Airbus A320. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016-2023) - page 1
@AIRBUS
A320
AIRCRAFT CHARACTERISTICS
AIRPORT AND MAINTENANCE PLANNING
AC
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AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
31707 Blagnac Cedex
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Issue: Sep 30/85
Rev: May 01/16
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 31 - May 01/16
LOCATIONS
CHG
DESCRIPTIONS OF CHANGE
CODE
CHAPTER 2
Section 2-1
R
Section 2-4
R
Subject 2-4-1
Interior Arrangements - Plan View
R
FIGURE Interior Arrangements - Plan
R
REPLACED ”TOURIST CLASS” BY
View - Typical Configuration - Single-
”ECONOMY CLASS” IN LEGEND AND
Class, High Density
IMPROVED LAYOUT.
FIGURE Interior Arrangements - Plan
R
REPLACED ”SUPER FIRST CLASS” BY
View - Typical Configuration - Two-Class
”FIRST CLASS” IN LEGEND AND
IMPROVED LAYOUT.
CHAPTER 3
Section 3-2
R
CHAPTER 5
Section 5-2
Subject 5-2-0
Terminal Operations - Full Servicing Turn
R
Round Time
Section 5-4
Subject 5-4-3
Hydraulic Servicing
R
DESCRIPTION TITLE UPDATED
FIGURE Ground Service Connections -
R
REPLACED TITLE ”HYDRAULIC SYSTEM”
Green System Ground Service Panel
BY ”GROUND SERVICE CONNECTIONS”.
ILLUSTRATION REVISED
FIGURE Ground Service Connections -
R
REPLACED TITLE ”HYDRAULIC SYSTEM”
Blue System Ground Service Panel
BY ”GROUND SERVICE CONNECTIONS”.
ILLUSTRATION REVISED
FIGURE Ground Service Connections -
R
REPLACED TITLE ”HYDRAULIC SYSTEM”
Yellow System Ground Service Panel
BY ”GROUND SERVICE CONNECTIONS”.
ILLUSTRATION REVISED
HIGHLIGHTS
Page 1
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
CHG
DESCRIPTIONS OF CHANGE
CODE
FIGURE Ground Service Connections -
N
ADDED ILLUSTRATION OF RAM AIR
RAT
TURBINE.
ILLUSTRATION ADDED
Section 5-7
Subject 5-7-0
FIGURE Preconditioned Airflow
R
ADDED THE CONDITIONS OF
Requirements
RECIRCULATION FANS AT MAXIMUM
AIRFLOW AND DELETED THE EXAMPLE.
Section 5-8
Subject 5-8-0
Ground Towing Requirements
R
PART EFFECTIVITY
ADDED/REVISED/DELETED
FIGURE Ground Towing Requirements
R
ADDED ”NEO” EFFECTIVITY.
ILLUSTRATION REVISED
PART EFFECTIVITY
ADDED/REVISED/DELETED
CHAPTER 7
Section 7-2
Subject 7-2-0
Landing Gear Footprint
R
FIGURE Landing Gear Footprint
R
UPDATED MAIN GEAR TIRE PRESSURE
FOR WV054 AND WV055.
Section 7-3
Subject 7-3-0
FIGURE Maximum Pavement Loads
R
UPDATED THE CONDITIONS OF V(NG)
AND V(MG).
FIGURE Maximum Pavement Loads
R
UPDATED THE CONDITIONS OF V(NG)
AND V(MG).
FIGURE Maximum Pavement Loads
R
REVISED MAXIMUM PAVEMENT LOAD
DATAS FOR WV052 AND WV053.
UPDATED THE CONDITIONS OF V(NG)
AND V(MG).
Section 7-5
Subject 7-5-0
HIGHLIGHTS
Page 2
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
CHG
DESCRIPTIONS OF CHANGE
CODE
FIGURE Flexible Pavement Requirements
R
REVISED TIRE PRESSURE TO 14.4 BAR
- WV054, MRW 79 400 kg, CG 36.1 %
(209 PSI).
Section 7-7
Subject 7-7-0
Rigid Pavement Requirements - Portland
R
Cement Association Design Method
FIGURE Rigid Pavement Requirements -
R
REVISED TIRE PRESSURE TO 14.4 BAR
WV054, MRW 79 400 kg, CG 36.1 %
(209 PSI).
Section 7-9
Subject 7-9-0
Aircraft Classification Number - Flexible
R
and Rigid Pavements
FIGURE Aircraft Classification Number -
R
REVISED ACN DATA FOR WV052, WV053,
ACN Table
WV054 AND WV055.
FIGURE Aircraft Classification Number -
R
REVISED TIRE PRESSURE TO 14.4 BAR
Flexible Pavement - WV054, MRW 79
(209 PSI).
400 kg, CG 36.1 %
CHAPTER 10
Section 10-0
Subject 10-0-0
FIGURE Front Page
R
UPDATED REVISION DATE.
FIGURE Wheel/Brake Overheat - Wheel
R
IMPROVED LAYOUT.
Safety Area
FIGURE Aircraft Ground Clearances
R
REVISED AIRCRAFT CONFIGURATIONS IN
THE TABLE AND IMPROVED LAYOUT.
HIGHLIGHTS
Page 3
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No.
31 - May
01/16
CONTENT
CHG
LAST REVISION
CODE
DATE
CHAPTER 1
Subject 1-1-0
Purpose
May
01/14
Subject 1-2-0
Glossary
May
01/14
CHAPTER 2
Subject 2-1-1
General Aircraft Characteristics Data
May
01/14
Subject 2-2-0
General Aircraft Dimensions
May
01/14
FIGURE General Aircraft Dimensions - Wing Tip Fence
May
01/15
FIGURE General Aircraft Dimensions
May
01/15
Subject 2-3-0
Ground Clearances
May
01/15
FIGURE Ground Clearances - Wing Tip Fence
Dec
01/15
FIGURE Ground Clearances - Sharklet
Dec
01/15
FIGURE Ground Clearances
May
01/15
FIGURE Ground Clearances - Trailing Edge Flaps - Extended
May
01/15
FIGURE Ground Clearances - Flap Tracks - Extended
May
01/15
FIGURE Ground Clearances - Trailing Edge Flaps - Extended
May
01/15
FIGURE Ground Clearances - Flap Tracks - Extended
May
01/15
FIGURE Ground Clearances - Flap Tracks - Retracted
May
01/15
FIGURE Ground Clearances - Flap Tracks - 1 + F
May
01/15
FIGURE Ground Clearances - Aileron Down
May
01/15
FIGURE Ground Clearances - Aileron Up
May
01/15
FIGURE Ground Clearances - Spoilers - Extended
May
01/15
L.E.C.
Page 1
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE Ground Clearances - Leading Edge Slats - Extended
May
01/15
Subject 2-4-1
Interior Arrangements - Plan View
R
May
01/16
FIGURE Interior Arrangements - Plan View - Typical Configuration -
R
May
01/16
Single-Class, High Density
FIGURE Interior Arrangements - Plan View - Typical Configuration -
R
May
01/16
Two-Class
Subject 2-5-0
Interior Arrangements - Cross Section
May
01/15
FIGURE Interior Arrangements - Cross Section - Economy Class,
6
May
01/15
Abreast - Wider Aisle
FIGURE Interior Arrangements - Cross Section - First-Class
May
01/15
Subject 2-6-0
Cargo Compartments
May
01/15
FIGURE Cargo Compartments - Locations and Dimensions
May
01/15
FIGURE Cargo Compartments - Loading Combinations
May
01/15
Subject 2-7-0
Door Clearances
May
01/15
FIGURE Door Identification and Location - Door Identification
May
01/14
FIGURE Doors Clearances - Forward Passenger/Crew Doors
May
01/15
FIGURE Doors Clearances - Emergency Exits
May
01/15
FIGURE Doors Clearances - Aft Passenger/Crew Doors
May
01/15
FIGURE Door Clearances - Forward Cargo Compartment Door
May
01/15
FIGURE Door Clearances - Forward Cargo Compartment Door
May
01/15
FIGURE Doors Clearances - Aft Cargo Compartment Door
May
01/15
FIGURE Doors Clearances - Bulk Cargo Compartment Door
May
01/15
FIGURE Doors Clearances - Main Landing Gear Doors
May
01/15
FIGURE Doors Clearances - Main Landing Gear Doors (Bogie)
May
01/15
FIGURE Doors Clearances - Radome
May
01/15
FIGURE Doors Clearances - APU and Nose Landing Gear Doors
May
01/15
L.E.C.
