft)
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_020900_1_0210101_01_00
Landing Gear Position
FIGURE-2-9-0-991-021-A01
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
HINGED DOOR
FIXED FAIRING DOOR
A
B
SHORTENING
MECHANISM
MAIN DOOR
(HYDRAULICALLY
OPERATED)
LH SHOWN
RH SYMMETRICAL
D
C
DOWNLOCK
ACTUATOR
SIDE STAY
ASSEMBLY
MLG LEG
ASSEMBLY
F
BOGIE PITCH
TRIMMER
ARTICULATING LINKS
TORQUE LINKS
AFT AXLE
SHOCK ABSORBER
BOGIE BEAM
ASSEMBLY
E
FWD AXLE
BRAKE ROD
ASSEMBLY
RADIAL OR BIAS
PLY TIRES
A
F_AC_020900_1_0220101_01_00
Main Landing Gear
(Sheet 1 of 3)
FIGURE-2-9-0-991-022-A01
2-9-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
QUICK RELEASE PIN
WARNING FLAG
DOOR ACTUATOR
QUICK RELEASE PIN
WARNING FLAG
SAFETY
COLLAR
B
GROUND LOCK PIN
WARNING FLAG
LOCK STAY
C
F_AC_020900_1_0220102_01_00
Main Landing Gear
Mechanical locking of MLG (Sheet 2 of 3)
FIGURE-2-9-0-991-022-A01
2-9-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
BLEED/INFLATION
VALVE
SEAL CHANGEOVER
VALVE
FILL VALVE
D
GROUND POINT
E
FWD
F
F_AC_020900_1_0220103_01_00
Main Landing Gear
MLG Servicing (Sheet 3 of 3)
FIGURE-2-9-0-991-022-A01
2-9-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FWD DOORS
(HYDRAULICALLY
OPERATED)
B
AFT DOOR
(MECHANICALLY OPERATED)
B
AFT DOOR
(MECHANICALLY OPERATED)
A
RETRACTION ACTUATOR
DOWNLOCK
ACTUATOR
D
UPPER DRAGSTAY
(FOLDING STRUT)
C
MAIN FITTING
LOWER DRAGSTAY
(FOLDING STRUT)
DOWNLOCK SPRINGS
H
E
NWS ACTUATORS
TORQUE LINKS
F
AXLE
G
SHOCK ABSORBER
RADIAL OR BIAS
PLY TIRES
TOWING BRACKET
A
F_AC_020900_1_0230101_01_00
Nose Landing Gear
(Sheet 1 of 4)
FIGURE-2-9-0-991-023-A01
2-9-0
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
QUICK RELEASE PIN
WARNING FLAG
DOOR ACTUATOR
QUICK RELEASE PIN
WARNING FLAG
SAFETY
COLLAR
B
RH SHOWN
LH SYMMETRICAL
DOWN LOCK
ACTUATOR
ATTACHMENT
UPPER
LOCK−LINK
LOWER
LOCK−LINK
LOCK SPRING
ATTACHMENT
GROUND
LOCK PIN
WARNING FLAG
DRAG STAY
ATTACHMENT
C
F_AC_020900_1_0230102_01_00
Nose Landing Gear
Mechanical Locking of NLG (Sheet 2 of 4)
FIGURE-2-9-0-991-023-A01
2-9-0
Page 7
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
INFLATION VALVE
(FIRST STAGE)
D
FWD
CHARGE VALVE
SEAL CHANGEOVER
VALVE
BLEED VALVE
E
F_AC_020900_1_0230103_01_00
Nose Landing Gear
NLG Servicing 1 (Sheet 3 of 4)
FIGURE-2-9-0-991-023-A01
2-9-0
Page 8
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
INFLATION VALVE
(SECOND STAGE)
F
FWD
GROUND POINT
TOWING LEVER
NORMAL POSITION
(NOSE WHEEL STEERING
OPERATIONAL)
LANDING GEAR
G
WARNING FLAG
TOWING POSITION
(NOSE WHEEL STEERING
DEACTIVATED)
SAFETY PIN
(TOWING POSITION)
H
F_AC_020900_1_0230104_01_00
Nose Landing Gear
NLG Servicing 2 (Sheet 4 of 4)
FIGURE-2-9-0-991-023-A01
2-9-0
Page 9
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ELECTRIC BOX
(NLG OVERSTEER WARNING)
8GH
CONNECTOR
8GHB
B
A
8G
H
TOW−TRUCK POWER CABLE 01
A
CONNECTOR
5GCB
ELECTRICAL
DEACTIVATION BOX
5GC
TOW−TRUCK POWER CABLE
WARNING FLAG
SAFETY PIN
B
NOTE:
01 CONNECT THE TOW−TRUCK POWER CABLE TO CONNECTOR 8GHB IF ELECTRICAL BOX
8GH IS INSTALLED ON THE AIRCRAFT.
F_AC_020900_1_0240101_01_00
Tow Truck Power
NLG Servicing 3
FIGURE-2-9-0-991-024-A01
2-9-0
Page 10
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0
Exterior Lighting
**ON A/C A330-700L
Exterior Lighting
1.
General
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
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)
WING SCAN LIGHTS
WING STROBE LIGHT (HIGH INTENSITY,
WHITE)
TAIL STROBE LIGHT (HIGH INTENSITY,
WHITE)
LANDING LIGHTS
RUNWAY TURN-OFF LIGHTS
TAXI LIGHTS
TAKE-OFF LIGHTS
CARGO-COMPARTMENT FLOOD LIGHTS
2-10-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
4
1 RH
2 LH
6
7
8
3
5
F_AC_021000_1_0100101_01_00
Exterior Lighting
Lights General Layout (Sheet 1 of 5)
FIGURE-2-10-0-991-010-A01
2-10-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
11
11
12
9
12
10
F_AC_021000_1_0100102_01_00
Exterior Lighting
Lights General Layout (Sheet 2 of 5)
FIGURE-2-10-0-991-010-A01
2-10-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
TAXIWAY
3
1
2
10
11
12
F_AC_021000_1_0100103_01_00
Exterior Lighting
(Sheet 3 of 5)
FIGURE-2-10-0-991-010-A01
2-10-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
TAXIWAY
8
4
4
7
7
6
6
9
9
F_AC_021000_1_0100104_01_00
Exterior Lighting
(Sheet 4 of 5)
FIGURE-2-10-0-991-010-A01
2-10-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
13
EXAMPLE FOR LIGHT N? 13
CEILING LIGHT
SPOT LIGHT
GROUND
F_AC_021000_1_0100105_01_00
Exterior Lighting
Aft Lower-Cargo light (Sheet 5 of 5)
FIGURE-2-10-0-991-010-A01
2-10-0
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0
Antennas and Probes Location
**ON A/C A330-700L
Antennas and Probes Location
1.
This section gives the location of antennas and probes.
2-11-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
WEATHER RADAR
STBY PITOT PROBE
CAPT PITOT PROBE
CAPT AOA PROBE
CAPT TAT
GPS(1)
GPS(2)
TCAS
ATC(1)/ATC(2)
VHF(1)
VOR
VHF(3)
SATCOM
ELT
LOC
GLIDE
DME(1)
DME(2)
TCAS
FOMAX
MARKER
FOMAX
STATIC PORT
ATC(1)/ATC(2)
VHF(2)
RA(1)
RA(2)
STATIC PORTS
STBY AOA PROBE
F/O AOA PROBE
F/O TAT
STATIC PORTS
F/O PITOT PROBE
F_AC_021100_1_0080101_01_01
Antennas and Probes
Location
FIGURE-2-11-0-991-008-A01
2-11-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0
Engine and Nacelle
**ON A/C A330-700L
Engine and Nacelle
1.
Engine and Nacelle - RR TRENT 700 Engine
A.
Engine
The RB211-TRENT 700 engine is a high bypass ratio, triple spool turbofan.
The principal modules of the engine are:
- The Low Pressure Compressor (LPC) rotor
- The Intermediate Pressure (IP) compressor
- The intermediate case
- The HP system (this includes the High Pressure Compressor (HPC), the combustion system
and the High Pressure Turbine (HPT))
- The Intermediate Pressure Turbine (IPT)
- The external gearbox
- The LPC case
- The Low Pressure Turbine (LPT).
The compressor system has three axial flow compressors in a triple spool configuration. The
compressors are turned independently by their related turbines, each at its most satisfactory
speed.
The LP system has a single-stage compressor installed at the front of the engine. A shaft
connects the compressor to a four-stage turbine at the rear of the gas generator. The gas
generator also includes an eight-stage IP compressor, a six-stage HPC and a combustion system.
Each of the compressors in the gas generator is connected to, and turned by, a different single
stage turbine. Between the HPC and the HPT is the annular combustion system which burns a
mixture of fuel and air to supply energy as heat. Behind the LPT there is a common nozzle
assembly which mixes the cold air and hot gas exhaust flows. The external gearbox module is
installed below the rear case of the fan case. It has a gear train that decreases and increases the
speed to meet the specified drive requirements of each accessory.
B.
Nacelle
The nacelle gives the engine an aerodynamic shape. Each engine is housed in a nacelle
suspended from a pylon attached below the wing. The nacelle consists of the following major
components:
(1) Air Intake Cowl
The air intake cowl is attached to the forward flange of the front LPC case. Its function is
to supply inlet air in a satisfactory condition for the engine compressors.
(2) Fan Cowl Doors
The fan cowl doors hang on the aircraft wing pylon and are closed around the LPC cases.
They can be opened during ground maintenance to give access to the components installed
on the cases and to let the thrust reverser cowl doors be opened.
2-12-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(3) Thrust Reverser
The thrust reverser is a component of the aircraft engine nacelle. The thrust reverser is a
twin thrust reverser cowl door (’C’ duct) construction providing a fan duct inner wall
fairing for the core engine between the top and bottom bifurcation walls. The thrust
reverser incorporates hydraulically-powered actuators to operate four pivoting doors which
redirect the fan air flow in reverse thrust. Hydraulic power is provided from the aircraft
hydraulic system to position the doors in a ”stowed” position for forward thrust and
”deployed” position for reverse thrust.
(4) Common Nozzle Assembly (CNA)
The CNA is attached to the aft flange of the exhaust case. The function of the CNA is to
mix the core engine exhaust with the LPC outlet air.
2-12-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
0.64 m
(2.10 ft)
4.17 m
(13.68 ft)
1.4 m
(4.59 ft)
IP COMPRESSOR
HP COMPRESSOR
HP TURBINE
LP TURBINE
LP COMPRESSOR
TURBINE EXHAUST
NOZZLE
0.81 m
(2.66 ft)
B
0.76 m
(2.49 ft)
1.55 m
(5.09 ft)
IP TURBINE
COMBUSTION
SECTION
1.22 m
(4.00 ft)
EXHAUST
CONE
ACCESSORY DRIVE
SECTION
3.91 m
(12.83 ft)
FWD
A
2.56 m
(8.40 ft)
2.79 m
(9.15 ft)
0.76 m
(2.49 ft)
0.84 m
(2.76 ft)
B
NOTE:
APPROXIMATE DIMENSIONS.
F_AC_021200_1_0300101_01_00
Engine and Nacelle
Engine Dimensions - RR TRENT 700
FIGURE-2-12-0-991-030-A01
2-12-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
7.32 m
(24.02 ft)
1.37 m
(4.49 ft)
1.7 m
(5.58 ft)
2.53 m
(8.30 ft)
NOSE
COWL
FAN COWL
THRUST
REVERSER
A
B
1.73 m
(5.68 ft)
COMMON
NOZZLE
ASSEMBLY
C
3.2 m
(10.50 ft)
1.89 m
(6.20 ft)
2.26 m
(7.41 ft)
C
A
B
3.05 m
(10.01 ft)
3.08 m
(10.10 ft)
2.49 m
(8.17 ft)
WL
100
BL 100
WL
100
BL 100
B B
A A
BL 100
C C
NOTE:
APPROXIMATE DIMENSIONS.
F_AC_021200_1_0310101_01_00
Engine and Nacelle
Nacelle Dimensions - RR TRENT 700
FIGURE-2-12-0-991-031-A01
2-12-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
3.08 m
(10.10 ft)
WL 100
CLOSED
5.84 m
(19.16 ft)
WL 100
FAN COWL
OPEN 55?
1.3 m
(4.27 ft)
2.93 m
(9.61 ft)
SEE 02−03−00
GROUND
NOTE:
APPROXIMATE DIMENSIONS.
F_AC_021200_1_0320101_01_00
Engine and Nacelle
Fan Cowls - RR TRENT 700
FIGURE-2-12-0-991-032-A01
2-12-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
3.08 m
(10.10 ft)
VIEW ON REAR OF
ENGINE
WL 100
CLOSED
5.21 m
(17.09 ft)
WL 100
THRUST
REVERSER
OPEN 43?
0.79 m
(2.59 ft)
1.91 m
(6.27 ft)
2.19 m
(7.19 ft)
0.59 m
(1.94 ft)
SEE 02−03−00
GROUND
NOTE:
APPROXIMATE DIMENSIONS.
F_AC_021200_1_0330101_01_00
Engine and Nacelle
Thrust Reverser Cowls - RR TRENT 700
FIGURE-2-12-0-991-033-A01
2-12-0
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-1
Auxiliary Power Unit
**ON A/C A330-700L
Auxiliary Power Unit
1.
General
The Auxiliary Power Unit (APU) and its related mechanical components are installed at the rear part
of the fuselage in the tailcone section. The APU compartment is a fireproof area (identified as the
Fire Zone).
The APU is a pneumatic and shaft-power gas-turbine engine and is used for the ground and in-flight
power supply of the aircraft.
The APU supplies:
- Mechanical shaft-power to operate a generator
- Bleed-air to the Main Engine Start (MES) and the Environmental Control System (ECS).
A part of the automatic system, with the pneumatic and the electromechanical controls, operates the
start and the acceleration functions of the APU.
An air intake system with a flap-type door is installed in front of the APU compartment. The exhaust
gases pass overboard at the end of the fuselage cone.
2.
Powerplant
The APU is the Garrett Gas-Turbine Compressor Power-unit (GTCP) 331-350C with a single shaft
engine.
The engine is the primary component of the APU, which is of the modular design. The modules of
the engine are:
- The power section
- The load compressor
- The accessory drive gearbox with LRU(s).
The power section has a two-stage centrifugal compressor, a reverse-flow annular combustion
chamber and a three-stage axial turbine. The power section directly operates the one-stage
centrifugal load-compressor which supplies the bleed-air to the pneumatic system. The inlet guide
vanes as part of the load compressor, control the airflow.
The power section also operates the gearbox which is attached to the load compressor. The following
LRU’s are mounted on the gearbox :
- The APU generator,
- The starter motor,
- The oil pump,
- The Fuel Control Unit (FCU),
- The cooling air fan.
The APU has a gearbox-driven oil-cooled AC generator.
The cooling air and ventilation system of the APU supplies the air for cooling of the APU and the
equipment on the APU. It also supplies the air for ventilation of the APU compartment.
2-12-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3.
Control Circuit
The Electronic Control Box (ECB), which controls the FCU and the Inlet Guide Vanes (IGV), keeps
the APU at a constant speed. The control circuit is used to start the APU, to shut it down, to
control it and to prevent internal failure.
4.
Controls and Indication
The primary APU controls and indications are installed in the overhead panel, on the center pedestal
panel and on the forward center panel. External APU panels are also installed on the nose landing
gear and on the refuel/defuel panel, to initiate an APU emergency shut-down.