Page 2
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Subject 2-8-0
Escape Slides
Dec
01/15
FIGURE Escape Slides - Location
Dec
01/15
FIGURE Escape Slides - Dimensions
Dec
01/15
Subject 2-9-0
Landing Gear
May
01/14
FIGURE Landing Gear - Main Landing Gear - Twin-Wheel
May
01/14
FIGURE Landing Gear - Main Landing Gear Dimensions - Twin-Wheel
May
01/14
FIGURE Landing Gear - Main Landing Gear - Four-Wheel Bogie
May
01/14
FIGURE Landing Gear - Main Landing Gear Dimensions - Four-Wheel
May
01/14
Bogie
FIGURE Landing Gear - Nose Landing Gear
May
01/14
FIGURE Landing Gear - Nose Landing Gear Dimensions
May
01/14
Landing Gear Maintenance Pits
May
01/14
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes
May
01/14
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes
May
01/14
Subject 2-10-0
Exterior Lighting
May
01/15
FIGURE Exterior Lighting
May
01/14
FIGURE Exterior Lighting
May
01/14
FIGURE Exterior Lighting
May
01/14
FIGURE Exterior Lighting
May
01/14
Subject 2-11-0
Antennas and Probes Location
May
01/14
FIGURE Antennas and Probes - Location
May
01/14
Subject 2-12-0
Auxiliary Power Unit
Dec
01/15
FIGURE Auxiliary Power Unit - Access Doors
Dec
01/15
FIGURE Auxiliary Power Unit - General Layout
Dec
01/15
L.E.C.
Page 3
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Engine and Nacelle
May
01/15
FIGURE Power Plant Handling - Major Dimensions - CFM56 Series
May
01/14
Engine
FIGURE Power Plant Handling - Major Dimensions - CFM56 Series
May
01/14
Engine
FIGURE Power Plant Handling - Fan Cowls - CFM56 Series Engine
May
01/14
FIGURE Power Plant Handling - Thrust Reverser Cowls - CFM56
May
01/14
Series Engine
FIGURE Power Plant Handling - Major Dimensions - IAE V2500
May
01/14
Series Engine
FIGURE Power Plant Handling - Major Dimensions - IAE V2500
May
01/14
Series Engine
FIGURE Power Plant Handling - Fan Cowls - IAE V2500 Series
May
01/14
Engine
FIGURE Power Plant Handling - Thrust Reverser Halves - IAE V2500
May
01/14
Series Engine
FIGURE Power Plant Handling - Major Dimensions - PW 1100G
May
01/14
Engine
FIGURE Power Plant Handling - Fan Cowls - PW 1100G Engine
May
01/14
FIGURE Power Plant Handling - Thrust Reverser Halves - PW 1100G
May
01/14
Engine
FIGURE Power Plant Handling - Major Dimensions - CFM LEAP-1A
May
01/15
Engine
FIGURE Power Plant Handling - Major Dimensions - CFM LEAP-1A
May
01/15
Engine
Subject 2-13-0
Leveling, Symmetry and Alignment
May
01/14
FIGURE Location of the Leveling Points
May
01/14
Subject 2-14-0
Jacking for Maintenance
May
01/14
FIGURE Jacking for Maintenance - Jacking Point Locations
May
01/15
FIGURE Jacking for Maintenance - Forward Jacking Point
May
01/14
L.E.C.
Page 4
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE Jacking for Maintenance - Wing Jacking Points
May
01/15
FIGURE Jacking for Maintenance - Safety Stay
May
01/15
FIGURE Jacking for Maintenance - Jacking Design
May
01/15
FIGURE Loads at the Aircraft Jacking Points - Forward Fuselage
May
01/14
Jacking Point - Twin Wheel/Bogie
FIGURE Loads at the Aircraft Jacking Points - Wing Jacking Point
May
01/14
Rib 8 - Twin Wheel/Bogie
FIGURE Jacking for Maintenance - Location of Shoring Cradles
May
01/14
Jacking of the Landing Gear
May
01/14
FIGURE Jacking of the Landing Gear - MLG Jacking Point Location -
May
01/14
Twin Wheels
FIGURE Jacking of the Landing Gear - MLG Jacking with Cantilever
May
01/14
Jack - Twin Wheels
FIGURE Jacking of the Landing Gear - Loads at MLG Jacking Points
May
01/14
- Twin Wheels
FIGURE Jacking of the Landing Gear - MLG Jacking Point Location
May
01/14
Bogie
FIGURE Jacking of the Landing Gear - MLG Jacking Point Location
May
01/14
Bogie
FIGURE Jacking of the Landing Gear - MLG Jacking Point Location
May
01/14
Bogie
FIGURE Jacking of the Landing Gear - Loads at MLG Jacking Points
May
01/14
- Bogie Version
FIGURE Jacking of the Landing Gear - Loads at MLG Jacking Points
May
01/14
- 77 000 kg
FIGURE Jacking of the Landing Gear - NLG Jacking - Point Location
May
01/14
FIGURE Jacking of the Landing Gear - Loads at NLG Jacking Points
May
01/14
FIGURE Jacking of the Landing Gear - Loads at NLG Jacking Points
May
01/14
- 77 000 kg
CHAPTER 3
Subject 3-1-0
General Information
May
01/14
L.E.C.
Page 5
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Subject 3-2-1
Payload/Range - ISA Conditions
May
01/15
FIGURE Payload/Range - ISA Conditions
May
01/15
FIGURE Payload/Range - ISA Conditions - Sharklet
May
01/15
FIGURE Payload/Range - ISA Conditions
May
01/15
Subject 3-3-1
Take-Off Weight Limitation - ISA Conditions
May
01/14
FIGURE Take-Off Weight Limitation - ISA Conditions - CFM56
May
01/14
Series Engine
FIGURE Take-Off Weight Limitation - ISA Conditions - IAE V2500
May
01/14
Series Engine
Subject 3-3-2
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
May
01/14
FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)
May
01/14
Conditions - CFM56 Series Engine
FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)
May
01/14
Conditions - IAE V2500 Series Engine
Subject 3-4-1
Landing Field Length - ISA Conditions
May
01/14
FIGURE Landing Field Length - ISA Conditions - CFM56 Series
May
01/14
Engine
FIGURE Landing Field Length - ISA Conditions - IAE V2500 Series
May
01/14
Engine
Subject 3-5-0
Final Approach Speed
May
01/14
CHAPTER 4
Subject 4-1-0
General Information
May
01/14
Subject 4-2-0
Turning Radii
Dec
01/15
FIGURE Turning Radii, No Slip Angle - Dual Landing Gear (Sheet 1)
Dec
01/15
L.E.C.
Page 6
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE Turning Radii, No Slip Angle - Dual Landing Gear (Sheet 2)
Dec
01/15
FIGURE Turning Radii, No Slip Angle - Bogie Landing Gear (Sheet 1)
Dec
01/15
FIGURE Turning Radii, No Slip Angle - Bogie Landing Gear (Sheet 2)
Dec
01/15
Subject 4-3-0
Minimum Turning Radii
Dec
01/15
FIGURE Minimum Turning Radii
May
01/14
Subject 4-4-0
Visibility from Cockpit in Static Position
May
01/14
FIGURE Visibility from Cockpit in Static Position
May
01/14
FIGURE Binocular Visibility Through Windows from Captain Eye
May
01/14
Position
Subject 4-5-0
Runway and Taxiway Turn Paths
May
01/14
Subject 4-5-1
135˚ Turn - Runway to Taxiway
May
01/14
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over Centerline
May
01/14
Method
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental Oversteering
May
01/14
Method
Subject 4-5-2
90˚ Turn - Runway to Taxiway
May
01/14
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over Centerline
May
01/14
Method
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental Oversteering
May
01/14
Method
Subject 4-5-3
180˚ Turn on a Runway
Dec
01/15
FIGURE 180˚ Turn on a Runway - Edge of Runway Method
Dec
01/15
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway
May
01/14
L.E.C.
Page 7
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline
May
01/14
Method
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway
May
01/14
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline
May
01/14
Method
Subject 4-6-0
Runway Holding Bay (Apron)
May
01/14
FIGURE Runway Holding Bay (Apron)
May
01/14
Subject 4-7-0
Minimum Line-Up Distance Corrections
May
01/14
FIGURE Minimum Line-Up Distance Corrections -
90˚ Turn on
May
01/14
Runway Entry
FIGURE Minimum Line-Up Distance Corrections -
180˚ Turn on
May
01/14
Runway Turn Pad
FIGURE Minimum Line-Up Distance Corrections -
180˚ Turn on
May
01/14
Runway Width
Subject 4-8-0
Aircraft Mooring
May
01/14
FIGURE Aircraft Mooring
May
01/14
CHAPTER 5
Subject 5-1-1
Aircraft Servicing Arrangements
May
01/14
Subject 5-1-2
Typical Ramp Layout - Open Apron
May
01/14
FIGURE Typical Ramp Layout - Open Apron - Bulk Loading
May
01/14
FIGURE Typical Ramp Layout - Open Apron - ULD Loading
May
01/14
Subject 5-1-3
Typical Ramp Layout - Gate
May
01/14
FIGURE Typical Ramp Layout - Gate
May
01/14
Subject 5-2-0
L.E.C.
Page 8
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Terminal Operations - Full Servicing Turn Round Time
R
May
01/16
FIGURE Full Servicing Turn Round Time Chart
May
01/14
Subject 5-3-0
Terminal Operations - Outstation Turn Round Time
May
01/14
FIGURE Outstation Turn Round Time Chart
May
01/14
Subject 5-4-1
Ground Service Connections Layout
May
01/14
FIGURE Ground Service Connections Layout
May
01/14
Subject 5-4-2
Grounding (Earthing) Points
May
01/14
FIGURE Ground Service Connections - Grounding (Earthing) Points -
May
01/14
Landing Gear
FIGURE Ground Service Connections - Grounding (Earthing) Points -
May
01/14
Wing (If Installed)
FIGURE Ground Service Connections - Grounding (Earthing) Point -
May
01/14
Avionics Compartment Door-Frame
FIGURE Ground Service Connections - Grounding (Earthing) Point -
May
01/14
High-Pressure Connector (If Installed)
FIGURE Ground Service Connections - Grounding (Earthing) Point -
May
01/14
Engine Air Intake (If Installed)
Subject 5-4-3
Hydraulic Servicing
R
May
01/16
FIGURE Ground Service Connections - Green System Ground Service
R
May
01/16
Panel
FIGURE Ground Service Connections - Blue System Ground Service
R
May
01/16
Panel
FIGURE Ground Service Connections - Yellow System Ground Service
R
May
01/16
Panel
FIGURE Ground Service Connections - RAT
N
May
01/16
Subject 5-4-4
Electrical System
May
01/15
FIGURE Ground Service Connections - External Power Receptacles
May
01/14
L.E.C.
Page 9
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Subject 5-4-5
Oxygen System
May
01/14
FIGURE Ground Service Connections - Oxygen System
May
01/14
Subject 5-4-6
Fuel System
May
01/14
FIGURE Ground Service Connections - Refuel/Defuel Control Panel
May
01/14
FIGURE Ground Service Connections - Refuel/Defuel Couplings
May
01/14
FIGURE Ground Service Connections - Overwing Gravity-Refuel Cap
May
01/14
(If Installed)
FIGURE Ground Service Connections - Overpressure Protectors and
May
01/14
NACA Vent Intake
Subject 5-4-7
Pneumatic System
May
01/14
FIGURE Ground Service Connections - LP and HP Ground
May
01/14
Connectors
Subject 5-4-8
Oil System
May
01/14
FIGURE Ground Service Connections - Engine Oil Tank -- CFM56
May
01/14
Series Engine
FIGURE Ground Service Connections - IDG Oil Tank -- CFM56 Series
May
01/14
Engine
FIGURE Ground Service Connections - Starter Oil Tank -- CFM56
May
01/14
Series Engine
FIGURE Ground Service Connections - Engine Oil Tank -- IAE V2500
May
01/14
Series Engine
FIGURE Ground Service Connections - IDG Oil Tank -- IAE V2500
May
01/14
Series Engine
FIGURE Ground Service Connections - Starter Oil Tank -- IAE V2500
May
01/14
Series Engine
FIGURE Ground Service Connections - APU Oil Tank
May
01/14
Subject 5-4-9
Potable Water System
May
01/14
L.E.C.
Page 10
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE Ground Service Connections - Potable Water Ground Service
May
01/14
Panels
FIGURE Ground Service Connections - Potable Water Tank Location
May
01/14
Subject 5-4-10
Vacuum Toilet System
May
01/14
FIGURE Ground Service Connections - Waste Water Ground Service
May
01/14
Panel
FIGURE Ground Service Connections - Waste Tank Location
May
01/14
Subject 5-5-0
Engine Starting Pneumatic Requirements
May
01/14
FIGURE Example for Use of the Charts
May
01/14
FIGURE Engine Starting Pneumatic Requirements - IAE V2500 Series
May
01/14
Engine
FIGURE Engine Starting Pneumatic Requirements - CFM56 Series
May
01/14
and CFM LEAP-1A NEO Engine
FIGURE Engine Starting Pneumatic Requirements - PW 1100G NEO
May
01/14
Engine
Subject 5-6-0
Ground Pneumatic Power Requirements
May
01/15
FIGURE Ground Pneumatic Power Requirements - Heating
May
01/14
FIGURE Ground Pneumatic Power Requirements - Cooling
May
01/14
Subject 5-7-0
Preconditioned Airflow Requirements
May
01/15
FIGURE Preconditioned Airflow Requirements
R
May
01/16
Subject 5-8-0
Ground Towing Requirements
R
May
01/16
FIGURE Ground Towing Requirements
R
May
01/16
Subject 5-9-0
De-Icing and External Cleaning
May
01/14
CHAPTER 6
L.E.C.
Page 11
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Subject 6-1-0
Engine Exhaust Velocities and Temperatures
Dec
01/15
Subject 6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power
Dec
01/15
FIGURE Engine Exhaust Velocities - Ground Idle Power -- CFM56
Dec
01/15
Series Engine
FIGURE Engine Exhaust Velocities - Ground Idle Power -- IAE V2500
Dec
01/15
Series Engine
FIGURE Engine Exhaust Velocities - Ground Idle Power -- CFM
Dec
01/15
LEAP-1A Engine
FIGURE Engine Exhaust Velocities - Ground Idle Power -- PW 1100G
Dec
01/15
Engine
Subject 6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power
Dec
01/15
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- CFM56
Dec
01/15
Series Engine
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- IAE
Dec
01/15
V2500 Series Engine
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- CFM
Dec
01/15
LEAP-1A Engine
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- PW
Dec
01/15
1100G Engine
Subject 6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
Dec
01/15
FIGURE Engine Exhaust Velocities - Breakaway Power -- CFM56
Dec
01/15
Series Engine
FIGURE Engine Exhaust Velocities - Breakaway Power -- IAE V2500
Dec
01/15
Series Engine
FIGURE Engine Exhaust Velocities - Breakaway Power 12% MTO --
Dec
01/15
CFM LEAP-1A Engine
FIGURE Engine Exhaust Velocities - Breakaway Power 12% MTO --
Dec
01/15
PW 1100G Engine
L.E.C.