2-12-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
Z300
A B
FR106A
FR103
FR101
FR95
316AR
FR94
FR92
317AL
FR91
315AL
313AL
A
F_AC_021201_1_0040101_01_00
Auxiliary Power Unit
Access Doors (Sheet 1 of 2)
FIGURE-2-12-1-991-004-A01
2-12-1
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
EXHAUST MUFFLER
FR101
APU
BLEED AIR LINE
FR106A
AIR INTAKE
REAR
FIRE WALL
OIL COOLER OUTLET
AIR INTAKE DUCT
FIRE EXTINGUISHER
BOTTLE
FORWARD
FIRE WALL
FR95
GUTTER
FR92
FIXED DIVERTER
FR90
B
F_AC_021201_1_0040103_01_00
Auxiliary Power Unit
General Layout (Sheet 2 of 2)
FIGURE-2-12-1-991-004-A01
2-12-1
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0
Levelling, symmetry and Alignment
**ON A/C A330-700L
Leveling and Symmetry
1.
Quick Leveling
The quick leveling procedures are documented in AMM.
2.
Precision Leveling
For precise leveling, it is necessary to install sighting rods in the receptacles located under the
fuselage (points 12 and 13 for longitudinal leveling) and under the wings (points 2LH and 2RH for
lateral leveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until the
reference marks on the sighting rods are aligned in the sighting plane (aircraft level).
2-13-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FR57.4 FR58
RIB12
13
2 LH
RIB12
2 RH
12
FR38 FR39
F_AC_021300_1_0080101_01_00
Location of Leveling Points
FIGURE-2-13-0-991-008-A01
2-13-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0
Jacking for Maintenance
**ON A/C A330-700L
Jacking for Maintenance
1.
Aircraft Jacking Points for Maintenance
A.
General
(1) The A330-700L can be jacked:
- At not more than 152 000 kg (335 103 lb),
- Within the limits of the permissible wind speed when the aircraft is jacked outside a
closed environment.
B.
Primary Jacking Points
(1) The aircraft is provided with three primary jacking points:
- One located under the forward fuselage (after FR11),
- Two located under the wings (one under each wing), at the intersection of RIB10 and
the rear of the spar-datum.
(2) Three jack adapters (ground equipment) are used as intermediary parts between the
aircraft jacking points and the jacks:
- One female spherical jack adapter at the forward fuselage,
- Two female spherical jack pad adapters at the wings (one at each wing).
C.
Auxiliary Jacking Point (Safety Stay)
(1) When the aircraft is on jacks, a safety stay is placed under the fuselage at FR87 to prevent
tail tipping caused by accidental displacement of the aircraft center of gravity.
(2) The safety point must not be used for lifting the aircraft.
(3) One male spherical stay adapter (ground equipment) is used as an intermediary part
between the aircraft safety point and the stay.
2.
Jacks and Safety Stay
A.
Jack Design
(1) The maximum eligible loads given in the table are the maximum loads applicable on jack
fittings.
(2) In fully retracted position (jack stroke at minimum), the height of the jack is such that the
jack may be placed beneath the aircraft under the most adverse conditions, namely, tires
deflated and shock absorbers depressurized, with sufficient clearance between the aircraft
jacking point and the jack upper end.
(3) The lifting jack stroke enables the aircraft to be jacked up so that the Fuselage Datum
Line (FDL) may be positioned up to 7.2 m (23.62 ft) from the ground to allow all required
maintenance procedures and in particular, the removal/installation of the landing-gear
shock absorbers.
2-14-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B.
Safety Stay
(1) The stay stroke enables the aircraft tail to be supported up to the FDL positioned 7.2 m
(23.62 ft) from the ground.
2-14-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
X
WING JACKING
POINT
B
X
A
C
Y
FWD FUSELAGE
JACKING POINT
B’
SAFETY STAY
POINT
WING JACKING
POINT
X
X
FORWARD FUSELAGE
JACKING POINT
A
MAXIMUM
JACKING FORCE
Y
m
ft
m
ft
daN
5.3
17.39
0
0
12 686.4
WING JACKING
POINT
B
29.85
97.93
8.51
27.92
71 923.3
B’
29.85
97.93
−8.51
−27.92
71 923.3
SAFETY STAY
C
55.17
181.00
0
0
4 500
NOTE:
SAFETY STAY IS NOT USED FOR JACKING.
F_AC_021400_1_0230101_01_00
Jacking for Maintenance
Jacking Points Layout and Maximum Jacking Force
FIGURE-2-14-0-991-023-A01
2-14-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FLIGHT
DATUM LINE
A
B
C
D
HEIGHT IN m (ft)
A
B
C
D
1.43
(4.69)
4.62
(15.16)
3.82
(12.53)
5.27
(17.29)
1.56
(5.12)
4.60
(15.09)
3.68
(12.07)
5.09
(16.70)
AIRCRAFT ON WHEELS WITH STANDARD
TIRES 01 , OEW 127 000 kg (279 987 lb)
1.52
(4.99)
4.68
(15.35)
3.87
(12.70)
5.31
(17.42)
AIRCRAFT ON WHEELS, NOSE LANDING
GEAR SHOCK ABSORBER DEFLATED
AND FLAT TIRES
1.0
(3.28)
4.68
(15.35)
4.29
(14.07)
5.83
(19.13)
AIRCRAFT ON WHEELS, BOTH MAIN LANDING
GEAR SHOCK ABSORBERS DEFLATED
AND FLAT TIRES
1.61
(5.28)
4.10
(13.45)
2.73
(8.96)
4.04
(13.25)
AIRCRAFT ON WHEELS, NOSE LANDING GEAR
AND LEFT MAIN LANDING GEAR SHOCK
ABSORBERS DEFLATED AND FLAT TIRES
1.06
(3.48)
3.71
(12.17)
5.18
(16.99)
AIRCRAFT ON JACKS, FUSELAGE DATUM
REFERENCE PARALLEL TO GROUND AT
6.51 m (21.36 ft), SHOCK−ABSORBER RELAXED,
CLEARANCE OF MAIN LANDING GEAR WHEELS:
0.24 m (0.79 ft) (STANDARD TIRES 01 ),
CLEARANCE OF NOSE LANDING GEAR WHEELS:
0.96 m (3.15 ft) (STANDARD TIRES 01 )
2.66
(8.73)
4.98
(16.34)
6.42
(21.06)
AIRCRAFT ON WHEELS WITH STANDARD
TIRES 01 , MAX. JACK WEIGHT
152 000 kg (335 103 lb)
(BALANCE 18% MEAN AERODYNAMIC CHORD)
AIRCRAFT ON WHEELS WITH STANDARD
TIRES 01 , MAX. JACK WEIGHT
152 000 kg (335 103 lb)
(BALANCE 34% MEAN AERODYNAMIC CHORD)
(LH)
3.96
(12.99)
(RH)
4.81
(15.78)
5.81
(19.06)
NOTE:
01 STANDARD TIRES: NOSE LANDING GEAR = 1 050 x 395 R16
MAIN LANDING GEAR = 1 400 x 530 R23
F_AC_021400_1_0240101_01_01
Jacking for Maintenance
Ground Clearance on Jacks
FIGURE-2-14-0-991-024-A01
2-14-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
RIB10
FR11
A
B
B
RIB10
NOSE
JACK ADAPTOR
A
WING JACK PAD
ADAPTOR
B
F_AC_021400_1_0250101_01_00
Jacking for Maintenance
Jacking Point Adaptors
FIGURE-2-14-0-991-025-A01
2-14-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-1
Jacking of the Landing Gear
**ON A/C A330-700L
Jacking of the Landing Gear
1.
Not applicable.
2-14-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
NORMAL ATTITUDE
FWD
JACKING POINT
376 mm
(14.80 in)
JACKING POINT
376 mm
(14.80 in)
AFT WHEELS JACKED UP
FWD WHEELS INSTALLED AND INFLATED
FWD
MAX DIAMETER
1 443.7 mm
(56.84 in)
JACKING POINT
570 mm
(22.44 in)
25.4 mm
(1.00 in)
FWD WHEELS JACKED UP
AFT WHEELS INSTALLED AND INFLATED
FWD
JACKING POINT
570 mm
(22.44 in)
25.4 mm
(1.00 in)
F_AC_021401_1_0270101_01_00
Jacking of the Landing Gear
Jacking of the Landing Gear (Sheet 1 of 3)
FIGURE-2-14-1-991-027-A01
2-14-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FWD AXLE
BOTH TIRES SHREDDED OR DEFLATED
FWD
JACKING POINT
376 mm
(14.80 in)
JACKING POINT
145.9 mm
(5.74 in)
AFT AXLE
BOTH TIRES SHREDDED OR DEFLATED
FWD
JACKING POINT
376 mm
(14.80 in)
JACKING POINT
145.5 mm
(5.73 in)
FWD AND AFT AXLE
BOTH TIRES SHREDDED OR DEFLATED
FWD
JACKING POINT
157 mm
(6.18 in)
JACKING POINT
157 mm
(6.18 in)
F_AC_021401_1_0270102_01_00
Jacking of the Landing Gear
Jacking of the Landing Gear (Sheet 2 of 3)
FIGURE-2-14-1-991-027-A01
2-14-1
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FWD AXLE
BOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
FWD
JACKING POINT
376 mm
(14.80 in)
JACKING POINT
118.8 mm
(4.68 in)
AFT AXLE
BOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
FWD
JACKING POINT
376 mm
(14.80 in)
JACKING POINT
118.8 mm
(4.68 in)
FWD AND AFT AXLES
TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
FWD
JACKING POINT
130 mm
(5.12 in)
JACKING POINT
130 mm
(5.12 in)
F_AC_021401_1_0270103_01_00
Jacking of the Landing Gear
Jacking of the Landing Gear (Sheet 3 of 3)
FIGURE-2-14-1-991-027-A01
2-14-1
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
400 mm
(15.75 in)
170 mm 25.4 mm
(6.69 in) (1.00 in)
180 mm MAX
(7.09 in)
FWD
110 mm 1 FLAT TIRE
(4.33 in)
F_AC_021401_1_0280101_01_00
Jacking of the Landing Gear
(Sheet 1 of 2)
FIGURE-2-14-1-991-028-A01
2-14-1
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
NORMAL ATTITUDE
FWD
297.5 mm
(11.71 in)
JACKING POINT
290 mm
(11.42 in)
270 mm
(10.63 in)
TWO TIRES DEFLATED OR SHREDDED
FWD
JACKING POINT
148.5 mm
(5.85 in)
HEIGHT OF JACKING POINT TO GROUND
TO CHANGE/REPLACE THE WHEEL ASSEMBLY
1 083 mm
(42.64 in)
JACKING POINT
400 mm
(15.75 in)
FWD
25.4 mm
(1.00 in)
F_AC_021401_1_0280102_01_00
Jacking of the Landing Gear
(Sheet 2 of 2)
FIGURE-2-14-1-991-028-A01
2-14-1
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0
General Information
**ON A/C A330-700L
General Information
1.
This section gives aircraft turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by the
geometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,
it reflects the turning capability of the aircraft in favorable operating circumstances. This data should
only be used as 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 airlines in question prior to layout planning.
4-1-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0
Turning Radii
**ON A/C A330-700L
Turning Radii
1.
This section gives the turning radii.
4-2-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
55?
60?
65?
72?
R1
R2
R3
R5
R6
R4
NOTE:
FOR TURNING RADII VALUES, REFER TO SHEET 2.
F_AC_040200_1_0180101_01_00
Turning Radii
(Sheet 1)
FIGURE-4-2-0-991-018-A01
4-2-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
BELUGA XL TURNING RADII
TYPE OF STEERING
EFFECTIVE
TURN
ANGLE (deg) STEERING ANGLE (deg)
2
20
19.2
2
25
23.9
2
30
28.6
2
35
33.3
2
40
38.0
2
45
42.5
2
50
46.9
2
55
51.2
2
60
55.1
2
65
59.6
2
72
62.0
1
50
48.4
1
55
52.2
1
60
57.7
1
65
62.2
1
72
68.1
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
m
ft
R1
RMLG
59.3
195
45.7
150
36.3
119
29.4
96
24.0
79
19.8
65
16.4
54
13.5
44
11.1
36
8.6
28
7.4
24
15.3
50
12.8
42
9.6
31
7.3
24
4.5
15
R2
LMLG
70.0
230
56.4
185
47.0
154
40.1
132
34.7
114
30.5
100
27.1
89
24.1
79
21.8
72
19.3
63
18.1
59
26.0
85
23.5
77
20.3
67
18.0
59
15.2
50
R3
NLG
68.0
223
55.3
181
46.8
154
40.9
134
36.5
120
33.2
109
30.8
101
28.8
94
27.4
90
26.0
85
25.4
83
30.0
98
28.4
93
26.5
87
25.3
83
24.1
79
R4
WING
94.4
310
80.9
265
71.6
235
64.7
212
59.4
195
55.3
181
51.9
170
49.1
161
46.8
154
44.4
146
43.2
142
50.9
167
48.5
159
45.4
149
43.1
141
40.4
133
R5
NOSE
70.6
232
58.5
192
50.8
167
45.4
149
41.6
136
38.8
127
36.8
121
35.2
115
34.1
112
33
108
32.6
107
36.2
119
34.9
115
33.4
110
32.5
107
31.6
104
R6
TAIL
80.4
264
68.2
224
60.1
197
54.4
178
50.2
165
47.1
155
44.7
147
42.7
140
41.3
135
39.8
131
39.1
128
43.7
143
42.4
139
40.4
133
39
128
37.6
123
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.
F_AC_040200_1_0190101_01_00
Turning Radii
(Sheet 2)
FIGURE-4-2-0-991-019-A01
4-2-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0
Minimum Turning Radii
**ON A/C A330-700L
Minimum Turning Radii
1.
This section gives the minimum turning radii.
4-3-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
X
A
(MINIMUM TURNING WIDTH)
Y
R3
OUTSIDE FACE
OF TIRE
R5
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.
R4
BELUGA XL MINIMUM TURNING RADII
EFFECTIVE
R3
TYPE OF STEERING
X
Y
A
ANGLE (deg) STEERING ANGLE (deg)
NLG
TURN
m 22.2 8.9 39.7 24.1
72 (MAX)
68.1
1
79
ft 73 29 130
m 22.2 11.8 43.8 25.4
72 (MAX)
62.0
2
83
ft 73 39 144
m 22.2 11.7 43.6 25.3
65 (MAX)
62.2
1
83
ft 73 38 143
m 22.2 13 45.6
26
65 (MAX)
59.6
2
85
ft 73 43 150
NOTE:
IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1
BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
R4
WING
40.4
133
43.2
142
43.1
141
44.4
146
R5
NOSE
31.6
104
32.6
107
32.5
107
33
108
R6
TAIL
37.6
123
39.1
128
39
128
39.8
131
F_AC_040300_1_0100101_01_00
Minimum Turning Radii
FIGURE-4-3-0-991-010-A01
4-3-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0
Visibility from Cockpit in Static Position
**ON A/C A330-700L
Visibility from Cockpit in Static Position
1.
This section gives the visibility from cockpit in static position.
4-4-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
NOT TO BE USED FOR
LANDING APPROACH VISIBILITY
VISUAL ANGLES IN VERTICAL
PLANE THROUGH PILOT
EYE POSITION.
DIMENSIONS ARE APPROXIMATE
25?
20?
2.4 m
(7.87 ft)
11.63 m
(38.16 ft)
115?
135?
8.17 m
(26.80 ft)
MAX AFT VISION WITH HEAD TURNED
AROUND SPINAL COLUMN.
WING TIP CAN BE SEEN WHEN HEAD IS MOVED
TO THE SIDE.
FIRST OFFICER
FIELD OF VIEW
VISUAL ANGLES IN
HORIZONTAL PLANE THROUGH
PILOT EYE POSITION.
CAPTAIN FIELD OF VIEW
115?
135?
0.53 m
(1.74 ft)
WITH HEAD MOVED
125 mm (5 in) OUTBOARD
VISUAL ANGLES IN PLANE
PERPENDICULAR TO
LONGITUDINAL AXIS.
62?
62?
42?
36?
42?
30?
30?
36?
NOTE:
PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
ZONE THAT CANNOT BE SEEN
F_AC_040400_1_0100101_01_00
Visibility from Cockpit in Static Position
FIGURE-4-4-0-991-010-A01
4-4-0
Page 2
Jul 01/21
30?
20?
10?
0?
10?
20?
30?
43?
40?
4-4-0
90?
80?
70?
60?
CAPTAIN SLIDING
WINDOW
50?
40?
30?
20?
10?
CAPTAIN
WINDSHIELD
EXAMPLE: WHEN CAPTAIN TURNS HIS HEAD BY 85? LEFT, VISIBILITY
WILL BE 43? UP AND 30? DOWN THROUGH THE SLIDING
WINDOW FRAME.
CAPTAIN’S FIELD OF VIEW SHOWN, THROUGH CAPTAIN WINDOWS ONLY.
FIRST OFFICER FIELD OF VIEW SYMMETRICAL.
A330−700L
WING TIP
VISIBLE
140? 130? 120? 110? 100?
CAPTAIN
FIXED WINDOW
0?
20?
30?
40?
PILOT EYE POSITION
(CAPTAIN POSITION)
10?
50?
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_040400_1_0110101_01_00
Binocular Visibility Through Windows from Captain Eye Position
FIGURE-4-4-0-991-011-A01
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0
Runway and Taxiway Turn Paths
**ON A/C A330-700L
Runway and Taxiway Turn Paths
1.
Runway and Taxiway Turn Paths.
4-5-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1
135˚ Turn - Runway to Taxiway
**ON A/C A330-700L
135˚ Turn - Runway to Taxiway
1.
This section gives the 135˚ turn - runway to taxiway.
4-5-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
X
O
PR
AP
R
m
9 t)
5. f
= (19
ET
LL
FI ft)
N 0
−I (25
AD m
LE 5
A =7
FA L
APPROX 11.3 m
(37 ft)
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
TAXIWAY CENTERLINE
23 m
(75 ft)
RUNWAY CENTERLINE
NLG PATH
45 m
(150 ft)
MLG PATH
F_AC_040501_1_0130101_01_00
135˚ Turn - Runway to Taxiway
Judgemental Oversteer Method
FIGURE-4-5-1-991-013-A01
4-5-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ET
LL
FI ft)
N 0
−I (25
AD m
LE 5
A =7
FA L
APPROX 4.5 m
(15 ft)
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
TAXIWAY CENTERLINE
23 m
(75 ft)
RUNWAY CENTERLINE
NLG PATH
MLG PATH
45 m
(150 ft)
F_AC_040501_1_0140101_01_00
135˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-1-991-014-A01
4-5-1
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2
90˚ Turn - Runway to Taxiway
**ON A/C A330-700L
90˚ Turn - Runway to Taxiway
1.
This section gives the 90˚ turn - runway to taxiway.
4-5-2
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
APPROX 14.3 m
(47 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m
(75 ft)
APPROX 13.6 m
(45 ft)
FILLET R = 25.5 m
(85 ft)
TAXIWAY
CENTERLINE
TURN R = 45 m
(150 ft)
RUNWAY
CENTERLINE
NLG PATH
MLG PATH
45 m
(150 ft)
F_AC_040502_1_0150101_01_00
90˚ Turn - Runway to Taxiway
Judgemental Oversteer Method
FIGURE-4-5-2-991-015-A01
4-5-2
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m
(75 ft)
APPROX 7.3 m
(24 ft)
FILLET R = 25.5 m
(85 ft)
TAXIWAY
CENTERLINE
TURN R = 45 m
(150 ft)
RUNWAY
CENTERLINE
NLG PATH
MLG PATH
45 m
(150 ft)
F_AC_040502_1_0160101_01_00
90˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-2-991-016-A01
4-5-2
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3
180˚ Turn on a Runway
**ON A/C A330-700L
180˚ Turn on a Runway
1.
This section gives the 180˚ turn on a runway.
4-5-3
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
RUNWAY CENTERLINE
4.5 m
(15 ft)
4.5 m
(15 ft)
NLG PATH
APPROX 48.8 m
(160 ft)
MLG PATH
F_AC_040503_1_0170101_01_00
180˚ Turn on a Runway
FIGURE-4-5-3-991-017-A01
4-5-3
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4
135˚ Turn - Taxiway to Taxiway
**ON A/C A330-700L
135˚ Turn - Taxiway to Taxiway
1.
This section gives the 135˚ turn - taxiway to taxiway.
4-5-4
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ET
LL
FI ft)
N 0
−I (25
AD
m
m
LE 5
3 t)
A =7
6. 1 f
=
FA L
R (2
X
O
PR
AP
APPROX 13 m
(43 ft)
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
23 m
(75 ft)
TAXIWAY CENTERLINE
TAXIWAY CENTERLINE
NLG PATH
23 m
(75 ft)
MLG PATH
F_AC_040504_1_0150101_01_00
135˚ Turn - Taxiway to Taxiway
Judgemental Oversteer Method
FIGURE-4-5-4-991-015-A01
4-5-4
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ET
LL
FI ft)
N 0
−I (25
AD m
LE 5
A =7
FA L
APPROX 5.5 m
(18 ft)
FILLET R = 25.5 m
(85 ft)
TURN R = 45 m
(150 ft)
23 m
(75 ft)
TAXIWAY CENTERLINE
TAXIWAY CENTERLINE
NLG PATH
23 m
(75 ft)
MLG PATH
F_AC_040504_1_0160101_01_00
135˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-4-991-016-A01
4-5-4
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5
90˚ Turn - Taxiway to Taxiway
**ON A/C A330-700L
90˚ Turn - Taxiway to Taxiway
1.
This section gives the 90˚ turn - taxiway to taxiway.
4-5-5
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
APPROX 14.4 m
(47 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m
(75 ft)
APPROX 13m
(43 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)
F_AC_040505_1_0170101_01_00
90˚ Turn - Taxiway to Taxiway
Judgemental Oversteer Method
FIGURE-4-5-5-991-017-A01
4-5-5
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m
(75 ft)
APPROX 6.2m
(20 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)
F_AC_040505_1_0180101_01_00
90˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-5-991-018-A01
4-5-5
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0
Runway Holding Bay (Apron)
**ON A/C A330-700L
Runway Holding Bay (Apron)
1.
This section gives the runway holding bay (Apron).
4-6-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
6.1 m
(20 ft)
94.5 m
(310 ft)
90 m
(300 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 AIRLINE FOR SPECIFIC PLANNED
OPERATING PROCEDURES.
F_AC_040600_1_0070101_01_00
Runway Holding Bay (Apron)
FIGURE-4-6-0-991-007-A01
4-6-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0
Minimum Line-Up Distance Corrections
**ON A/C A330-700L
Minimum Line-Up Distance Corrections
1.
The ground maneuvers were performed using asymmetric thrust and differential-only braking 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, see FIGURE 4-7-0-991-028-A.
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, see FIGURE 4-7-0-991-029-A.
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, see FIGURE 4-7-0-991-030-A.
The value of this angle depends on the aircraft type and is mentioned in the FCOM.
During the turn, all the clearances must meet the minimum value of 4.5 m (15 ft) for this category of
aircraft as recommended in ICAO Annex 14.
4-7-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
4.5 m
(15 ft)
TODA
ASDA
TAXIWAY
CENTERLINE
> 4.5 m
(15 ft)
RUNWAY
CENTERLINE
90? TURN ON RUNWAY ENTRY
45 m (150 ft)/60 m (200 ft) WIDE RUNWAY
AIRCRAFT TYPE
A330−700L
A330−700L
MAX
STEERING
ANGLE
65?
72?
MINIMUM LINE−UP DISTANCE CORRECTION
ON TODA
22.5 m
74 ft
19.7 m
65 ft
NOTE:
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
ON ASDA
44.7 m
41.9 m
147 ft
137 ft
F_AC_040700_1_0280101_01_00
Minimum Line-Up Distance Corrections
90˚ Turn on Runway Entry
FIGURE-4-7-0-991-028-A01
4-7-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
MINIMUM PAVEMENT WIDTH
TODA
> 4.5 m
(15 ft)
4.5 m
(15 ft)
ASDA
RUNWAY CENTERLINE
180? TURN ON RUNWAY TURNPAD
45 m (150 ft)/60 m (200 ft) WIDE RUNWAY
AIRCRAFT
TYPE
A330−700L
A330−700L
MAX
STEERING
ANGLE
65?
72?
REQUIRED
MINIMUM
PAVEMENT
WIDTH
MINIMUM LINE−UP
DISTANCE CORRECTION
ON TODA
30.1 m
99 ft
28.9 m
95 ft
ON ASDA
52.2 m
171 ft
51.1 m
168 ft
NOTE:
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
56.7 m 186 ft
51.1 m 168 ft
F_AC_040700_1_0290101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Turn Pad
FIGURE-4-7-0-991-029-A01
4-7-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
4.5 m
(15 ft)
TODA
4.5 m
(15 ft)
ASDA
> 4.5 m
(15 ft)
20?
RUNWAY CENTERLINE
180? TURN ON RUNWAY WIDTH
AIRCRAFT
TYPE
MAX
STEERING
ANGLE
45 m (150 ft) WIDE RUNWAY
(STANDARD WIDTH)
60 m (200 ft) WIDE RUNWAY
MINIMUM LINE−UP
DISTANCE CORRECTION
MINIMUM LINE−UP
DISTANCE CORRECTION
ON TODA
A330−700L
A330−700L
65?
72?
ON ASDA
NOT POSSIBLE
ON TODA
44.5 m
146 ft
28.9 m
95 ft
NOTE:
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
ON ASDA
66.6 m
219 ft
51.1 m
168 ft
F_AC_040700_1_0300101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Width
FIGURE-4-7-0-991-030-A01
4-7-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-8-0
Aircraft Mooring
**ON A/C A330-700L
Aircraft Mooring
1.
This section gives information on aircraft mooring.
4-8-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
TOWING FITTING
B
A
TOWING FITTING
GROUND ANCHOR
A
WARNING FLAG
B
F_AC_040800_1_0020101_01_00
Aircraft Mooring
FIGURE-4-8-0-991-002-A01
4-8-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-1-2
Typical Ramp Layout - Open Apron
**ON A/C A330-700L
05-01-02 Typical Ramp Layout
1.
This section gives information about the typical ramp layout.
5-1-2
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FEET
0 10 20 30 40 50 60
0
4
8
12 16
METERS
HANGAR
20
STAND SAFETY LINE
FUEL
F_AC_050102_1_0120101_01_00
Typical Ramp Layout
FIGURE-5-1-2-991-012-A01
5-1-2
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1
Ground Service Connections Layout
**ON A/C A330-700L
Ground Service Connections Layout
1.
This section gives the ground service connections layout.
5-4-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
1 (INSIDE FWD CARGO)
12
10
7A
9
8
6A
15
17
3 2
4 6A
7A
13
11
8
17
9
3
5
16
1 − OXYGEN SERVICING
2 − GROUND ELECTRICAL POWER CONNECTORS
3 − POTABLE WATER DRAIN
4 − LOW PRESSURE AIR PRE−CONDITIONING
5 − HIGH PRESSURE AIR PRE−CONDITIONING
AND ENGINE STARTING
6A − ENGINE OIL FILLING
7A − IDG OIL FILLING
8 − PRESSURE REFUEL/DEFUEL COUPLINGS
9 − OVERWING REFUEL
10 − HYDRAULIC GROUND POWER SUPPLY (YELLOW)
11 − HYDRAULIC RESERVOIR FILLING AND GROUND
POWER SUPPLY (GREEN)
12 − HYDRAULIC RESERVOIR AIR PRESSURIZATION
AND GROUND POWER SUPPLY (BLUE)
13 − REFUEL/DEFUEL PANEL
15 − WASTE WATER SERVICE PANEL
16 − APU OIL FILLING
17 − GROUNDING (EARTHING) POINT
F_AC_050401_1_0070101_01_00
Ground Service Connections Layout
FIGURE-5-4-1-991-007-A01
5-4-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2
Grounding Points
**ON A/C A330-700L
Grounding (Earthing) Points
1.
Grounding (Earthing) Points
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
On NLG leg
On left MLG leg
On right MLG leg
AFT OF NOSE
8.17 m
(26.80 ft)
32.1 m
(105.31 ft)
32.1 m
(105.31 ft)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
On centerline
5.34 m
(17.52 ft)
5.34 m
(17.52 ft)
MEAN HEIGHT
FROM GROUND
1.40 m
(4.59 ft)
1.50 m
(4.92 ft)
1.50 m
(4.92 ft)
A.
The grounding (earthing) stud on each landing gear leg is designed for use with a clip-on
connector (such as Appleton TGR).
B.
The grounding (earthing) studs are used to connect the aircraft to an approved ground (earth)
connection on the ramp or in the hangar for:
- Refuel/defuel operations
- Maintenance operations
- Bad weather conditions
- Loading/Unloading operations.
NOTE : In all other conditions, the electrostatic discharge through the tire is sufficient.
5-4-2
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
FR18
FR17A
B
125EL
A
C
BRACKET
B
GROUNDING
(EARTHING) CABLE
C
F_AC_050402_1_0060101_01_00
Ground Service Connections
Grounding (Earthing) Points
FIGURE-5-4-2-991-006-A01
5-4-2
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
A
NOSE LANDING GEAR
MAIN LANDING GEAR
LANDING
GEAR
GROUNDING (EARTHING) POINT
GROUNDING (EARTHING) CABLE
A
TYPICAL
F_AC_050402_1_0070101_01_00
Ground Service Connections
Grounding (Earthing) Points
FIGURE-5-4-2-991-007-A01
5-4-2
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
RIB22
RIB23
A
01
F
W
D
NOTE:
01 LH SHOWN RH SYMMETRICAL
F_AC_050402_1_0080101_01_00
Ground Service Connections
Grounding (Earthing) Points
FIGURE-5-4-2-991-008-A01
5-4-2
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3
Hydraulic System
**ON A/C A330-700L
Hydraulic System
1.
Ground Service Panels
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
Green system:
Access door 197CB
Yellow system:
Access door 196BB
Blue system:
Access door 195BB
2.