Page 12
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE Engine Exhaust Velocities - Breakaway Power 24% MTO --
Dec
01/15
CFM LEAP-1A Engine
FIGURE Engine Exhaust Velocities - Breakaway Power 24% MTO --
Dec
01/15
PW 1100G Engine
Subject 6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power
Dec
01/15
FIGURE Engine Exhaust Temperatures - Breakaway Power -- CFM56
Dec
01/15
Series Engine
FIGURE Engine Exhaust Temperatures - Breakaway Power -- IAE
Dec
01/15
V2500 Series Engine
FIGURE Engine Exhaust Temperatures - Breakaway Power 12%
Dec
01/15
MTO - CFM LEAP-1A Engine
FIGURE Engine Exhaust Temperatures - Breakaway Power 12%
Dec
01/15
MTO - PW 1100G Engine
FIGURE Engine Exhaust Temperatures - Breakaway Power 24%
Dec
01/15
MTO - CFM LEAP-1A Engine
FIGURE Engine Exhaust Temperatures - Breakaway Power 24%
Dec
01/15
MTO - PW 1100G Engine
Subject 6-1-5
Engine Exhaust Velocities Contours - Takeoff Power
Dec
01/15
FIGURE Engine Exhaust Velocities - Takeoff Power -- CFM56 Series
Dec
01/15
Engine
FIGURE Engine Exhaust Velocities - Takeoff Power -- IAE V2500
Dec
01/15
Series Engine
FIGURE Engine Exhaust Velocities - Takeoff Power -- CFM LEAP-1A
Dec
01/15
Engine
FIGURE Engine Exhaust Velocities - Takeoff Power -- PW 1100G
Dec
01/15
Engine
Subject 6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power
Dec
01/15
FIGURE Engine Exhaust Temperatures - Takeoff Power -- CFM56
Dec
01/15
Series Engine
L.E.C.
Page 13
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE Engine Exhaust Temperatures - Takeoff Power -- IAE V2500
Dec
01/15
Series Engine
FIGURE Engine Exhaust Temperatures - Takeoff Power - CFM
Dec
01/15
LEAP-1A Engine
FIGURE Engine Exhaust Temperatures - Takeoff Power - PW 1100G
Dec
01/15
Engine
Subject 6-3-0
Danger Areas of Engines
May
01/14
Subject 6-3-1
Ground Idle Power
Dec
01/15
FIGURE Danger Areas of the Engines - CFM56 Series Engine
May
01/15
FIGURE Danger Areas of the Engines - IAE V2500 Series Engine
May
01/15
FIGURE Danger Areas of the Engines - CFM LEAP-1A Engine
Dec
01/15
FIGURE Danger Areas of the Engines - PW 1100G Engine
Dec
01/15
Subject 6-3-2
Takeoff Power
Dec
01/15
FIGURE Danger Areas of the Engines - CFM56 Series Engine
Dec
01/15
FIGURE Danger Areas of the Engines - IAE V2500 Series Engine
Dec
01/15
FIGURE Danger Areas of the Engines - CFM LEAP-1A Engine
Dec
01/15
FIGURE Danger Areas of the Engines - PW 1100G Engine
Dec
01/15
Subject 6-4-1
APU - APIC & GARRETT
May
01/14
FIGURE Exhaust Velocities and Temperatures - APU -- APIC &
May
01/14
GARRETT
CHAPTER 7
Subject 7-1-0
General Information
May
01/15
Subject 7-2-0
Landing Gear Footprint
R
May
01/16
FIGURE Landing Gear Footprint
May
01/14
L.E.C.
Page 14
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
FIGURE Landing Gear Footprint
May
01/14
FIGURE Landing Gear Footprint
R
May
01/16
Subject 7-3-0
Maximum Pavement Loads
May
01/15
FIGURE Maximum Pavement Loads
R
May
01/16
FIGURE Maximum Pavement Loads
R
May
01/16
FIGURE Maximum Pavement Loads
R
May
01/16
Subject 7-4-0
Landing Gear Loading on Pavement
May
01/15
FIGURE Landing Gear Loading on Pavement - WV006, MRW
66
400
May
01/14
kg, CG 43%
FIGURE Landing Gear Loading on Pavement - WV015, MRW
78
400
May
01/14
kg, CG 36.8%
FIGURE Landing Gear Loading on Pavement - WV056, MRW
70
400
May
01/14
kg, CG 41%
FIGURE Landing Gear Loading on Pavement - WV054, MRW
79
400
May
01/14
kg, CG 36.1%
FIGURE Landing Gear Loading on Pavement - WV000 (Bogie), MRW
May
01/14
73 900 kg, CG 40%
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of Engineers
May
01/15
Design Method
FIGURE Flexible Pavement Requirements - WV006, MRW 66 400 kg,
May
01/14
CG 43 %
FIGURE Flexible Pavement Requirements - WV015, MRW 78 400 kg,
May
01/14
CG 36.8 %
FIGURE Flexible Pavement Requirements - WV056, MRW 70 400 kg,
May
01/14
CG 41 %
FIGURE Flexible Pavement Requirements - WV054, MRW 79 400 kg,
R
May
01/16
CG 36.1 %
FIGURE Flexible Pavement Requirements - WV000 (Bogie), MRW 73
May
01/14
900 kg, CG 40 %
Subject 7-6-0
L.E.C.
Page 15
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Flexible Pavement Requirements - LCN Conversion
May
01/15
Subject 7-7-0
Rigid Pavement Requirements - Portland Cement Association Design
R
May
01/16
Method
FIGURE Rigid Pavement Requirements - WV006, MRW 66 400 kg,
May
01/14
CG 43 %
FIGURE Rigid Pavement Requirements - WV015, MRW 78 400 kg,
May
01/14
CG 36.8 %
FIGURE Rigid Pavement Requirements - WV056, MRW 70 400 kg,
May
01/14
CG 41 %
FIGURE Rigid Pavement Requirements - WV054, MRW 79 400 kg,
R
May
01/16
CG 36.1 %
FIGURE Rigid Pavement Requirements - WV000 (Bogie), MRW 73
May
01/14
900 kg, CG 40 %
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion
May
01/15
Subject 7-9-0
Aircraft Classification Number - Flexible and Rigid Pavements
R
May
01/16
FIGURE Aircraft Classification Number - ACN Table
May
01/14
FIGURE Aircraft Classification Number - Flexible Pavement - WV006,
May
01/14
MRW 66 400 kg, CG 43 %
FIGURE Aircraft Classification Number - Flexible Pavement - WV015,
May
01/14
MRW 78 400 kg, CG 36.8 %
FIGURE Aircraft Classification Number - Flexible Pavement - WV000
May
01/14
(Bogie), MRW 73 900 kg, CG 40 %
FIGURE Aircraft Classification Number - ACN Table
R
May
01/16
FIGURE Aircraft Classification Number - Flexible Pavement - WV056,
May
01/14
MRW 70 400 kg, CG 41 %
FIGURE Aircraft Classification Number - Flexible Pavement - WV054,
R
May
01/16
MRW 79 400 kg, CG 36.1 %
CHAPTER 8
Subject 8-0-0
L.E.C.
Page 16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Scaled Drawings
Dec
01/15
FIGURE Scaled Drawing
Dec
01/15
FIGURE Scaled Drawing
Dec
01/15
CHAPTER 10
Subject 10-0-0
Aircraft Rescue and Fire Fighting
May
01/15
FIGURE Front Page
R
May
01/16
FIGURE Highly Flammable and Hazardous Materials and Components
May
01/15
FIGURE Batteries Location and Access
May
01/15
FIGURE Wheel/Brake Overheat - Wheel Safety Area
R
May
01/16
FIGURE Composite Materials
May
01/14
FIGURE L/G Ground Lock Safety Devices
May
01/14
FIGURE Emergency Evacuation Devices
Dec
01/15
FIGURE Pax/Crew Doors
May
01/14
FIGURE Emergency Exit Hatch
May
01/14
FIGURE FWD and AFT Lower Deck Cargo Doors
May
01/14
FIGURE Control Panels
May
01/14
FIGURE APU Access Door
May
01/14
FIGURE Aircraft Ground Clearances
R
May
01/16
FIGURE Structural Break-in Points
May
01/14
L.E.C.