AFT OF NOSE
33.10 m
(108.60 ft)
27.30 m
(89.57 ft)
26.30 m
(86.29 ft)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
1.28 m
(4.20 ft)
1.32 m
(4.33 ft)
1.28 m
(4.20 ft)
MEAN HEIGHT
FROM GROUND
2.23 m
(7.32 ft)
1.95 m
(6.40 ft)
1.94 m
(6.36 ft)
Reservoir Pressurization
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT OF NOSE
Blue system ground 26.34 m
service panel:
(86.42 ft)
Access door 195BB
3.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
1.28 m
(4.20 ft)
MEAN HEIGHT
FROM GROUND
1.94 m
(6.36 ft)
Accumulator Charging
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT OF NOSE
Blue system
26.34 m
accumulator:
(86.42 ft)
Access door 195BB
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
1.28 m
(4.20 ft)
MEAN HEIGHT
FROM GROUND
1.94 m
(6.36 ft)
5-4-3
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4.
Reservoir Filling
Two connections (one self-sealing connection for pressurized supply on the Green system ground
service panel).
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
One handpump
filling connection:
Access door
197CBB
5.
AFT OF NOSE
33.22 m
(108.99 ft)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
1.28 m
(4.20 ft)
MEAN HEIGHT
FROM GROUND
2.23 m
(7.32 ft)
A/C Emergency Generation
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT OF NOSE
Ram Air Turbine
32.90 m
(RAT) safety-pin
(107.94 ft)
installation:
Access panel 633SL
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
14.20 m
(46.59 ft)
5-4-3
MEAN HEIGHT
FROM GROUND
4.35 m
(14.27 ft)
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
197CB
FR53.4 FR53.5
MAN SELECTOR
VALVE−RSVR
FILLING
RSVR
FILLING VALVE
GND CNCTR−SELF
SEALING, G SUCTION
FILTER−RSVR
FILLING
HYD
RSVR FILLING
ADJUSTMENT
INDICATOR
PRESS GAGE
G POWER ACCU
VALVE−MAN
DEPRESS, G−RSVR
GND CNCTR
NITROGEN CHARGING
G POWER ACCU
GND CNCTR−SELF
SEALING, G DELIVERY
HAND PUMP
RSVR FILLING
GND CNCTR−SELF
SEALING RSVR
FILLING
FWD
LEVER HAND
PUMP
A
F_AC_050403_1_0130101_01_00
Ground Service Connections
Green System Ground Service Panel
FIGURE-5-4-3-991-013-A01
5-4-3
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
FR44 FR45
195BB
PRESS GAGES
PARK BRK ACCU
PRESS GAGE
B POWER ACCU
GND CNCTR
NITROGEN
CHARGING
B POWER ACCU
PARK BRK ACCU
PARK BRK ACCU
GND CNCTR
SELF−SEALING,
B SUCTION
VALVE−MAN
DEPRESS, B RSVR
GND CNCTR
SELF−SEALING,
B/Y RSVR PRESS
GND CNCTR
SELF−SEALING,
G RSVR PRESS
FWD
A
GND CNCTR−SELF
SEALING,
B DELIVERY
F_AC_050403_1_0140101_01_00
Ground Service Connections
Blue System Ground Service Panel
FIGURE-5-4-3-991-014-A01
5-4-3
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FR46 FR47
A
196BB
HAND PUMP
CARGO DOORS, Y
RAT STOW PANEL
CARGO DOOR
SELECTOR MANIFOLD
SIGHT
GLASS
GND CNCTR−SELF
SEALING, Y DELIVERY
GND CNCTR−SELF
SEALING, Y SUCTION
GND CNCTR
NITROGEN CHARGING
Y POWER ACCU
VALVE−MAN
PRESS GAGE
DEPRESS, Y RSVR Y POWER ACCU
FWD
A
F_AC_050403_1_0150101_01_00
Ground Service Connections
Yellow System Ground Service Panel
FIGURE-5-4-3-991-015-A01
5-4-3
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
Z633
633SL
A
B
C
RAT UPLOCK
SAFETY−PIN
B
RAT RETRACTED
633GB
RAM AIR TURBINE (RAT)
C
RAT EXTENDED
F_AC_050403_1_0160101_01_00
Ground Service Connections
RAT
FIGURE-5-4-3-991-016-A01
5-4-3
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4
Electrical System
**ON A/C A330-700L
Electrical Servicing
1.
A/C External Power
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
A/C external
power:
Access door 121EL
AFT OF NOSE
8.70 m
(28.54 ft)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.10 m
(0.33 ft)
MEAN HEIGHT
FROM GROUND
1.95 m
(6.40 ft)
NOTE : Distances are approximate.
2.
Technical Specifications
A.
External power receptacles:
- Two receptacles according to MS 90362-3 - 90 kVA.
B.
Power supply:
- Three-phase, 115 V, 400 Hz.
C.
Electrical connectors for servicing:
- AC outlets: HUBBELL 5258
- DC outlets: HUBBELL 7472.
D.
Maintenance bus switch:
- Inside A/C near bulkhead door.
5-4-4
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
EXTERNAL POWER RECEPTACLES
B
FR17A
FR18
121EL
A
TYPICAL
925VU
B
F_AC_050404_1_0070101_01_01
Ground Service Connections
Electrical Service Panel
FIGURE-5-4-4-991-007-A01
5-4-4
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FR40
A
Z131 (Z132)
FR20
FR21A
B
A
BULKHEAD DOOR
MAINTENANCE BUS
BELLY DOOR
B
F_AC_050404_1_0080101_01_00
Ground Service Connections
Maintenance Bus-Switch Location
FIGURE-5-4-4-991-008-A01
5-4-4
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5
Oxygen System
**ON A/C A330-700L
Oxygen System
1.
Oxygen Servicing
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
Oxygen
replenishment
(option 1):
5750HT
Oxygen
replenishment
(option 2):
5751HT
AFT OF NOSE
12.54 m
(41.14 ft)
12.54 m
(41.14 ft)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.44 m
(1.44 ft)
MEAN HEIGHT
FROM GROUND
3.46 m
(11.35 ft)
0.44 m
(1.44 ft)
3.46 m
(11.35 ft)
NOTE : Internal charging connection near the belly door, inside aircraft.
5-4-5
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FR40
A
FR26
FR20
Z131 (Z132)
B
A
TEST PORT
5750HT
C
FR26
5751HT
C
B
OXYGEN
FILLING PORT
C
01
NOTE:
01 LH SHOWN, RH SYMMETRICAL
F_AC_050405_1_0050101_01_00
Ground Service Connections
Oxygen Servicing
FIGURE-5-4-5-991-005-A01
5-4-5
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6
Fuel System
**ON A/C A330-700L
Fuel System
1.
Refuel/Defuel Control Panel
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT OF NOSE
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
Refuel/Defuel
32.6 m
control panel:
(106.96 ft)
Access door 198DB
2.
0.8 m
(2.62 ft)
A.
Flow rate: 1 580 l/min (417 US gal/min) per connection.
B.
Maximum pressure: 50 psi (3.45 bar).
MEAN HEIGHT
FROM GROUND
1.9 m
(6.23 ft)
Refuel/Defuel Connectors
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
Refuel/Defuel
coupling, right:
Access door 622HB
Overwing gravity
refuel cap
A.
B.
3.
AFT OF NOSE
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
28.3 m
(92.85 ft)
32.8 m
(107.61 ft)
17.2 m
(56.43 ft)
MEAN HEIGHT
FROM GROUND
12.6 m
(41.34 ft)
5.1 m
(16.73 ft)
17.2 m
(56.43 ft)
6.1 m
(20.01 ft)
Four standard 2.5 in. ISO 45 connections.
Two service connections (gravity refuel).
Overpressure Protector and NACA Flame Arrestor
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
5-4-6
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
ACCESS
Overpressure
protector (wing):
Access panel 550EB
(650EB)
NACA flame
arrestor (wing):
Access panel
550DB (650DB)
AFT OF NOSE
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
37.8 m
(124.02 ft)
27.17 m
(89.14 ft)
27.17 m
(89.14 ft)
5.75 m
(18.86 ft)
37.4 m
(122.70 ft)
26.53 m
(87.04 ft)
26.53 m
(87.04 ft)
5.7 m
(18.70 ft)
5-4-6
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
FR53.2
198DB
FR53.4
HIGH LEVEL
L OUTER TK L INNER TK
CTR TK
OVERFLOW
TRIM TK
L OUTER
MODE SELECT
REFUEL
OFF
DEFUEL
CENTER
TRIM
LOAD
CLOSED
DEC
R INNER TK R OUTER TK
TRIM TK
R
OPEN
x 1000 PRESELECTED
CKPT
END
ACTUAL
R OUTER
R INR.
REFUEL/DEFUEL VALVES
L OUTER TK L INNER TK CTR TK
TT
HI LEVEL TRANSF. VALVE
TEST
INC
1b kg
L INR.
L
R INNER TK R OUTER TK
OPEN
NORM
SHUT
PWR
SUPPLY
APU EMERG.
NORM SHUT
DOWN
BAT
A
F_AC_050406_1_0210101_01_00
Ground Service Connections
Refuel/Defuel Control Panel
FIGURE-5-4-6-991-021-A01
5-4-6
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
622HB
A
REFUEL/DEFUEL
COUPLING
REFUEL/DEFUEL
COUPLING CAP
REFUEL/DEFUEL
COUPLING CAP
A
F_AC_050406_1_0220101_01_00
Ground Service Connections
Refuel/Defuel Coupling
FIGURE-5-4-6-991-022-A01
5-4-6
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
RIB38
A
550EB
(650EB)
RIB37
RIB36
C
550DB
(650DB)
B
FWD
A
LH SHOWN
RH SYMMETRICAL
NACA FLAME ARRESTOR
B
C
OVERPRESSURE PROTECTOR
F_AC_050406_1_0230101_01_00
Ground Service Connections
Overpressure Protector and NACA Flame Arrestor - Wing
FIGURE-5-4-6-991-023-A01
5-4-6
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7
Pneumatic System
**ON A/C A330-700L
Pneumatic System
1.
High Pressure Air Connection
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT OF NOSE
20.94 m
HP connectors:
Access door 193CB (68.70 ft)
A.
2.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.84 m
(2.76 ft)
MEAN HEIGHT
FROM GROUND
1.79 m
(5.87 ft)
Connectors:
- Two standard 3 in. ISO 2026 connections.
Low Pressure Air Connection
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT OF NOSE
22.66 m
LP connectors:
Access door 191EB (74.34 ft)
A.
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.4 m
(1.31 ft)
MEAN HEIGHT
FROM GROUND
8m
(26.25 ft)
Connectors:
- Two standard 8 in. SAE AS4262 connections.
5-4-7
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
191EB
193CB
B
A
FR40
HP CONNECTOR
A
LP CONNECTOR
B
F_AC_050407_1_0040101_01_00
Ground Service Connections
LP and HP Ground Connectors
FIGURE-5-4-7-991-004-A01
5-4-7
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8
Oil System
**ON A/C A330-700L
Oil System
1.
RR Trent 700 Series Engine
A.
Engine Oil Replenishment:
One gravity filling cap.
One ozone self-sealing pressure fill and overfill connector per engine.
NOTE : The mean height from ground in the below table may change according to the CG
position and aircraft weight.
ACCESS
AFT OF NOSE
25.40 m
Engine 1:
Access door 416CR (83.33 ft)
25.40 m
Engine 2:
Access door 426CR (83.33 ft)
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
7.92 m
(25.98 ft)
10.82 m
(35.50 ft)
MEAN HEIGHT
FROM GROUND
2.05 m
(6.73 ft)
2.05 m
(6.73 ft)
(1) Tank capacity:
- Full level: 23.30 l (6.16 US gal).
- Usable: 22.71 l (6.00 US gal).
B.
IDG Oil Replenishment:
One ozone self-sealing pressure fill and overfill connector per engine.
NOTE : The mean height from ground in the below table may change according to the CG
position and aircraft weight.
DISTANCE
ACCESS
Engine 1:
Access door 415CL
Engine 2:
Access door 425CL
AFT OF NOSE
25.9 m
(84.97 ft)
25.9 m
(84.97 ft)
FROM AIRCRAFT CENTERLINE
LH SIDE
9.65 m
(31.66 ft)
MEAN HEIGHT
FROM GROUND
RH SIDE
9.09 m
(29.82 ft)
0.80 m
(2.62 ft)
0.80 m
(2.62 ft)
(1) Max delivery pressure required: 2.76 bar (40 psi).
(2) Max oil capacity of the IDG: 5.50 l (1.45 Us gal).
5-4-8
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
C.
Starter Oil Replenishment:
One filling connection per engine.
NOTE : The mean height from ground in the below table may change according to the CG
position and aircraft weight.
ACCESS
AFT OF NOSE
Engine 1:
25.9 m
Access door 415AL
(84.97 ft)
(416AR)
Engine 2:
25.9 m
Access door 425AL
(84.97 ft)
(426AR)
-
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
9.65 m
(31.66 ft)
MEAN HEIGHT
FROM GROUND
0.80 m
(2.62 ft)
9.09 m
(29.82 ft)
0.80 m
(2.62 ft)
Max oil capacity of the starter: 0.50 l (0.13 US gal).
5-4-8
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
416CR (ENGINE 1)
426CR (ENGINE 2)
A
OIL TANK
OIL FILLER CAP
B
OVERFLOW
COUPLING
US QUARTZ REQUIRED
FULL
1
1
2
2
3
3
4
4
5
LITERS REQUIRED
FULL
PRESSURE FILL
COUPLING
5
SIGHT GLASS
A
FWD
B
F_AC_050408_1_0280101_01_00
Ground Service Connections
Engine Oil Tank - RR Trent 700 Series Engine
FIGURE-5-4-8-991-028-A01
5-4-8
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
(ENGINE 1) 415CL
(ENGINE 2) 425CL
B
OVER FULL
PRESSURE
FILL CONNECTOR
SIGHT GLASS
OVERFILL
DRAIN CONNECTOR
FWD
DRAIN PLUG
A
ADD
OIL
STABLE OIL
B
F_AC_050408_1_0290101_01_00
Ground Service Connections
IDG Oil Tank - RR Trent 700 Series Engine
FIGURE-5-4-8-991-029-A01
5-4-8
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
416AR (ENGINE 1)
426AR (ENGINE 2)
415AL (ENGINE 1)
425AL (ENGINE 2)
A
PNEUMATIC
STARTER
OIL FILL
PLUG
SIGHT GLASS
EXTERNAL
GEARBOX
OIL DRAIN PLUG
MAGNETIC CHIP
DETECTOR
A
OIL LEVEL
OVERFLOW
PLUG
F_AC_050408_1_0300101_01_00
Ground Service Connections
Starter Oil Tank - RR Trent 700 Series Engine
FIGURE-5-4-8-991-030-A01
5-4-8
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
APU Oil Servicing
1.
APU Oil Servicing:
APU oil gravity filling cap.
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT OF NOSE
APU oil
58.94 m
replenishment:
Access doors 315AL (193.37 ft)
and 316AR
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
0.4 m
(1.31 ft)
MEAN HEIGHT
FROM GROUND
8m
(26.25 ft)
5-4-8
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
Z310
OIL PUMP
MODULE
OIL FILLER
CAP
B
FR101
A
OIL SCUPPER
GRAVITY FILL
PORT
GENERATOR
SCAVENGE
OIL FILTER
LUBRIFICATION
OIL FILTER
316AR
A
315AL
FR95
PRESSURE FILL
OVERFLOW PORT
PRESSURE
FILL PORT
DO NOT REMOVE OIL
FILLER CAP WHEN OIL
LEVEL IS ABOVE FULL
MARK ON SIGHT GLASS
OIL SIGHT
GLASS
FWD
B
F_AC_050408_1_0310101_01_00
Ground Service Connections
APU Oil Servicing
FIGURE-5-4-8-991-031-A01
5-4-8
Page 7
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10
Waste Water System
**ON A/C A330-700L
Waste Water System
1.