Page 17
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TABLE OF CONTENTS
1
SCOPE
1-1-0
Introduction
1-2-0
Glossary
2
AIRCRAFT DESCRIPTION
2-1-1
General Aircraft Characteristics Data
2-2-0
General Aircraft Dimensions
2-3-0
Ground Clearances
2-4-1
Interior Arrangements - Plan View
2-5-0
Interior Arrangements - Cross Section
2-6-0
Cargo Compartments
2-7-0
Door Clearances and Location
2-8-0
Escape Slides
2-9-0
Landing Gear
2-10-0
Exterior Lighting
2-11-0
Antennas and Probes Location
2-12-0
Power Plant
2-13-0
Leveling, Symmetry and Alignment
2-14-0
Jacking
3
AIRCRAFT PERFORMANCE
3-1-0
General Information
3-2-1
Payload / Range - ISA Conditions
3-3-1
Take-off Weight Limitation - ISA Conditions
3-3-2
Take-off Weight Limitation - ISA +15˚C (+59˚F) Conditions
3-4-1
Landing Field Length - ISA Conditions
3-5-0
Final Approach Speed
4
GROUND MANEUVERING
4-1-0
General Information
4-2-0
Turning Radii
4-3-0
Minimum Turning Radii
4-4-0
Visibility from Cockpit in Static Position
4-5-0
Runway and Taxiway Turn Paths
4-5-1
135˚ Turn - Runway to Taxiway
T.O.C.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2
90˚ Turn - Runway to Taxiway
4-5-3
180˚ Turn on a Runway
4-5-4
135˚ Turn - Taxiway to Taxiway
4-5-5
90˚ Turn - Taxiway to Taxiway
4-6-0
Runway Holding Bay (Apron)
4-7-0
Minimum Line-Up Distance Corrections
4-8-0
Aircraft Mooring
5
TERMINAL SERVICING
5-1-1
Aircraft Servicing Arrangements
5-1-2
Typical Ramp Layout - Open Apron
5-1-3
Typical Ramp Layout - Gate
5-2-0
Terminal Operations - Full Servicing Turn Round Time Chart
5-3-0
Terminal Operation - Outstation Turn Round Time Chart
5-4-1
Ground Service Connections
5-4-2
Grounding Points
5-4-3
Hydraulic System
5-4-4
Electrical System
5-4-5
Oxygen System
5-4-6
Fuel System
5-4-7
Pneumatic System
5-4-8
Oil System
5-4-9
Potable Water System
5-4-10
Waste Water System
5-5-0
Engine Starting Pneumatic Requirements
5-6-0
Ground Pneumatic Power Requirements
5-7-0
Preconditioned Airflow Requirements
5-8-0
Ground Towing Requirements
5-9-0
De-Icing and External Cleaning
6
OPERATING CONDITIONS
6-1-0
Engine Exhaust Velocities and Temperatures
6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power
6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power
6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power
6-1-5
Engine Exhaust Velocities Contours - Takeoff Power
6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power
T.O.C.
Page 2
May 01/16
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0
Danger Areas of Engines
6-3-1
Ground Idle Power
6-3-2
Takeoff Power
6-4-1
APU
7
PAVEMENT DATA
7-1-0
General Information
7-2-0
Landing Gear Footprint
7-3-0
Maximum Pavement Loads
7-4-0
Landing Gear Loading on Pavement
7-5-0
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-6-0
Flexible Pavement Requirements - LCN Conversion
7-7-0
Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-0
Rigid Pavement Requirements - LCN Conversion
7-9-0
ACN/PCN Reporting System - Flexible and Rigid Pavements
8
SCALED DRAWINGS
8-0-0
SCALED DRAWINGS
10
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0
AIRCRAFT RESCUE AND FIRE FIGHTING
T.O.C.
Page 3
May 01/16
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0
Introduction
**ON A/C A320-200 A320neo
Purpose
1.
General
The A320 AIRCRAFT CHARACTERISTICS -- AIRPORT AND MAINTENANCE PLANNING (AC)
manual is issued for the A320-200 series aircraft equipped with wing-tip fences or sharklets, to
provide necessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO)
for airport and maintenance facilities planning.
Preliminary information on neo (New Engine Option) given in this document can be subject to
change, pending completion of the flight test phase.
This document is not customized and must not be used for training purposes. No information within
may constitute a contractual commitment.
The A320 Family is the world’s best-selling single-aisle aircraft. An A320 takes off or lands
somewhere in the world every 2.5 seconds of every day, the family has logged more than 50 million
cycles since entry-into-service and records a best-in-class dispatch reliability of 99.7%.
To ensure this true market leadership, Airbus continues to invest in improvements in the A320
Family: enhancements to aerodynamics such as the sharklet wingtip devices, upgrades to the widest
passenger cabin in its class, the A320 Family neo. The latter combines top-of-class engine efficiency
offered by two new engine options: the PW1100G PurePower from Pratt&Whitney and the LEAP-1A
from CFM International with superior aerodynamics offered by the new sharklet devices.
The neo will offer a minimum of 15% fuel savings and an additional flight range of about 500 nm
(926 km). For the environment, the neo fuel savings will translate into some 3 600 t (7 936 639 lb)
less CO2 per aircraft per year, together with a double-digit reduction in NOx emissions and reduced
engine noise.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
1, Rond Point Maurice BELLONTE
31707 BLAGNAC CEDEX
FRANCE
Page 1
May 01/16
1-1-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1-2-0
Glossary
**ON A/C A320-200 A320neo
Glossary
1.
List of Abbreviations
A/C
Aircraft
ACN
Aircraft Classification Number
AMM
Aircraft Maintenance Manual
APU
Auxiliary Power Unit
B/C
Business Class
CBR
California Bearing Ratio
CC
Cargo Compartment
CG
Center of Gravity
CKPT
Cockpit
E
Young’s Modulus
ELEC
Electric, Electrical, Electricity
ESWL
Equivalent Single Wheel Load
FAA
Federal Aviation Administration
F/C
First Class
FDL
Fuselage Datum Line
FR
Frame
FSTE
Full Size Trolley Equivalent
FWD
Forward
GPU
Ground Power Unit
GSE
Ground Support Equipment
HYD
Hydraulic
ICAO
International Civil Aviation Organisation
IDG
Integrated Drive Generator
ISA
International Standard Atmosphere
L
Left
L
Radius of relative stiffness
LCN
Load Classification Number
LD
Lower Deck
L/G
Landing Gear
LH
Left Hand
LPS
Last Pax Seating
MAC
Mean Aerodynamic Chord
MAX
Maximum
Page 1
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1-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
MIN
Minimum
MLG
Main Landing Gear
NLG
Nose Landing Gear
OAT
Outside Air Temperature
PAX
Passenger
PBB
Passenger Boarding Bridge
PCA
Portland Cement Association
PCN
Pavement Classification Number
PRM
Passenger with Reduced Mobility
R
Right
RH
Right Hand
ULD
Unit Load Device
US
United States
WV
Weight Variant
Y/C
Tourist Class
2.
Design Weight Terminology
-
Maximum Design Ramp Weight (MRW):
Maximum weight for ground maneuver (including weight of taxi and run-up fuel) as limited by
aircraft strength and airworthiness requirements. It is also called Maximum Design Taxi Weight
(MTW).
-
Maximum Design Landing Weight (MLW):
Maximum weight for landing as limited by aircraft strength and airworthiness requirements.
-
Maximum Design Takeoff Weight (MTOW):
Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (This
is the maximum weight at start of the take-off run).
-
Maximum Design Zero Fuel Weight (MZFW):
Maximum permissible weight of the aircraft without usable fuel.
-
Maximum Seating Capacity:
Maximum number of passengers specifically certified or anticipated for certification.
-
Usable Volume:
Usable volume available for cargo, pressurized fuselage, passenger compartment and cockpit.
-
Water Volume:
Maximum volume of cargo compartment.
-
Usable Fuel:
Fuel available for aircraft propulsion.
Page 2
May 01/16
1-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-1
General Aircraft Characteristics Data
**ON A/C A320-200 A320neo
General Aircraft Characteristics Data
**ON A/C A320-200
1.
The following table provides characteristics of A320-200 Models, these data are specific to each
Weight Variant:
Aircraft Characteristics
WV000
WV001
WV002
WV003
WV004
Maximum Ramp Weight
(MRW)
73 900 kg
68 400 kg
70 400 kg
75 900 kg
71 900 kg
Maximum Taxi Weight
(162 922 lb)
(150 796 lb)
(155 205 lb)
(167 331 lb)
(158 512 lb)
(MTW)
Maximum Take-Off Weight
73 500 kg
68 000 kg
70 000 kg
75 500 kg
71 500 kg
(MTOW)
(162 040 lb)
(149 914 lb)
(154 324 lb)
(166 449 lb)
(157 630 lb)
Maximum Landing Weight
64 500 kg
64 500 kg
64 500 kg
64 500 kg
64 500 kg
(MLW)
(142 198 lb)
(142 198 lb)
(142 198 lb)
(142 198 lb)
(142 198 lb)
Maximum Zero Fuel Weight
60 500 kg
60 500 kg
60 500 kg
60 500 kg
60 500 kg
(MZFW)
(133 380 lb)
(133 380 lb)
(133 380 lb)
(133 380 lb)
(133 380 lb)
Aircraft Characteristics
WV005
WV006
WV007
WV008
WV009
Maximum Ramp Weight
(MRW)
67 400 kg
66 400 kg
77 400 kg
73 900 kg
75 900 kg
Maximum Taxi Weight
(148 592 lb)
(146 387 lb)
(170 638 lb)
(162 922 lb)
(167 331 lb)
(MTW)
Maximum Take-Off Weight
67 000 kg
66 000 kg
77 000 kg
73 500 kg
75 500 kg
(MTOW)
(147 710 lb)
(145 505 lb)
(169 756 lb)
(162 040 lb)
(166 449 lb)
Maximum Landing Weight
64 500 kg
64 500 kg
64 500 kg
64 500 kg
64 500 kg
(MLW)
(142 198 lb)
(142 198 lb)
(142 198 lb)
(142 198 lb)
(142 198 lb)
Maximum Zero Fuel Weight
60 500 kg
60 500 kg
60 500 kg
61 000 kg
61 000 kg
(MZFW)
(133 380 lb)
(133 380 lb)
(133 380 lb)
(134 482 lb)
(134 482 lb)
Page 1
May 01/16
2-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics
WV010
WV011
WV012
WV013
WV014
Maximum Ramp Weight
(MRW)
77 400 kg
75 900 kg
77 400 kg
71 900 kg
73 900 kg
Maximum Taxi Weight
(170 638 lb)
(167 331 lb)
(170 638 lb)
(158 512 lb)
(162 922 lb)
(MTW)
Maximum Take-Off Weight
77 000 kg
75 500 kg
77 000 kg
71 500 kg
73 500 kg
(MTOW)
(169 756 lb)
(166 449 lb)
(169 756 lb)
(157 630 lb)
(162 040 lb)
Maximum Landing Weight
64 500 kg
66 000 kg
66 000 kg
64 500 kg
64 500 kg
(MLW)
(142 198 lb)
(145 505 lb)
(145 505 lb)
(142 198 lb)
(142 198 lb)
Maximum Zero Fuel Weight
61 000 kg
62 500 kg
62 500 kg
61 000 kg
61 500 kg
(MZFW)
(134 482 lb)
(137 789 lb)
(137 789 lb)
(134 482 lb)
(135 584 lb)
Aircraft Characteristics
WV015
WV016
WV017
WV018
Maximum Ramp Weight (MRW)
78 400 kg
73 900 kg
78 400 kg
71 900 kg
Maximum Taxi Weight (MTW)
(172 842 lb)
(162 922 lb)
(172 482 lb)
(158 512 lb)
Maximum Take-Off Weight
78 000 kg
73 500 kg
78 000 kg
71 500 kg
(MTOW)
(171 961 lb)
(162 040 lb)
(171 961 lb)
(157 630 lb)
Maximum Landing Weight (MLW)
64 500 kg
66 000 kg
66 000 kg
66 000 kg
(142 198 lb)
(145 505 lb)
(145 505 lb)
(145 505 lb)
Maximum Zero Fuel Weight
61 000 kg
62 500 kg
62 500 kg
62 500 kg
(MZFW)
(134 482 lb)
(137 789 lb)
(137 789 lb)
(137 789 lb)
**ON A/C A320neo
2.
The following table provides characteristics of A320neo Models, these data are specific to each
Weight Variant:
Aircraft Characteristics
WV050
WV051
WV052
WV053
Maximum Ramp Weight (MRW)
73 900 kg
73 900 kg
77 400 kg
77 400 kg
Maximum Taxi Weight (MTW)
(162 921 lb)
(162 921 lb)
(170 638 lb)
(170 638 lb)
Maximum Take-Off Weight
73 500 kg
73 500 kg
77 000 kg
77 000 kg
(MTOW)
(162 040 lb)
(162 040 lb)
(169 756 lb)
(169 756 lb)
Maximum Landing Weight (MLW)
66 300 kg
67 400 kg
66 300 kg
67 400 kg
(146 166 lb)
(148 591 lb)
(146 166 lb)
(148 591 lb)
Maximum Zero Fuel Weight
62 800 kg
64 300 kg
62 800 kg
64 300 kg
(MZFW)
(138 450 lb)
(141 757 lb)
(138 450 lb)
(141 757 lb)
Page 2
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2-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics
WV054
WV055
WV056
WV057
Maximum Ramp Weight (MRW)
79 400 kg
79 400 kg
70 400 kg
70 400 kg
Maximum Taxi Weight (MTW)
(175 047 lb)
(175 047 lb)
(155 205 lb)
(155 205 lb)
Maximum Take-Off Weight
79 000 kg
79 000 kg
70 000 kg
70 000 kg
(MTOW)
(174 165 lb)
(174 165 lb)
(154 324 lb)
(154 324 lb)
Maximum Landing Weight (MLW)
66 300 kg
67 400 kg
66 300 kg
67 400 kg
(146 166 lb)
(148 591 lb)
(146 166 lb)
(148 591 lb)
Maximum Zero Fuel Weight
62 800 kg
64 300 kg
62 800 kg
64 300 kg
(MZFW)
(138 450 lb)
(141 757 lb)
(138 450 lb)
(141 757 lb)
**ON A/C A320-200 A320neo
3.
The following table provides characteristics of A320-200 and A320neo Models, these data are
common to each Weight Variant:
Aircraft Characteristics
Standard Seating Capacity
180
(Single-Class)
Usable Fuel Capacity
23 859 l - 26 759 l * - 29 659 l **
(density = 0.785 kg/l)
(6
303 US gal -
7 069 US gal * - 7 835 US gal **)
18 729 kg - 21 005 kg * - 23 282 kg **
(41 290 lb - 46 308 lb * - 51 328 lb **)
Pressurized Fuselage Volume (A/C non
330 m3
equipped)
(11 654 ft3)
Passenger Compartment Volume
139 m3
(4 909 ft3)
Cockpit Volume
9 m3
(318 ft3)
Usable Volume, FWD CC
13.28 m3
(469 ft3)
Usable Volume, AFT CC
18.26 m3
(645 ft3)
Usable Volume, Bulk CC
5.88 m3
(208 ft3)
Water Volume, FWD CC
15.56 m3
(549 ft3)
Water Volume, AFT CC
20.77 m3
(733 ft3)
Page 3
May 01/16
2-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics
Water Volume, Bulk CC
7.76 m3
(274 ft3)
* OPTION: 1 ACT
** OPTION: 2 ACT
Page 4
May 01/16
2-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0
General Aircraft Dimensions
**ON A/C A320-200 A320neo
General Aircraft Dimensions
1.