Waste Water Servicing
A.
There are two waste-water ground-service panels:
- First panel: One standard connection Roylyn 1 in. (ISO 17775) for flushing and filling
- Second panel: One standard Taco type valve 4 in. (ISO 17775) for draining.
NOTE : Handle used for drainage is located on the first panel.
B.
Capacity waste tanks:
- Standard: 35 l (9.25 US gal).
NOTE : The waste water drain-system discards the waste water from the galley sink and the
lavatory washbasin overboard.
The toilet system moves the waste materials and liquids from the toilet to the waste
tank.
C.
Chemical fluid:
- Standard: 9.5 l (2.51 US gal).
NOTE : The mean height from ground in the below table may change according to the CG
position and aircraft weight.
ACCESS
Waste-water
ground-servicepanel 1:
Access door 121GL
Waste-water
ground-servicepanel 2:
Access door 121FL
AFT OF NOSE
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
6.39 m
(20.96 ft)
2.03 m
(6.66 ft)
2.16 m
(7.09 ft)
7.13 m
(23.39 ft)
1.91 m
(6.27 ft)
2.19 m
(7.19 ft)
5-4-10
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
FR13 FR15
B
A
Z120
FR13A
FR13
CAP FLUSH NIPPLE
5345MG
FLUSH NIPPLE
44DV
121GL
FR15
FR14A
WASTE−CAP
DRAIN VALVE
5360MG
A
121FL
B
F_AC_050410_1_0080101_01_01
Ground Service Connections
Waste-Water Ground-Service Panels
FIGURE-5-4-10-991-008-A01
5-4-10
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-11
Cargo Control Panels
**ON A/C A330-700L
Cargo Control Panels
1.
Cargo Control Panels
NOTE : The mean height from ground in the below table may change according to the CG position
and aircraft weight.
ACCESS
AFT cargo door
panel:
Access door 152NR
Main Deck Cargo
Door (MDCD)
inner operation
panel
MDCD outer
operation panel
AFT OF NOSE
DISTANCE
FROM AIRCRAFT CENTERLINE
LH SIDE
RH SIDE
MEAN HEIGHT
FROM GROUND
40.73 m
(133.6 ft)
2.68 m
(8.8 ft)
4.41 m
(14.5 ft)
9.26 m
(30.4 ft)
3.23 m
(10.6 ft)
6.09 m
(20.0 ft)
10.25 m
(33.6 ft)
3.55 m
(11.6 ft)
6.26 m
(20.5 ft)
5-4-11
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
197CB
152NR
B
D
E
A
C
HAND PUMP
7155JE
A
HAND PUMP
LEVER
196BB
B
F
W
D
GREEN INDICATOR LIGHT
C
HANDLE FLAP
LOCKING HANDLE
RESIDUAL PRESSURE
WARNING LIGHT
DOOR OPERATION
LEVER
FWD
PUSHBUTTON
INDICATOR FLAG
D
LATCHING HANDLE
E
F_AC_050411_1_0080101_01_00
Lower Cargo Door Operation Panel
FIGURE-5-4-11-991-008-A01
5-4-11
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
B
C
A
FR21A
FR18A
FR21 FR19A
FWD
A
C
FWD
MDCD OUTER
OPERATION PANEL
"FULLY
OPEN"
LIGHT
B
MDCD INNER
OPERATION PANEL
"FAULT"
WARNING LIGHT
"OPEN/CLOSE"
TOGGLE SWITCH
C
TYPICAL
MDCD OPERATION PANEL
F_AC_050411_1_0090101_01_00
MDCD Control Panel
FIGURE-5-4-11-991-009-A01
5-4-11
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0
Engine Starting Pneumatic Requirements
**ON A/C A330-700L
Engine Starting Pneumatic Requirements
1.
The purpose of this section is to give 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
discharge temperature, absolute discharge pressure and mass flow rate.
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
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ROLLS ROYCE TRENT 700 SERIES/SEA LEVEL
STARTING TIME: LESS THAN 90 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
240
130
230
120
220
110
210
200
100
AIRFLOW (lb/min)
AIRFLOW (kg/min)
140
190
90
180
80
ABSOLUTE PRESSURE (psia)
45
50
55
ABSOLUTE PRESSURE (psia)
60
65
60
55
50
ASU DISCHARGE TEMPERATURE:
85? C (185? F)
150? C (302? F)
220? C (428? F) MAX.
45
40
−60
−50
−60
−40 −30 −20 −10
0
10
20
OUTSIDE AIR TEMPERATURE OAT (? C)
−40 −20
0
20
40
60
OUTSIDE AIR TEMPERATURE OAT (? F)
30
80
40
100
EXAMPLE:
FOR AN OAT OF 15? C (59? F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 85? C (185? F)
AT HPGC:
− THE REQUIRED PRESSURE AT HPGC IS 48.85 psia
− THE REQUIRED AIRFLOW AT HPGC IS 114.9 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 117.5? C (243.5? F)
AT HPGC, INTERPOLATING BETWEEN THE LINES 85? C (185? F) AND 150? C (302? F) RESULTS IN:
− A REQUIRED PRESSURE AT HPGC OF 47.84 psia
− A REQUIRED AIRFLOW AT HPGC OF 113.9 kg/min.
F_AC_050500_1_0110101_01_00
Engine Starting Pneumatic Requirements
Rolls Royce Trent 700 Series Engine
FIGURE-5-5-0-991-011-A01
5-5-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0
Ground Towing Requirements
**ON A/C A330-700L
Ground Towing Requirements
1.
This section gives information on aircraft towing.
The A330-700L is designed with means for conventional or towbarless towing.
Information/procedures can be found for both 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.
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.
The chart is based on the A330 engine type with the highest idle thrust.
The chart is therefore valid for A330-700L model.
2.
Towbar design guidelines
The aircraft towbar shall comply with the following standards:
- 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 (276 991 lbf.in).
The towing head is designed according to ISO 8267-1, cat. III.
3.
This section gives information on aircraft towing with towbarless tractors.
There are special approval procedures for towbarless tractors. Before towing, make sure that the
towbarless tractor is approved for towing A330-700L.
The list of towbarless towing vehicles that are specially accepted for A330-700L are given in Airbus
In-Service Information, refer to ISI 09.11.00001.
Ram Air Outlet (RAO) 1 and RAO 2 must be closed when a towbarless tractor approaches the
aircraft.
If RAO 2 (RH) is stuck open, the towbarless towing is permitted but special attention is necessary
because of the space between RAO and the tractor is very less in this configuration.
For safe approach of the tractor for the aircraft towing, it is recommended to follow the aircraft
center-line trajectory.
5-8-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
50
BREAKAWAY RESISTANCE 4%
# OF ENGINES ON FOR PB: 1
ENGINE THRUST 1 500 daN
RE
TE
30
W
15
1.5% SLOPE
1 ENGINE ON
Y
20 18.8
CO
CO
NC
25
ET
OW
D SN
230
= 0.2
HAR
10
5
32.9
230
210
190
170
150
130
110
= 0.05
ICE
A/C WEIGHT (x 1 000 kg)
0.
ET
R
NC
=
35
0.
E
8
40
57
=
DR
DRAWBARPULL (x 1 000 kg)
45
0
0
10
20
30
40
50
60
70
80
TOTAL TRACTION WHEEL LOAD (x 1 000 kg)
0
1
2
0
No. OF ENGINES
AT IDLE
0.5
1.0
1.5
2.0
SLOPE ( % )
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A330 AT 230 000 kg, AT 1.5% SLOPE,
1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
−
−
−
−
−
−
−
ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (230 000 kg),
FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),
FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 2,
FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED No. OF ENGINES (1),
FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,
THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (18 800 kg),
SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE.
THE OBTAINED X−COORDINATE IS THE RECOMMENDED TOTAL TRACTION
WHEEL LOAD (32 900 kg).
F_AC_050800_1_0150101_01_00
Ground Towing Requirements
FIGURE-5-8-0-991-015-A01
5-8-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
A
Z190
B
B
RAO 2
RAO 1
RAO LOCATION
A
RAO IN CLOSED POSITION
FWD
RAO IN OPENED POSITION
FWD
B
TYPICAL
F_AC_050800_1_0180101_01_00
Ground Towing Requirements
Location of the RAOs (Sheet 1 of 2)
FIGURE-5-8-0-991-018-A01
5-8-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
HANGAR
TOWBARLESS
TRACTOR
AIRCRAFT
CENTER LINE
TOWBARLESS
TRACTOR
F_AC_050800_1_0180102_01_00
Ground Towing Requirements
Tractor Trajectory for Towing Operations (Sheet 2 of 2)
FIGURE-5-8-0-991-018-A01
5-8-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0
De-Icing and External Cleaning
**ON A/C A330-700L
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 20 m (65.62 ft).
5-9-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
TOP THIRD 120? ARC
WING TOP WING TIP DEVICES
AREA SURFACE (BOTH INSIDE AND
(BOTH OUTSIDE SURFACES)
SIDES)
(BOTH SIDES)
m?
(ft?)
306
(3 294)
11
(118)
HTP TOP
VTP
FUSELAGE TOP NACELLE, PYLON TOTAL
SURFACE SURFACE
SURFACE
TOP SURFACE DE−ICED
(BOTH
(BOTH
(TOP THIRD− (TOP THIRD−
AREA
SIDES)
SIDES)
120? ARC)
120? ARC)
(ALL ENGINES)
65
(700)
210
(2 260)
410
(4 413)
46
(495)
1 048
(11 281)
F_AC_050900_1_0010101_01_00
De-Icing and External Cleaning
FIGURE-5-9-0-991-001-A01
5-9-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0
Engine Exhaust Velocities and Temperatures
**ON A/C A330-700L
Engine Exhaust Velocities and Temperatures
1.
General
This section shows the estimated engine exhaust efflux velocities and temperatures contours for
ground idle, breakaway and maximum takeoff conditions.
6-1-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A330-700L
Engine Exhaust Velocities Contours - Ground Idle Power
1.
This section gives engine exhaust velocities contours at ground idle power.
NOTE : The three values give velocities isolines values at the borders of colored areas.
6-1-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ft
m
24
80
18
60
12
40
6
20
0
0
(100 fps = 68 MPH = 109 kmph)
200 fps
100 fps
50 fps
ELEVATION
0
50
100
150
15
30
45
FEET
METERS
0
(100 fps = 68 MPH = 109 kmph)
ft
m
24
80
18
60
12
40
6
20
0
0
200 fps
100 fps
50 fps
PLAN
F_AC_060101_1_0070101_01_00
Engine Exhaust Velocities
Ground Idle Power - RR Trent 700 Series Engine
FIGURE-6-1-1-991-007-A01
6-1-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A330-700L
Engine Exhaust Temperatures Contours - Ground Idle Power
1.
This section gives engine exhaust temperatures contours at ground idle power.
NOTE : The three values give temperature isolines values at the borders of colored areas.
6-1-2
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ft
m
24
80
18
60
12
40
6
20
0
0
113?F
(45?C)
95?F
(35?C)
77?F
(25?C)
ELEVATION
FEET
0
50
100
150
METERS
0
15
30
45
ft
m
24
80
18
60
12
40
6
20
0
0
113?F
(45?C)
95?F
(35?C)
77?F
(25?C)
PLAN
F_AC_060102_1_0070101_01_00
Engine Exhaust Temperatures
Ground Idle Power - RR Trent 700 Series Engine
FIGURE-6-1-2-991-007-A01
6-1-2
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A330-700L
Engine Exhaust Velocities Contours - Breakaway Power
1.
This section gives engine exhaust velocities contours at breakaway power.
NOTE : The three values give velocities isolines values at the borders of colored areas.
6-1-3
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
(100 fps = 68 MPH = 109 kmph)
200 fps
ft
m
24
80
18
60
12
40
6
20
0
0
100 fps
50 fps
ELEVATION
0
50
100
150
0
15
30
45
200
250
300
60
75
90
FEET
METERS
(100 fps = 68 MPH = 109 kmph)
ft
m
24
80
18
60
12
40
6
20
0
0
200 fps
100 fps
50 fps
PLAN
F_AC_060103_1_0090101_01_00
Engine Exhaust Velocities
Breakaway Power - RR Trent 700 Series Engine
FIGURE-6-1-3-991-009-A01
6-1-3
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A330-700L
Engine Exhaust Temperatures Contours - Breakaway Power
1.
This section gives engine exhaust temperatures contours at breakaway power.
NOTE : The three values give temperature isolines values at the borders of colored areas.
6-1-4
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ft
m
24
80
18
60
12
40
6
20
0
0
113?F
(45?C)
95?F
(35?C)
77?F
(25?C)
ELEVATION
m
FEET
0
50
100
150
METERS
ft
0
15
30
45
24
80
18
60
12
40
6
20
0
0
113?F
(45?C)
95?F
(35?C)
77?F
(25?C)
PLAN
F_AC_060104_1_0090101_01_00
Engine Exhaust Temperatures
Breakaway Power - RR Trent 700 Series Engine
FIGURE-6-1-4-991-009-A01
6-1-4
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5
Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A330-700L
Engine Exhaust Velocities Contours - Takeoff Power
1.
This section gives engine exhaust velocities contours at takeoff power.
NOTE : The three values give velocities isolines values at the borders of colored areas.
6-1-5
Page 1
Jul 01/21
6-1-5
0
0
40
12
20
60
18
6
80
24
m
0
0
FEET
ELEVATION
ft
PLAN
15
20
6
METERS 0
40
12
50
60
18
ft
0
80
m
24
30
100
45
150
200 fps
200 fps
60
200
75
50 fps
90
300
TO
470 ft
143 m
105
350
TO
1 175 ft
358 m
50 fps
TO
470 ft
143 m
TO
1 175 ft
358 m
(100 fps = 68 MPH = 109 kmph)
250
100 fps
100 fps
(100 fps = 68 MPH = 109 kmph)
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_060105_1_0070101_01_00
Engine Exhaust Velocities
Takeoff Power - RR Trent 700 Series Engine
FIGURE-6-1-5-991-007-A01
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A330-700L
Engine Exhaust Temperatures Contours - Takeoff Power
1.
This section gives engine exhaust temperatures contours at takeoff power.
NOTE : The three values give temperature isolines values at the borders of colored areas.
6-1-6
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
77?F
(25?C)
TO
430 ft
(131 m)
105
90
75
95?F
(35?C)
60
PLAN
30
60
40
20
0
18
12
6
0
ft
80
m
50
15
24
0
0
0
20
6
METERS
40
12
0
60
18
FEET
80
m
24
ft
ELEVATION
100
113?F
(45?C)
113?F
(45?C)
45
150
95?F
(35?C)
200
250
77?F
(25?C)
300
TO
430 ft
(131 m)
350
**ON A/C A330-700L
F_AC_060106_1_0070101_01_00
Engine Exhaust Temperatures
Takeoff Power - RR Trent 700 Series Engine
FIGURE-6-1-6-991-007-A01
6-1-6
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0
Danger Areas of Engines
**ON A/C A330-700L
Danger Areas of Engines
1.
Danger Areas of the Engines.
6-3-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1
Ground Idle Power
**ON A/C A330-700L
Ground Idle Power
1.
This section gives danger areas of the engines at ground idle power conditions.
6-3-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
1m
(3.28 ft)
R=3m
(10 ft)
30?
TO 78 m (256 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA MINIMUM POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
F_AC_060301_1_0070101_01_00
Danger Areas of Engines
RR Trent 700 Series Engine
FIGURE-6-3-1-991-007-A01
6-3-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2
Breakaway Power
**ON A/C A330-700L
Breakaway Power
1.
This section gives danger areas of the engines at breakaway power conditions.
6-3-2
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
R = 7.6 m
(25 ft)
2.4 m
(8 ft)
30?
TO 150 m (492 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA BREAKAWAY POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
F_AC_060302_1_0070101_01_00
Danger Areas of Engines
RR Trent 700 Series Engine
FIGURE-6-3-2-991-007-A01
6-3-2
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-3
Takeoff Power
**ON A/C A330-700L
Take-Off Power
1.
This section gives danger areas of the engines at maximum take-off power conditions.
6-3-3
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
R = 7.6 m
(25 ft)
2.4 m
(8 ft)
30?
TO 640 m (2 100 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA TAKE−OFF POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
F_AC_060303_1_0070101_01_00
Danger Areas of Engines
RR Trent 700 Series Engine
FIGURE-6-3-3-991-007-A01
6-3-3
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0
APU Exhaust Velocities and Temperatures
**ON A/C A330-700L
APU Exhaust Velocities and Temperatures
1.
APU Exhaust Velocities and Temperatures.
6-4-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1
APU
**ON A/C A330-700L
APU - GARRETT
1.
This section gives APU exhaust velocities and temperatures.
6-4-1
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
METERS FEET
204?C
(399?F)
315.5?C
(600?F)
93?C
(200?F)
121?C
(250?F)
40
10
30
20
149?C
(300?F)
177?C
(351?F)
FD
5
10
260?C
427?C (500?F)
(801?F)
METERS
0
0
5
10
15
0
20
FEET
0
10
20
30
40
50
60
18 m/s
(59 ft/s)
METERS FEET
15 m/s
(49 ft/s)
24 m/s
(79 ft/s)
30.5 m/s
(100 ft/s)
40
10
46 m/s
(151 ft/s)
61 m/s
(200 ft/s)
30
20
5
FD
10
METERS
0
0
5
10
15
0
20
FEET
0
10
20
30
40
50
60
F_AC_060401_1_0040101_01_00
Exhaust Velocities and Temperatures
APU -- GARRETT GTCP 331-350
FIGURE-6-4-1-991-004-A01
6-4-1
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-5-0
Pilot Visibility in Approach
**ON A/C A330-700L
Pilot Visibility in Approach
1.
This section gives data about pilot visibility in approach.
Distance
H
H1
H4
Value m (ft)
7.14 m (23.43 ft)
8.91 m (29.23 ft)
7.42 m (24.34 ft)
6-5-0
Page 1
Jul 01/21
IMPACT POINT
OF THE MLG
46?
H
RUNWAY THRESHOLD
H4
H1
LOWEST POINT ON TIRE
NOTE:
H IS THE DISTANCE BETWEEN THE INSTRUMENT LANDING SYSTEM (ILS) BEAM AND THE WHEEL PATH.
H1 IS THE DISTANCE BETWEEN THE PILOT EYE PATH AND THE WHEEL PATH.
H4 IS THE DISTANCE OF THE HEIGHT OF THE PILOT’S EYE RELATIVE TO THE LOW POINT OF THE LANDING GEAR.
PILOT EYE PATH
GLIDESLOPE ILS
MLG PATH
GLIDESLOPE RECEIVER
RUNWAY
46?
GLIDESLOPE TRANSMITTER
PILOT EYE POSITION
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_060500_1_0010101_01_00
Pilot Visibility in Approach
Navigation Aids
FIGURE-6-5-0-991-001-A01
6-5-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0
General Information
**ON A/C A330-700L
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 Main Landing Gear (MLG).
All curves on the charts represent data at a constant specified tire pressure with:
- The aircraft loaded to the Maximum Ramp Weight (MRW),
- The CG at its maximum permissible aft position.
Pavement requirements for commercial aircraft are derived from the static analysis of loads imposed
on the MLG struts.
Landing Gear Footprint:
Section 07-02-00presents basic data on the landing gear footprint configuration, MRW and tire sizes
and pressures.
Maximum Pavement Loads:
Section 07-03-00shows maximum vertical and horizontal pavement loads for certain critical conditions
at the tire-ground interfaces.
Landing Gear Loading on Pavement:
Section 07-04-00contains charts to find these loads throughout the stability limits of the aircraft at
rest on the pavement.
These MLG loads are used as the point of entry to the pavement design charts which follow,
interpolating load values where necessary.
Flexible Pavement Requirements - US Army Corps of Engineers Design Method:
Section 07-05-00uses procedures in Instruction Report No. S-77-1 ”Procedures for Development of
CBR Design Curves”, dated June 1977 and as modified according to the methods described in ICAO
Aerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCN
Method), and utilizing the alpha factors approved by ICAO in October 2007.
The report was prepared by the ”U.S. Army Corps Engineers Waterways Experiment Station, Soils
and Pavement Laboratory, Vicksburg, Mississippi”.
The line showing 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).
Flexible Pavement Requirements - LCN Conversion Method:
The Load Classification Number (LCN) curves are no longer given in section 07-06-00since 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 07-07-00gives the rigid pavement design curves that have been prepared with the use of the
Westergaard Equation.
7-1-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
This is in general accordance with the procedures outlined in the Portland Cement Association
publications, ”Design of Concrete Airport Pavement”, 1973 and ”Computer Program for Airport
Pavement Design” (Program PDILB), 1967 both by Robert G. Packard.
Rigid Pavement Requirements - LCN Conversion:
Section 07-08-00gives the rigid pavement requirements. All LCN curves shown in ’Rigid Pavement
Requirements - Radius of Relative Stiffness (other values of E and µ) - were developed from a
computer program based on data in ICAO document 7920- AN/865/2, Aerodrome manual, Part 2,
”Aerodrome Physical Characteristics”, Second Edition, 1965.
Rigid Pavement Requirements - LCN Conversion - Radius of Relative Stiffness:
The LCN curves are no longer given in section 07-08-00since 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 07-09-00gives ACN data prepared according to the ACN/PCN system as referenced in ICAO
Annex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations” Fourth Edition, July 2004,
incorporating Amendments 1 to 6.
The ACN/PCN system gives a standardized international aircraft/pavement rating system replacing
the various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world.
ACN is the Aircraft Classification Number and PCN is the corresponding Pavement Classification
Number.
An aircraft having an ACN less than or equal to the PCN can operate without restriction on the
pavement.
Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.
The derived single wheel load is defined as the load on a single tire inflated to 1.25 MPa (181 psi)
that would have the same pavement requirements as the aircraft.
Computationally the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1 for
flexible pavements to calculate ACN values.
The Airport Authority must decide on the method of pavement analysis and the results of their
evaluation shown as follows:
PCN
PAVEMENT TYPE
SUBGRADE
TIRE PRESSURE CATEGORY
EVALUATION
CATEGORY
METHOD
R - Rigid
A - High
W - No pressure limit
T - Technical
F - Flexible
B - Medium
X - High pressure limited to 1.75
U - Using Aircraft
MPa (254 psi)
Y - Medium pressure limited to
C - Low
1.25 MPa (181 psi)
D - Ultra Low
Z - Low pressure limited to 0.5
MPa (73 psi)
For flexible pavements, the four subgrade categories (CBR) are:
7-1-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
-
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/m3 (550 pci)
80 MN/m3 (300 pci)
40 MN/m3 (150 pci)
20 MN/m3 (75 pci)
7-1-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0
Landing Gear Footprint
**ON A/C A330-700L
Landing Gear Footprint
1.
This section gives data about the landing gear footprint in relation to the aircraft MRW and tire sizes
and pressures.
The landing-gear footprint information is given for all the operational weight variants of the aircraft.
7-2-0
Page 1
Jul 01/21
MAXIMUM
RAMP
WEIGHT
A330−700L 227 900 kg
ZCG −0.5 m (502 425 lb)
A330−700L 227 900 kg
ZCG −0.4 m (502 425 lb)
A330−700L 227 900 kg
ZCG 0 m (502 425 lb)
A330−700L 227 900 kg
ZCG 0.4 m (502 425 lb)
A330−700L 202 300 kg
ZCG 0.6 m (446 000 lb)
CG
HEIGHT
0.71 m
(2.33 ft)
7-2-0
1 050x395R16 28PR
1 050x395R16 28PR
1 050x395R16 28PR
90.9%
91.7%
1 050x395R16 28PR
91.7%
91.7%
1 050x395R16 28PR
91.7%
PERCENTAGE
OF WEIGHT
NOSE GEAR TIRE
ON MAIN
SIZE
GEAR GROUP
22.19 m
(72.80 ft)
12.7 bar
(184 psi)
12.7 bar
(184 psi)
12.7 bar
(184 psi)
12.7 bar
(184 psi)
12.7 bar
(184 psi)
1 400x530R23 36PR
1 400x530R23 36PR
1 400x530R23 36PR
1 400x530R23 36PR
1 400x530R23 36PR
NOSE GEAR MAIN GEAR TIRE
TIRE
SIZE
PRESSURE
1.40 m
(4.59 ft)
14.2 bar
(206 psi)
14.2 bar
(206 psi)
14.2 bar
(206 psi)
14.2 bar
(206 psi)
14.2 bar
(206 psi)
MAIN GEAR
TIRE
PRESSURE
1.98 m
(6.50 ft)
10.68 m
(35.04 ft)
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070200_1_0560101_01_00
Landing Gear Footprint
FIGURE-7-2-0-991-056-A01
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0
Maximum Pavement Loads
**ON A/C A330-700L
Maximum Pavement Loads
1.
This section gives 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
Jul 01/21
7-3-0
42 440 kg
(93 575 lb)
20.6 %
MAC
(a)
NOTE:
(a) LOADS CALCULATED USING AIRCRAFT AT MRW.
(b) BRAKED MAIN GEAR.
202 300 kg 23 650 kg
ZCG 0.6 m (446 000 lb) (52 150 lb)
227 900 kg 24 700 kg
ZCG 0.4 m (502 425 lb) (54 450 lb)
39 970 kg
(88 125 lb)
41 170 kg
(90 775 lb)
20.6 %
MAC
(a)
227 900 kg 24 700 kg
(502 425 lb) (54 450 lb)
18 %
MAC
(a)
39 890 kg
(87 950 lb)
20.6 %
MAC
(a)
227 900 kg 24 700 kg
ZCG −0.4 m (502 425 lb) (54 450 lb)
ZCG 0 m
38 150 kg
(84 100 lb)
22.5 %
MAC
(a)
STATIC BRAKING
AT 10 ft/s?
DECELERATION
4
227 900 kg 23 280 kg
ZCG −0.5 m (502 425 lb) (51 325 lb)
STATIC LOAD AT
MOST FWD CG
MAXIMUM
RAMP
WEIGHT
CG
HEIGHT
V (NG)
3
2
1
26 %
MAC
(a)
28.2 %
MAC
(a)
28.2 %
MAC
(a)
28.2 %
MAC
(a)
92 710 kg 28.2 %
(204 400 lb) MAC
(a)
103 620 kg
(228 450 lb)
104 440 kg
(230 250 lb)
104 440 kg
(230 250 lb)
104 440 kg
(230 250 lb)
STATIC LOAD AT
MAX AFT CG
5
V(MG) (PER STRUT)
31 440 kg
(b)
(69 325 lb)
35 420 kg
(b)
(78 100 lb)
35 420 kg
(b)
(78 100 lb)
35 420 kg
(b)
(78 100 lb)
35 420 kg
(b)
(78 100 lb)
74 160 kg
(b)
(163 500 lb)
82 890 kg
(b)
(182 750 lb)
83 550 kg
(b)
(184 200 lb)
83 550 kg
(b)
(184 200 lb)
83 550 kg
(b)
(184 200 lb)
STEADY BRAKING AT INSTANTANEOUS
AT 10 ft/s?
BRAKING
DECELERATION COEFFICIENT = 0.8
6
H (PER STRUT)
V(MG)
V (NG)
V(NG) MAXIMUM VERTICAL NOSE GEAR GROUND LOAD AT MOST FWD CG
V(MG) MAXIMUM VERTICAL MAIN GEAR GROUND LOAD AT MOST AFT CG
H MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING
H
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070300_1_0220101_01_00
Maximum Pavement Loads
FIGURE-7-3-0-991-022-A01
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0
Landing Gear Loading on Pavement
**ON A/C A330-700L
Landing Gear Loading on Pavement
1.
This section gives data about the landing gear loading on pavement.
The MLG loading on pavement graphs are given at standard tire pressure for all the aircraft
operational weight variants.
Example, see FIGURE 7-4-0-991-015-A(Sheet 5), calculation of the total weight on the MLG for:
- An aircraft with a MRW of 202 300 kg (446 000 lb),
- The aircraft gross weight is 195 000 kg (429 900 lb),
- A percentage of weight on the MLG of 91.65% (percentage of weight on the MLG at MRW and
maximum aft CG at MRW).
The total weight on the MLG group is 178 720 kg (394 000 lb).
NOTE : The CG in the figure title is the CG used for ACN/LCN calculation.
7-4-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
15
20
PERCENTAGE MAC
25
30
35
40
45
50
250
250
550
240
240
MTOW − 227 000 kg
CG FOR ACN/LCN
CALCULATION
28.2% MAC
500
220
220
22.5% MAC
210
450
200
200
190
190
180
180
MLW
170
170
160
160
150
400
(x 1 000 lb)
AIRCRAFT GROSS WEIGHT
210
230
(x 1 000 kg)
WEIGHT ON MAIN LANDING GEAR x 1 000 kg
230
350
150
MZFW
140
140
300
130
130
120
86
88
90
92
94
96
98
120
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
F_AC_070400_1_0150101_01_00
Landing Gear Loading on Pavement
WVZCG -0.5 m, MRW 227 900 kg, CG 28.2% (Sheet 1 of 5)
FIGURE-7-4-0-991-015-A01
7-4-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
15
20
PERCENTAGE MAC
25
30
35
40
45
50
250
250
550
240
240
MTOW − 227 000 kg
CG FOR ACN/LCN
CALCULATION
28.2% MAC
500
220
220
20.6% MAC
210
450
200
200
190
190
180
180
MLW
170
170
160
160
150
400
(x 1 000 lb)
AIRCRAFT GROSS WEIGHT
210
230
(x 1 000 kg)
WEIGHT ON MAIN LANDING GEAR (x 1 000 kg)
230
350
150
MZFW
140
140
300
130
130
120
86
88
90
92
94
96
98
120
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
F_AC_070400_1_0150102_01_00
Landing Gear Loading on Pavement
WVZCG -0.4 m, MRW 227 900 kg, CG 28.2% (Sheet 2 of 5)
FIGURE-7-4-0-991-015-A01
7-4-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
15
20
PERCENTAGE MAC
25
30
35
40
45
50
250
250
550
240
240
MTOW − 227 000 kg
CG FOR ACN/LCN
CALCULATION
28.2% MAC
500
220
220
20.6% MAC
210
450
200
200
190
190
180
180
MLW
170
170
160
160
150
400
(x 1 000 lb)
AIRCRAFT GROSS WEIGHT
210
230
(x 1 000 kg)
WEIGHT ON MAIN LANDING GEAR (x 1 000 kg)
230
350
150
MZFW
140
140
300
130
130
120
86
88
90
92
94
96
98
120
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
F_AC_070400_1_0150103_01_00
Landing Gear Loading on Pavement
WVZCG 0 m, MRW 227 900 kg, CG 28.2% (Sheet 3 of 5)
FIGURE-7-4-0-991-015-A01
7-4-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
15
PERCENTAGE MAC
25
30
35
40
20
45
50
250
250
550
240
240
MTOW − 227 000 kg
CG FOR ACN/LCN
CALCULATION
26% MAC
500
220
220
210
230
20.6% MAC
210
200
190
190
180
180
MLW
170
170
160
160
400
350
(x 1 000 lb)
AIRCRAFT GROSS WEIGHT
450
200
(x 1 000 kg)
WEIGHT ON MAIN LANDING GEAR (x 1 000 kg)
230
150
150
MZFW
140
140
300
130
130
120
86
88
90
92
94
96
98
120
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
F_AC_070400_1_0150104_01_00
Landing Gear Loading on Pavement
WVZCG 0.4 m, MRW 227 900 kg, CG 26% (Sheet 4 of 5)
FIGURE-7-4-0-991-015-A01
7-4-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
15
20
PERCENTAGE MAC
25
30
35
40
45
50
250
250
240
240
230
230
550
220
210
MTOW − 202 300 kg
CG FOR ACN/LCN
CALCULATION
28.2% MAC
450
200
200
190
210
190
18% MAC
180
180
MLW
170
170
160
160
150
400
(x 1 000 lb)
AIRCRAFT GROSS WEIGHT
220
(x 1 000 kg)
WEIGHT ON MAIN LANDING GEAR (x 1 000 kg)
500
350
150
MZFW
140
140
300
130
130
120
86
88
90
92
94
96
98
120
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
F_AC_070400_1_0150105_01_00
Landing Gear Loading on Pavement
WVZCG 0.6 m, MRW 202 300 kg, CG 28.2% (Sheet 5 of 5)
FIGURE-7-4-0-991-015-A01
7-4-0
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A330-700L
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
1.