This section provides general aircraft dimensions.
Page 1
May 01/16
2-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
5.87 m
(19.26 ft)
4.14 m
(13.58 ft)
12.64 m
(41.47 ft)
5.07 m
(16.63 ft)
34.10 m
(111.88 ft)
12.45 m
(40.85 ft)
0.50 m
(1.64 ft)
0.93 m
(3.05 ft)
7.59 m
(24.90 ft)
8.95 m
(29.36 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0040101_01_04
General Aircraft Dimensions
Wing Tip Fence (Sheet 1 of 4)
FIGURE-2-2-0-991-004-A01
Page 2
May 01/16
2-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
37.57 m
(123.27 ft)
6.07 m
(19.91 ft)
5.75 m
(18.86 ft)
1.24 m
(4.07 ft)
3.95 m
(12.96 ft)
3.31 m
(10.86 ft)
8.30 m
(27.23 ft)
11.91 m
(39.07 ft)
11.19 m
CFM56
4.87 m
(36.71 ft)
(15.98 ft)
11.12 m
V2500
(36.48 ft)
1.50 m
0.76 m
(4.92 ft)
(2.49 ft)
1.82 m
(5.97 ft)
22.40 m
(73.49 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0040104_01_02
General Aircraft Dimensions
Wing Tip Fence (Sheet 2 of 4)
FIGURE-2-2-0-991-004-A01
Page 3
May 01/16
2-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
5.87 m
(19.26 ft)
4.14 m
(13.58 ft)
12.64 m
(41.47 ft)
5.07 m
(16.63 ft)
35.80 m
(117.45 ft)
12.45 m
(40.85 ft)
2.43 m
(7.97 ft)
3.79 m
0.50 m
(12.43 ft)
(1.64 ft)
0.93 m
(3.05 ft)
7.59 m
(24.90 ft)
8.95 m
(29.36 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0040103_01_02
General Aircraft Dimensions
Sharklet (Sheet 3 of 4)
FIGURE-2-2-0-991-004-A01
Page 4
May 01/16
2-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
37.57 m
(123.27 ft)
6.07 m
(19.91 ft)
5.75 m
(18.86 ft)
1.24 m
(4.07 ft)
3.95 m
3.31 m
(12.96 ft)
(10.86 ft)
8.30 m
(27.23 ft)
11.91 m
(39.07 ft)
16.29 m
(53.44 ft)
11.19 m
CFM56
4.87 m
(36.71 ft)
(15.98 ft)
11.12 m
V2500
(36.48 ft)
1.64 m
(5.38 ft)
1.61 m
3.22 m
(5.28 ft)
(10.56 ft)
23.45 m
(76.94 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0040105_01_02
General Aircraft Dimensions
Sharklet (Sheet 4 of 4)
FIGURE-2-2-0-991-004-A01
Page 5
May 01/16
2-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
5.87 m
(19.26 ft)
4.14 m
(13.58 ft)
12.64 m
(41.47 ft)
5.07 m
(16.63 ft)
35.80 m
(117.45 ft)
12.45 m
(40.85 ft)
2.43 m
(7.97 ft)
3.79 m
0.50 m
(12.43 ft)
(1.64 ft)
0.93 m
(3.05 ft)
7.59 m
(24.90 ft)
8.95 m
(29.36 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0090101_01_01
General Aircraft Dimensions
(Sheet 1 of 2)
FIGURE-2-2-0-991-009-A01
Page 6
May 01/16
2-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
37.57 m
(123.27 ft)
6.07 m
(19.91 ft)
5.75 m
1.24 m
(18.86 ft)
(4.07 ft)
3.95 m
(12.96 ft)
3.31 m
(10.86 ft)
8.30 m
(27.23 ft)
11.91 m
(39.07 ft)
16.29 m
CFM LEAP−1A/
11.14 m
(53.44 ft)
4.87 m
PW 1100G
(36.55 ft)
(15.98 ft)
1.64 m
(5.38 ft)
1.61 m
3.22 m
(5.28 ft)
(10.56 ft)
23.45 m
(76.94 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0090102_01_01
General Aircraft Dimensions
(Sheet 2 of 2)
FIGURE-2-2-0-991-009-A01
Page 7
May 01/16
2-2-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0
Ground Clearances
**ON A/C A320-200 A320neo
Ground Clearances
1.
This section provides the height of various points of the aircraft, above the ground, for different
aircraft configurations.
Dimensions in the tables are approximate and will vary with tire type, weight and balance and other
special conditions.
The dimensions are given for:
-
A light weight, for an A/C in maintenance configuration with a mid CG,
-
An aircraft at Maximum Ramp Weight with a FWD CG and an AFT CG,
-
Aircraft on jacks, FDL at 4.60 m (15.09 ft).
NOTE : Passenger and cargo door ground clearances are measured from the center of the door sill
and from floor level.
Page 1
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
CP1
D1
D2
W2
W1
D3
AP
N1
VT
HT
C3
C2 F2
BF1
F1 C1
F4
F3
41 000 kg
MRW
(90 389 lb)
A/C JACKED
A/C CONFIGURATION
FDL = 4.60 m (15.09 ft)
FWD CG (17%)
AFT CG (36.8%)
CG (26.5%)
m
ft
m
ft
m
ft
m
ft
D1
3.38
11.09
3.45
11.32
3.48
11.42
4.13
13.55
D2
3.87
12.70
3.88
12.73
3.98
13.06
4.54
14.89
DOORS
D3
3.60
11.81
3.50
11.48
3.70
12.14
4.13
13.55
C1
1.98
6.50
2.04
6.69
2.09
6.86
2.71
8.89
C2
2.12
6.96
2.07
6.79
2.22
7.28
2.71
8.89
C3
2.19
7.19
2.11
6.92
2.29
7.51
2.75
9.02
F1
1.72
5.64
1.76
5.77
1.82
5.97
2.43
7.97
F2
1.84
6.04
1.79
5.87
1.95
6.40
2.43
7.97
F3
5.86
19.23
5.90
19.36
5.97
19.59
6.58
21.59
FUSELAGE
F4
5.99
19.65
5.93
19.46
6.09
19.98
6.58
21.59
BF1
1.62
5.31
1.60
5.25
1.72
5.64
2.26
7.41
CP1
4.17
13.68
4.27
14.01
4.28
14.04
4.96
16.27
W1
4.76
15.62
4.71
15.45
4.86
15.94
5.35
17.55
WINGS
W2
3.78
12.40
3.74
12.27
3.89
12.76
4.38
14.37
HT
5.46
17.91
5.32
17.45
5.56
18.24
5.93
19.46
TAILPLANE
AP
4.74
15.55
4.59
15.06
4.84
15.88
5.20
17.06
VT
11.98
39.30
11.83
38.81
12.08
39.63
12.45
40.85
ENGINE/
N1 (CFM)
0.57
1.87
0.58
1.90
0.67
2.20
1.24
4.07
NACELLE
N1 (IAE)
0.75
2.46
0.76
2.49
0.85
2.79
1.42
4.66
NOTE:
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER
OF THE DOOR SILL AND FROM FLOOR LEVEL.