This section gives data about the flexible pavement requirements.
The flexible pavement requirements graphs are given at standard tire pressure for all the aircraft
operational weight variants.
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 7-5-0-991-013-A(Sheet 3), calculation of the thickness of the flexible pavement
for:
- An aircraft with a Maximum Ramp Weight (MRW) of 202 300 kg (446 000 lb),
- A ”CBR” value of 10,
- An annual departure level of 3 000,
- The load on one MLG of 80 000 kg (176 375 lb).
The required flexible pavement thickness is 59.4 cm (23 in).
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-5-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
3
SUBGRADE STRENGTH − CBR
10
15
20
30
6
40
60
80
WEIGHT ON ONE MAIN LANDING GEAR
104 440 kg (230 250 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
70 000 kg (154 325 lb)
60 000 kg (132 275 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
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
F_AC_070500_1_0130101_01_00
Flexible Pavement Requirements
WVZCG -0.5 m, WVZCG -0.4 m, WVZCG 0 m, MRW 227 900 kg, CG 28.2% (Sheet 1 of 3)
FIGURE-7-5-0-991-013-A01
7-5-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
3
SUBGRADE STRENGTH − CBR
10
15
20
30
6
40
60
80
WEIGHT ON ONE MAIN LANDING GEAR
103 620 kg (228 450 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
70 000 kg (154 325 lb)
60 000 kg (132 275 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
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
F_AC_070500_1_0130102_01_00
Flexible Pavement Requirements
WVZCG 0.4 m, MRW 227 900 kg, CG 26% (Sheet 2 of 3)
FIGURE-7-5-0-991-013-A01
7-5-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
SUBGRADE STRENGTH − CBR
3
6
10
15
20
30
40
60
80
WEIGHT ON ONE MAIN LANDING GEAR
92 710 kg (204 400 lb)
80 000 kg (176 375 lb)
70 000 kg (154 325 lb)
60 000 kg (132 275 lb)
50 000 kg (110 225 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
1 400 x 530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
F_AC_070500_1_0130103_01_00
Flexible Pavement Requirements
WVZCG 0.6 m, MRW 202 300 kg, CG 28.2% (Sheet 3 of 3)
FIGURE-7-5-0-991-013-A01
7-5-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0
Flexible Pavement Requirements - LCN Conversion
**ON A/C A330-700L
Flexible Pavement Requirements - LCN Conversion
1.
The Load Classification Number (LCN) curves are no longer provided in section 07-06-00since 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
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0
Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A330-700L
Rigid Pavement Requirements - Portland Cement Association Design Method
1.
This section gives data about the rigid pavement requirements for the PCA (Portland Cement
Association) design method.
The rigid pavement requirements graphs are given at standard tire pressure for all the aircraft
operational weight variants.
They are calculated with the PCA design method.
To find a rigid pavement thickness, you must know the Subgrade Modulus (k), the permitted working
stress and the weight on one MLG.
The procedure that follows is used to develop rigid pavement design curves:
- With the scale for pavement thickness on the left and the scale for permitted working stress on
the right, a random load line is made. This represents the MLG maximum weight to be shown,
- A plot is then made of all values of the subgrade modulus (k values),
- More load lines for the incremental values of the weight on the MLG are made based on the
curve for k = 80 MN/m3, which is already shown on the graph.
Example, see FIGURE 7-7-0-991-012-A(sheet 3), calculation of the thickness of the rigid pavement
for:
- An aircraft with a Maximum Ramp Weight (MRW) of 202 300 kg (446 000 lb),
- A k value of 80 MN/m3 (300 lbf/in3),
- A permitted working stress of 38.67 kg/cm2 (550 lb/in2),
- The load on one MLG is 80 000 kg (176 375 lb).
The required rigid pavement thickness is 230 mm (9 in).
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-7-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
15
38
36
14
900
k = 20 MN/m?
k = 40 MN/m?
k = 80 MN/m?
k = 150 MN/m?
63
58
800
MAXIMUM POSSIBLE MAIN
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
34
53
13
700
12
600
48
28
26
11
500
10
(lb/in?)
38
400
24
28
23
9
300
18
22
8
20
18
33
(kg/cm?)
ALLOWABLE WORKING STRESS
43
30
(in)
RIGID PAVEMENT THICKNESS
(cm)
32
WEIGHT ON ONE MAIN
LANDING GEAR
104 440 kg (230 250 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
70 000 kg (154 325 lb)
60 000 kg (132 275 lb)
7
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/m? BUT DEVIATE SLIGHTLY
FOR ANY OTHER VALUES OF k.
200
100
13
8
REFERENCE:
"DESIGN OF CONCRETE AIRPORT
PAVEMENTS" AND "COMPUTER
PROGRAM FOR AIRPORT
PAVEMENT DESIGN − PROGRAM
PDILB" PORTLAND CEMENT
ASSOCIATION.
F_AC_070700_1_0120101_01_00
Rigid Pavement Requirements
WVZCG -0.5 m, WVZCG -0.4 m, WVZCG 0 m, MRW 227 900 kg, CG 28.2% (Sheet 1 of 3)
FIGURE-7-7-0-991-012-A01
7-7-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
15
38
36
14
900
k = 20 MN/m?
k = 40 MN/m?
k = 80 MN/m?
k = 150 MN/m?
63
58
800
MAXIMUM POSSIBLE MAIN
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
34
53
13
700
12
600
48
28
26
11
500
10
(lb/in?)
38
400
24
28
23
9
300
18
22
8
20
18
33
(kg/cm?)
ALLOWABLE WORKING STRESS
43
30
(in)
RIGID PAVEMENT THICKNESS
(cm)
32
WEIGHT ON ONE MAIN
LANDING GEAR
103 610 kg (228 425 lb)
90 000 kg (198 425 lb)
80 000 kg (176 375 lb)
70 000 kg (154 325 lb)
60 000 kg (132 275 lb)
200
7
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/m? BUT DEVIATE SLIGHTLY
FOR ANY OTHER VALUES OF k.
100
13
8
REFERENCE:
"DESIGN OF CONCRETE AIRPORT
PAVEMENTS" AND "COMPUTER
PROGRAM FOR AIRPORT
PAVEMENT DESIGN − PROGRAM
PDILB" PORTLAND CEMENT
ASSOCIATION.
F_AC_070700_1_0120102_01_00
Rigid Pavement Requirements
WVZCG 0.4 m, MRW 227 900 kg, CG 26% (Sheet 2 of 3)
FIGURE-7-7-0-991-012-A01
7-7-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
15
38
36
14
900
k = 20 MN/m?
k = 40 MN/m?
k = 80 MN/m?
k = 150 MN/m?
63
58
800
MAXIMUM POSSIBLE MAIN
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
34
53
13
700
12
600
48
28
26
11
500
10
(lb/in?)
38
400
24
28
23
9
300
18
22
8
20
18
33
(kg/cm?)
ALLOWABLE WORKING STRESS
43
30
(in)
RIGID PAVEMENT THICKNESS
(cm)
32
WEIGHT ON ONE MAIN
LANDING GEAR
92 710 kg (204 375 lb)
80 000 kg (176 375 lb)
70 000 kg (154 325 lb)
60 000 kg (132 275 lb)
50 000 kg (110 225 lb)
200
7
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/m? BUT DEVIATE SLIGHTLY
FOR ANY OTHER VALUES OF k.
100
13
8
REFERENCE:
"DESIGN OF CONCRETE AIRPORT
PAVEMENTS" AND "COMPUTER
PROGRAM FOR AIRPORT
PAVEMENT DESIGN − PROGRAM
PDILB" PORTLAND CEMENT
ASSOCIATION.
F_AC_070700_1_0120103_01_00
Rigid Pavement Requirements
WVZCG 0.6 m, MRW 202 300 kg, CG 28.2% (Sheet 3 of 3)
FIGURE-7-7-0-991-012-A01
7-7-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-0
Rigid Pavement Requirements - LCN Conversion
**ON A/C A330-700L
Rigid Pavement Requirements - LCN Conversion
1.
The Load Classification Number (LCN) curves are no longer provided in section 07-08-00since 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
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0
ACN/PCN Reporting System - Flexible and Rigid Pavements
**ON A/C A330-700L
Aircraft Classification Number - Flexible and Rigid Pavements
1.
This section gives data about the Aircraft Classification Number (ACN) for an aircraft gross weight in
relation to a subgrade strength value for flexible and rigid pavement.
The flexible and rigid pavement requirements graphs are given at standard tire pressure for all the
aircraft operational weight variants.
To find the ACN of an aircraft on flexible and rigid pavement, you must know the aircraft gross
weight and the subgrade strength.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on that
pavement, subject to any limitation on the tire pressure.
(Ref: ICAO Aerodrome Design Manual, Part 3, Chapter 1, Second Edition 1983).
Example, see FIGURE 7-9-0-991-031-A(sheet 1), calculation of the ACN for flexible pavement for:
- An aircraft with a MRW of 202 300 kg (446 000 lb),
- An aircraft gross weight of 195 000 kg (429 900 lb),
- A medium subgrade strength (code B).
The ACN for flexible pavement is 48.
Example, see FIGURE 7-9-0-991-031-A(sheet 2), calculation of the ACN for rigid pavement for:
- An aircraft with a MRW of 202 300 kg (446 000 lb),
- An aircraft gross weight of 195 000 kg (429 900 lb),
- A medium subgrade strength (code B).
The ACN for rigid pavement is 47.
Aircraft Classification Number - ACN table
The table in FIGURE 7-9-0-991-028-Agives 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 - 130 000 kg)/(MRW - 130
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 = 130 000 kg + (MRW - 130 000 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
130 000 kg.
7-9-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
ACN FOR
ACN FOR
LOAD ON
RIGID PAVEMENT
FLEXIBLE PAVEMENT
TIRE
MRW/OWE ONE MAIN
SUBGRADES − MN/m?
SUBGRADES − CBR
AIRCRAFT TYPE MASS (kg) GEAR LEG PRESSURE
(MPa)
High Medium Low Ultra−low High Medium Low Ultra−low
(%)
150
80
40
20
15
10
6
3
A330−700L
WVZCG −0.5 m
227 900
45.80
130 000
45.80
A330−700L
WVZCG −0.4 m
227 900
45.80
130 000
45.80
A330−700L
WVZCG 0 m
227 900
45.80
130 000
45.80
A330−700L
WVZCG 0.4 m
227 900
45.50
130 000
45.50
A330−700L
WVZCG 0.6 m
202 300
45.80
130 000
45.80
1.42
1.42
1.42
1.42
1.42
68
79
54
58
29
32
57
68
37
28
79
54
29
29
32
37
28
49
29
57
68
79
29
32
37
49
57
67
79
29
28
32
37
43
49
58
68
29
29
32
37
49
57
29
49
67
90
29
31
39
58
67
90
29
31
39
54
58
67
90
28
29
31
39
53
58
66
89
27
29
31
39
47
50
57
76
28
29
31
39
F_AC_070900_1_0280101_01_00
Aircraft Classification Number
ACN Table
FIGURE-7-9-0-991-028-A01
7-9-0
Page 2
Jul 01/21
7-9-0
0
10
20
30
40
50
60
70
80
90
100
110
120
120
300
320
340
130
140
150
SUBGRADE STRENGTH
D − CBR 3 (ULTRA LOW)
C − CBR 6 (LOW)
B − CBR 10 (MEDIUM)
A − CBR 15 (HIGH)
ALPHA FACTOR = 0.8
280
160
360
420
180
190
(x 1 000 kg)
400
(x 1 000 lb)
200
440
AIRCRAFT GROSS WEIGHT
170
380
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
210
460
220
480
230
500
240
520
540
ACN WAS DETERMINED AS REFERENCED IN
ICAO AERODROME DESIGN MANUAL PART 3
CHAPTER 1. SECOND EDITION 1983.
250
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070900_1_0290101_01_00
Aircraft Classification Number
Flexible Pavement - WVZCG -0.5 m, WVZCG -0.4 m, WVZCG 0 m, MRW 227 900 kg, CG 28.2% (Sheet 1 of 2)
FIGURE-7-9-0-991-029-A01
Page 3
Jul 01/21
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7-9-0
0
10
20
30
40
50
60
70
80
90
100
110
120
120
300
320
340
130
140
150
360
160
SUBGRADE STRENGTH
D − k = 20 MN/m? (ULTRA LOW)
C − k = 40 MN/m? (LOW)
B − k = 80 MN/m? (MEDIUM)
A − k = 150 MN/m? (HIGH)
280
190
420
(x 1 000 kg)
180
400
(x 1 000 lb)
200
440
AIRCRAFT GROSS WEIGHT
170
380
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
210
460
220
480
230
500
240
520
540
ACN WAS DETERMINED AS REFERENCED IN
ICAO AERODROME DESIGN MANUAL PART 3
CHAPTER 1. SECOND EDITION 1983.
250
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070900_1_0290102_01_00
Aircraft Classification Number
Rigid Pavement - WVZCG -0.5 m, WVZCG -0.4 m, WVZCG 0 m, MRW 227 900 kg, CG 28.2% (Sheet 2 of 2)
FIGURE-7-9-0-991-029-A01
Page 4
Jul 01/21
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7-9-0
0
10
20
30
40
50
60
70
80
90
100
110
120
120
300
320
340
130
140
150
SUBGRADE STRENGTH
D − CBR 3 (ULTRA LOW)
C − CBR 6 (LOW)
B − CBR 10 (MEDIUM)
A − CBR 15 (HIGH)
ALPHA FACTOR = 0.8
280
160
360
190
420
(x 1 000 kg)
180
400
(x 1 000 lb)
200
440
AIRCRAFT GROSS WEIGHT
170
380
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
210
460
220
480
230
500
240
520
540
ACN WAS DETERMINED AS REFERENCED IN
ICAO AERODROME DESIGN MANUAL PART 3
CHAPTER 1. SECOND EDITION 1983.
250
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070900_1_0300101_01_00
Aircraft Classification Number
Flexible Pavement - WVZCG 0.4 m, MRW 227 900 kg, CG 26% (Sheet 1 of 2)
FIGURE-7-9-0-991-030-A01
Page 5
Jul 01/21
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7-9-0
0
10
20
30
40
50
60
70
80
90
100
110
120
120
130
280
140
300
340
360
380
400
150
160
190
(x 1 000 kg)
180
200
440
AIRCRAFT GROSS WEIGHT
170
420
(x 1 000 lb)
SUBGRADE STRENGTH
D − k = 20 MN/m? (ULTRA LOW)
C − k = 40 MN/m? (LOW)
B − k = 80 MN/m? (MEDIUM)
A − k = 150 MN/m? (HIGH)
320
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
210
460
220
480
230
500
240
520
540
ACN WAS DETERMINED AS REFERENCED IN
ICAO AERODROME DESIGN MANUAL PART 3
CHAPTER 1. SECOND EDITION 1983.
250
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070900_1_0300102_01_00
Aircraft Classification Number
Rigid Pavement - WVZCG 0.4 m, MRW 227 900 kg, CG 26% (Sheet 2 of 2)
FIGURE-7-9-0-991-030-A01
Page 6
Jul 01/21
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7-9-0
0
10
20
30
40
50
60
70
80
90
100
110
120
120
300
320
340
130
140
150
SUBGRADE STRENGTH
D − CBR 3 (ULTRA LOW)
C − CBR 6 (LOW)
B − CBR 10 (MEDIUM)
A − CBR 15 (HIGH)
ALPHA FACTOR = 0.8
280
160
360
420
180
190
(x 1 000 kg)
400
(x 1 000 lb)
200
440
AIRCRAFT GROSS WEIGHT
170
380
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
210
460
220
480
230
500
240
520
540
ACN WAS DETERMINED AS REFERENCED IN
ICAO AERODROME DESIGN MANUAL PART 3
CHAPTER 1. SECOND EDITION 1983.
250
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070900_1_0310101_01_00
Aircraft Classification Number
Flexible Pavement - WVZCG 0.6 m, MRW 202 300 kg, CG 28.2% (Sheet 1 of 2)
FIGURE-7-9-0-991-031-A01
Page 7
Jul 01/21
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7-9-0
0
10
20
30
40
50
60
70
80
90
100
110
120
120
300
320
340
130
140
150
360
160
SUBGRADE STRENGTH
D − k = 20 MN/m? (ULTRA LOW)
C − k = 40 MN/m? (LOW)
B − k = 80 MN/m? (MEDIUM)
A − k = 150 MN/m? (HIGH)
280
190
420
(x 1 000 kg)
180
400
(x 1 000 lb)
200
440
AIRCRAFT GROSS WEIGHT
170
380
1 400x530R23 PR36 TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
210
460
220
480
230
500
240
520
540
ACN WAS DETERMINED AS REFERENCED IN
ICAO AERODROME DESIGN MANUAL PART 3
CHAPTER 1. SECOND EDITION 1983.
250
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_070900_1_0310102_01_00
Aircraft Classification Number
Rigid Pavement - WVZCG 0.6 m, MRW 202 300 kg, CG 28.2% (Sheet 2 of 2)
FIGURE-7-9-0-991-031-A01
Page 8
Jul 01/21
AIRCRAFT CLASSIFICATION NUMBER (ACN)
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0
SCALED DRAWINGS
**ON A/C A330-700L
Scaled Drawings
1.
This section gives the scaled drawings.
NOTE : When printing this drawing, make sure to adjust for proper scaling.
8-0-0
Page 1
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
0
0
4
10
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.
F_AC_080000_1_0070101_01_00
Scaled Drawing
FIGURE-8-0-0-991-007-A01
8-0-0
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0
AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A330-700L
Aircraft Rescue and Fire Fighting
1.
Aircraft Rescue and Fire Fighting Charts
This sections gives the 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
Jul 01/21
L
10-0-0
AIRBUS S.A.S. 2018 . All rights reserved.
JAN 2020
F_RF_000000_1_A33070L
THIS CHART GIVES THE GENERAL LAYOUT OF THE A330−700L 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.
7
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0860101_01_00
Front Page
FIGURE-10-0-0-991-086-A01
Page 2
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0870101_01_01
Highly Flammable and Hazardous Materials and Components
FIGURE-10-0-0-991-087-A01
10-0-0
Page 3
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B
FR57.2
FR57.1
ACCESS VIA
CARGO
COMPARTMENT
DOOR 823
ELT
ELT ANTENNA
ACCESS VIA
COCKPIT HATCH 851
Z120
FR0
A
B
C
FR21
A
BATTERY 2
C
BATTERY 1
D
FR60
FR73
Z160
D
ACCESS VIA
COCKPIT HATCH 851
BATTERY APU
**ON A/C A330-700L
F_AC_100000_1_0880101_01_00
Batteries Location and Access
FIGURE-10-0-0-991-088-A01
10-0-0
Page 4
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
01
RISK OF DIRECT
PROJECTION
01
01
02
100 m (328 ft)
120?
RISK OF INDIRECT
PROJECTION
02 30?
100 m (328 ft)
120?
RISK OF DIRECT
PROJECTION
RISK OF INDIRECT
PROJECTION
02 30?
**ON A/C A330-700L
F_AC_100000_1_0890101_01_01
Wheel/Brake Overheat
Wheel Safety Area (Sheet 1 of 2)
FIGURE-10-0-0-991-089-A01
10-0-0
Page 5
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0890102_01_00
Wheel/Brake Overheat
Recommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-089-A01
10-0-0
Page 6
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
A
A
B
B
**ON A/C A330-700L
F_AC_100000_1_0910101_01_00
Ground Lock Safety-Devices
FIGURE-10-0-0-991-091-A01
10-0-0
Page 7
Jul 01/21
10-0-0
A
A
CURTAIN BETWEEN COURIER
AREA AND COCKPIT
B
01
LAVATORY
COURIER
AREA
03
02
B
EMERGENCY EVACUATION THROUGH COCKPIT SLIDING WINDOWS
LOCATED ON BOTH A/C SIDES WITH THE ESCAPE ROPE.
BELLY DOOR
02
PRESSURE BULKHEAD DOOR
ACCESS DOOR BETWEEN COURIER
AREA AND FORWARD CARGO HOLD
LIFE RAFT IS LOCATED INSIDE THE COURIER AREA, NEAR TO THE COCKPIT CURTAIN.
VIEW LOOKING FORWARD
NOTE:
01 ESCAPE ROPES ARE LOCATED ON BOTH A/C SIDES BEHIND THE CEILING PANELS.
01
03
03
COCKPIT
CARGO
ACCESS
DOOR
EMERGENCY EVACUATION
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0920101_01_01
Emergency Evacuation Devices
FIGURE-10-0-0-991-092-A01
Page 8
Jul 01/21
10-0-0
HANDLE
A
BUTTON
A
ESCAPE ROPE STORAGE
EVACUATION FROM THE INTERIOR BY SLIDING
WINDOWS
− PUSH THE BUTTON AND PULL THE HANDLE
UNTIL IT STOP TO OPEN THE SLIDING WINDOW
− USE THE ESCAPE ROPE TO GET DOWN
A
ACCESS FROM THE EXTERIOR BY SLIDING
WINDOWS
− TURN THE HANDLE TO OPEN
− PUSH WINDOW INWARD THEN SLIDE
AFTWARD
HANDLE
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_1010101_01_00
Sliding Windows Evacuation
FIGURE-10-0-0-991-101-A01
Page 9
Jul 01/21
A
BELLY DOOR IN OPEN POSITION
BELLY DOOR IN CLOSED POSITION
B
FLAP
A
10-0-0
B
INDICATOR FLAG
DOOR OPENING:
1 − PUSH THE FLAP TO HOLD HANDLE AND INNER GRIP.
2 − PUSH THE INNER GRIP.
3 − PULL THE HANDLE FULLY DOWN.
4 − EXTEND THE FOLDABLE STAIR BY HAND.
5 − CHECK THAT INDICATOR FLAGS ARE OUT.
FWD
INNER GRID
HANDLE
BELLY DOOR EXTERIOR CONTROL HANDLE
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0930101_01_01
Belly-Door Exterior Control-Handle
FIGURE-10-0-0-991-093-A01
Page 10
Jul 01/21
10-0-0
B
UNLOCKED
POSITION
OPEN THE BELLY DOOR FROM THE INSIDE
LOCKED
POSITION
HANDLE
A
C
UNLOCKED
POSITION
LOCKING
INDICATORS
B
OPEN THE BELLY DOOR FROM THE INSIDE
LOCKED
POSITION
F
W
D
NOTE:
1 − PULL THE LOCK HANDLE UP.
2 − MAKE SURE THAT THE LOCKING INDICATORS SHOW RED AND WHITE STRIPES.
3 − PUSH THE HANDLE UNTIL IT STOPS.
4 − MAKE SURE THAT THE BELLY DOOR IS IN FULL DOWN POSITION.
5 − PUSH THE STAIR HANDLE TO DEPLOY THE MOBILE STAIRS.
LOCK
HANDLE
Z130
A
C
HANDLE
STAIR
HANDLE
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_1020101_01_00
Belly-Door Interior Control-Handle
FIGURE-10-0-0-991-102-A01
Page 11
Jul 01/21
HANDLE
HANDLE
B
A
10-0-0
1 − TURN THE HANDLE COUNTERCLOCKWISE.
2 − MAKE SURE THAT GREEN LINE ON HANDLE AND RED
LINE ON DOOR LINING ARE ALIGNED.
3 − MAKE SURE THAT THE VISUAL INDICATOR SHOWS
A RED TARGET.
4 − PULL THE PRESSURE BULKHEAD DOOR.
1 − TURN THE HANDLE CLOCKWISE.
2 − MAKE SURE THAT GREEN LINE ON HANDLE AND RED
LINE ON DOOR LINING ARE ALIGNED.
3 − PUSH THE PRESSURE BULKHEAD DOOR.
OPENING OF THE PRESSURE BULKHEAD DOOR FROM
COURIER AREA
VISUAL INDICATOR
C
Z132
OPENING OF THE PRESSURE BULKHEAD DOOR FROM
FORWARD COMPARTMENT AREA
A
B
FR21
C
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_1030101_01_00
Pressure Bulkhead Door
FIGURE-10-0-0-991-103-A01
Page 12
Jul 01/21
10-0-0
B
B
F
W
D
OPEN THIS DOOR
BEFORE TO ACCESS TO
CARGO ACCESS DOOR
A
VIEW LOOKING DOWNWARD
EXTERNAL HANDLE
IN "CLOSED" POSITION
CARGO ACCESS DOOR
DOOR IN
"CLOSED"
POSITION.
VIEW LOOKING BACKWARD
C
VIEW LOOKING BACKWARD
A
C
MAIN DECK ACCESS DOOR
DOOR IN
"OPEN"
POSITION
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0940101_01_01
Main-Deck Access Door
FIGURE-10-0-0-991-094-A01
Page 13
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B
196BB
7155JE
FWD
197CB
A C
B
F
W
D
C
FWD
D
A
E
E
D
152NR
**ON A/C A330-700L
F_AC_100000_1_0950101_01_00
Aft-Cargo-Compartment Door Controls
FIGURE-10-0-0-991-095-A01
10-0-0
Page 14
Jul 01/21
FR18A
10-0-0
FWD
B
B
A
C
C
MAIN DECK CARGO DOOR
OUTER OPERATION PANEL
MAIN DECK CARGO DOOR
INNER OPERATION PANEL
FR21 FR19A
FR21A
A
FWD
C
"OPEN/CLOSE"
TOGGLE SWITCH
TYPICAL
MAIN DECK CARGO DOOR
OPERATION PANEL
"FAULT"
WARNING LIGHT
"FULLY
OPEN"
LIGHT
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0960101_01_01
Main-Deck Cargo Door-Control
FIGURE-10-0-0-991-096-A01
Page 15
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
C
C
A
D
A
B
B
121EL
D
198DB
**ON A/C A330-700L
F_AC_100000_1_0970101_01_01
Control Panels
FIGURE-10-0-0-991-097-A01
10-0-0
Page 16
Jul 01/21
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOTE:
IF THERE IS AN APU FIRE:
− YOU CAN GO ON THE 990 VU PANEL TO CUT THE APU ALIMENTATION.
− YOU CAN APPLY EXTINGUISHER DIRECTLY ON THE APU AIR INTAKE.
FWD
A
A
198DB
B
B
**ON A/C A330-700L
F_AC_100000_1_1040101_01_00
APU Air Intake
FIGURE-10-0-0-991-104-A01
10-0-0
Page 17
Jul 01/21
10-0-0
BF3
BF2
N1 BF1
F2
FWD CG (18%)
m
ft
17.18
56.36
12.37
40.58
5.09
16.70
3.31
10.86
3.36
11.02
19.21
63.02
7.16
23.49
7.12
23.36
AFT CG (25%)
m
ft
17.25 56.59
12.43 40.78
5.16
16.93
3.27
10.73
3.30
10.83
19.10 62.66
7.06
23.16
7.02
23.03
135 000 kg (297 625 lb)
WINGS
NACELLE
FUSELAGE
F1
F2
BF1
BF2
BF3
CP1
N1 (RR)
W1
W2
A/C CONFIGURATION
F1
D2 D1
CP1
FWD CG (18%)
m
ft
1.28
4.20
13.02
42.72
2.11
6.92
2.11
6.92
2.15
7.05
3.77
12.37
1.04
3.41
8.18
26.84
6.81
22.34
AFT CG (25%)
m
ft
1.35
4.43
13.06 42.85
2.12
6.96
2.11
6.92
2.14
7.02
3.84
12.60
1.05
3.44
8.14
26.71
6.77
22.21
135 000 kg (297 625 lb)
D3
NOTE:
CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
TAIL PLANE
D1
D2
D3
C1
C2
VT
HT
AP
A/C CONFIGURATION
DOORS
W1 W2
C2 C1
DIMENSIONS ARE RELATED TO AIRCRAFT WEIGHT AND CG CONFIGURATION
VT AP HT
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_0990101_01_00
Ground Clearances
FIGURE-10-0-0-991-099-A01
Page 18
Jul 01/21
10-0-0
B
B
NOTE:
1 − THE BREAK IN SURFACE SHALL PERMIT ACCESS FROM OUTSIDE IN ORDER TO RESCUE PERSONNEL TO GET IN
AND TAKE VICTIMS OUT OF THE DAMAGED AIRCRAFT.
2 − RESCUE TEAM WOULD USE AN AXE OR A GRINDER TO CLEAR A FREE − AISLE THROUGH THE FUSELAGE IN
BREAK − IN MARKED AREA.
A
A
@A330-700L
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A330-700L
F_AC_100000_1_1000101_01_01
Structural Break-in Points
FIGURE-10-0-0-991-100-A01
Page 19
Jul 01/21