N_AC_020300_1_0040101_01_07
Ground Clearances
Wing Tip Fence
FIGURE-2-3-0-991-004-A01
Page 2
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
CP1
D1
D2
W2 W1
D3
AP
N1
VT
HT
C3
C2 F2 BF1
F1 C1
F4
F3
41 000 kg
MRW
(90 389 lb)
A/C JACKED
A/C CONFIGURATION
FDL = 4.60 m (15.09 ft)
FWD CG (17%)
AFT CG (36.8%)
CG (26.5%)
m
ft
m
ft
m
ft
m
ft
D1
3.38
11.09
3.45
11.32
3.48
11.42
4.13
13.55
D2
3.87
12.70
3.88
12.73
3.98
13.06
4.54
14.89
DOORS
D3
3.60
11.81
3.50
11.48
3.70
12.14
4.13
13.55
C1
1.98
6.50
2.04
6.69
2.09
6.86
2.71
8.89
C2
2.12
6.96
2.07
6.79
2.22
7.28
2.71
8.89
C3
2.19
7.19
2.11
6.92
2.29
7.51
2.75
9.02
F1
1.72
5.64
1.76
5.77
1.82
5.97
2.43
7.97
F2
1.84
6.04
1.79
5.87
1.95
6.40
2.43
7.97
F3
5.86
19.23
5.90
19.36
5.97
19.59
6.58
21.59
FUSELAGE
F4
5.99
19.65
5.93
19.46
6.09
19.98
6.58
21.59
BF1
1.62
5.31
1.60
5.25
1.72
5.64
2.26
7.41
CP1
4.17
13.68
4.27
14.01
4.28
14.04
4.96
16.27
W1
6.70
21.98
6.65
21.82
6.80
22.31
7.25
23.79
WINGS
W2
4.05
13.29
4.01
13.16
4.16
13.65
4.65
15.26
HT
5.46
17.91
5.32
17.45
5.56
18.24
5.93
19.46
TAILPLANE
AP
4.74
15.55
4.59
15.06
4.84
15.88
5.20
17.06
VT
11.98
39.30
11.83
38.81
12.08
39.63
12.45
40.85
ENGINE/
N1 (CFM)
0.57
1.87
0.58
1.90
0.67
2.20
1.24
4.07
NACELLE
N1 (IAE)
0.75
2.46
0.76
2.49
0.85
2.79
1.42
4.66
NOTE:
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER
OF THE DOOR SILL AND FROM FLOOR LEVEL.
N_AC_020300_1_0290101_01_02
Ground Clearances
Sharklet
FIGURE-2-3-0-991-029-A01
Page 3
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
CP1
D1
D2
W2
W1
D3
AP
N1
VT
HT
C3
C2 F2 BF1
F1 C1
F4
F3
41 000 kg
MRW
(90 389 lb)
A/C JACKED
A/C CONFIGURATION
FDL = 4.60 m (15.09 ft)
FWD CG (17%)
AFT CG (36.8%)
CG (26.5%)
m
ft
m
ft
m
ft
m
ft
D1
3.38
11.09
3.45
11.32
3.48
11.42
4.13
13.55
D2
3.87
12.70
3.88
12.73
3.98
13.06
4.54
14.89
D3
3.60
11.81
3.50
11.48
3.70
12.14
4.13
13.55
DOORS
C1
1.98
6.50
2.04
6.69
2.09
6.86
2.71
8.89
C2
2.12
6.96
2.07
6.79
2.22
7.28
2.71
8.89
C3
2.19
7.19
2.11
6.92
2.29
7.51
2.75
9.02
F1
1.72
5.64
1.76
5.77
1.82
5.97
2.43
7.97
F2
1.84
6.04
1.79
5.87
1.95
6.40
2.43
7.97
F3
5.86
19.23
5.90
19.36
5.97
19.59
6.58
21.59
FUSELAGE
F4
5.99
19.65
5.93
19.46
6.09
19.98
6.58
21.59
BF1
1.62
5.31
1.60
5.25
1.72
5.64
2.26
7.41
CP1
4.17
13.68
4.27
14.01
4.28
14.04
4.96
16.27
W1
6.70
21.98
6.65
21.82
6.80
22.31
7.25
23.79
WINGS
W2
4.05
13.29
4.01
13.16
4.16
13.65
4.65
15.26
HT
5.46
17.91
5.32
17.45
5.56
18.24
5.93
19.46
TAILPLANE
AP
4.74
15.55
4.59
15.06
4.84
15.88
5.20
17.06
VT
11.98
39.30
11.83
38.81
12.08
39.63
12.45
40.85
N1 (CFM
ENGINE/
0.46
1.51
0.47
1.54
0.56
1.84
1.13
3.71
LEAP−1A)
NACELLE
N1 (PW 1100G)
0.46
1.51
0.47
1.54
0.56
1.84
1.13
3.71
NOTE:
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROM THE CENTER
OF THE DOOR SILL AND FROM FLOOR LEVEL.
N_AC_020300_1_0320101_01_01
Ground Clearances
FIGURE-2-3-0-991-032-A01
Page 4
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
D
C
B
A
FLAPS EXTENDED
CFM 56 ENGINE
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
FLAP 1 INBD
A
2.09
6.86
1.99
6.53
1.96
6.43
FLAP 1 OUTBD
B
2.82
9.25
2.71
8.89
2.69
8.83
FLAP 2 INBD
C
2.86
9.38
2.75
9.02
2.72
8.92
FLAP 2 OUTBD
D
3.68
12.07
3.56
11.68
3.52
11.55
N_AC_020300_1_0160101_01_01
Ground Clearances
Trailing Edge Flaps - Extended
FIGURE-2-3-0-991-016-A01
Page 5
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
C
B
A
FLAP TRACKS EXTENDED
CFM 56 ENGINE
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
FLAP TRACK 2
A
2.18
7.15
2.08
6.82
2.05
6.73
FLAP TRACK 3
B
2.66
8.73
2.55
8.37
2.52
8.27
FLAP TRACK 4
C
3.10
10.17
2.99
9.81
2.95
9.68
N_AC_020300_1_0410101_01_00
Ground Clearances
Flap Tracks - Extended
FIGURE-2-3-0-991-041-A01
Page 6
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
D
C
B
A
FLAPS EXTENDED
IAE V2500, PW 1100G AND CFM LEAP−1A ENGINES
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
FLAP 1 INBD
A
2.05
6.73
1.94
6.37
1.92
6.30
FLAP 1 OUTBD
B
2.77
9.09
2.66
8.73
2.64
8.66
FLAP 2 INBD
C
2.81
9.22
2.70
8.86
2.68
8.78
FLAP 2 OUTBD
D
3.64
11.94
3.53
11.58
3.49
11.45
N_AC_020300_1_0170101_01_02
Ground Clearances
Trailing Edge Flaps - Extended
FIGURE-2-3-0-991-017-A01
Page 7
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
C
B
A
FLAP TRACKS EXTENDED
IAE V2500, PW 1100G AND CFM LEAP−1A ENGINES
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
FLAP TRACK 2
A
2.09
6.86
1.98
6.49
1.95
6.40
FLAP TRACK 3
B
2.59
8.50
2.48
8.14
2.44
8.01
FLAP TRACK 4
C
3.03
9.94
2.92
9.58
2.88
9.45
N_AC_020300_1_0420101_01_00
Ground Clearances
Flap Tracks - Extended
FIGURE-2-3-0-991-042-A01
Page 8
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
A
B
C
FLAP TRACKS RETRACTED
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
FLAP TRACK 2
A
2.70
8.86
2.60
8.53
2.58
8.46
FLAP TRACK 3
B
3.10
10.17
3.00
9.84
2.97
9.74
FLAP TRACK 4
C
3.50
11.48
3.39
11.12
3.36
11.02
N_AC_020300_1_0180101_01_01
Ground Clearances
Flap Tracks - Retracted
FIGURE-2-3-0-991-018-A01
Page 9
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
A
B
C
FLAP TRACKS 1+F
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
FLAP TRACK 2
A
1.95
6.40
1.85
6.07
1.83
6.00
FLAP TRACK 3
B
2.31
7.58
2.21
7.25
2.18
7.15
FLAP TRACK 4
C
2.89
9.48
2.78
9.12
2.75
9.02
N_AC_020300_1_0430101_01_00
Ground Clearances
Flap Tracks - 1 + F
FIGURE-2-3-0-991-043-A01
Page 10
May 01/16
2-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
B
A
AILERON DOWN
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
AILERON INBD
A
3.83
12.57
3.72
12.21
3.68
12.07
AILERON OUTBD
B
4.17
13.68
4.06
13.32
4.01
13.16
N_AC_020300_1_0190101_01_01
Ground Clearances
Aileron Down
FIGURE-2-3-0-991-019-A01
Page 11
May 01/16
2-3-0
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