Airbus A319. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016) - page 1
@AIRBUS
A319
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
FRANCE
Issue: Jul
01/95
Rev: May 01/16
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 15 - 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
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).
Section 7-9
Subject 7-9-0
Aircraft Classification Number - Flexible
R
and Rigid Pavements
CHAPTER 10
Section 10-0
Subject 10-0-0
HIGHLIGHTS
Page 2
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS
CHG
DESCRIPTIONS OF CHANGE
CODE
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.
15 - 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 - 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
FIGURE Ground Clearances - Leading Edge Slats - Extended
May
01/15
Subject 2-4-1
L.E.C.
Page 1
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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 Doors Clearances - Forward Cargo Compartment Door
May
01/15
FIGURE Doors Clearances - Forward Cargo Compartment Door
May
01/15
FIGURE Doors Clearances - Aft Cargo Compartment Door
May
01/15
FIGURE Doors Clearances - Main Landing Gear Doors
May
01/15
FIGURE Doors Clearances - Radome
May
01/15
FIGURE Doors Clearances - APU and Nose Landing Gear Doors
May
01/15
Subject 2-8-0
Escape Slides
Dec
01/15
FIGURE Escape Slides - Location
Dec
01/15
FIGURE Escape Slides - Dimensions
Dec
01/15
L.E.C.
Page 2
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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 - 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
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
L.E.C.
Page 3
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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
FIGURE Jacking for Maintenance - Wing Jacking Points
May
01/14
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 - Wing Jacking Point
May
01/14
and Forward Fuselage Jacking Point
FIGURE Jacking for Maintenance - Location of Shoring Cradles
May
01/14
Jacking of the Landing Gear
May
01/14
L.E.C.
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May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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 - Loads at MLG Jacking Points
May
01/14
- 75 500 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
- 75 500 kg
CHAPTER 3
Subject 3-1-0
General Information
May
01/14
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
L.E.C.
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May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Subject 3-4-1
Landing Field Length - ISA Conditions
May
01/14
FIGURE Landing Field Length - ISA Conditions - CFM56-5A 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 - (Sheet 1)
Dec
01/15
FIGURE Turning Radii, No Slip Angle - (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
L.E.C.
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May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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
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
L.E.C.
Page 7
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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
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
Engine Air Intake (If Installed)
Subject 5-4-3
L.E.C.
Page 8
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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
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
L.E.C.
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May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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
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
L.E.C.
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May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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
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
L.E.C.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Subject 6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
Dec
01/15
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
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 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
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 Temperatures - Takeoff Power -- CFM56
Dec
01/15
Series Engine
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
L.E.C.
Page 13
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Landing Gear Footprint
R
May
01/16
FIGURE Landing Gear Footprint
May
01/15
FIGURE Landing Gear Footprint
May
01/15
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
Subject 7-4-0
Landing Gear Loading on Pavement
May
01/15
FIGURE Landing Gear Loading on Pavement - WV012, MRW
62
400
May
01/14
kg, CG 36%
FIGURE Landing Gear Loading on Pavement - WV010, MRW
76
900
May
01/14
kg, CG 36%
FIGURE Landing Gear Loading on Pavement - WV050, MRW
64
400
May
01/15
kg, CG 34%
FIGURE Landing Gear Loading on Pavement - WV054, MRW
75
900
May
01/14
kg, CG 36%
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of Engineers
May
01/15
Design Method
FIGURE Flexible Pavement Requirements - WV012, MRW 62 400 kg,
May
01/14
CG 36 %
FIGURE Flexible Pavement Requirements - WV010, MRW 76 900 kg,
May
01/14
CG 36 %
FIGURE Flexible Pavement Requirements - WV050, MRW 64 400 kg,
May
01/15
CG 34 %
FIGURE Flexible Pavement Requirements - WV054, MRW 75 900 kg,
May
01/14
CG 36 %
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion
May
01/15
Subject 7-7-0
L.E.C.
Page 14
May 01/16
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
Rigid Pavement Requirements - Portland Cement Association Design
May
01/15
Method
FIGURE Rigid Pavement Requirements - WV012, MRW 62 400 kg,
May
01/14
CG 36 %
FIGURE Rigid Pavement Requirements - WV010, MRW 76 900 kg,
May
01/14
CG 36 %
FIGURE Rigid Pavement Requirements - WV050, MRW 64 400 kg,
May
01/15
CG 34 %
FIGURE Rigid Pavement Requirements - WV054, MRW 75 900 kg,
May
01/14
CG 36 %
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
01/15
FIGURE Aircraft Classification Number - Flexible Pavement - WV012,
May
01/14
MRW 62 400 kg, CG 36 %
FIGURE Aircraft Classification Number - Flexible Pavement - WV010,
May
01/14
MRW 76 900 kg, CG 36 %
FIGURE Aircraft Classification Number - ACN Table
May
01/15
FIGURE Aircraft Classification Number - Flexible Pavement - WV050,
May
01/15
MRW 64 400 kg, CG 34 %
FIGURE Aircraft Classification Number - Flexible Pavement - WV054,
May
01/14
MRW 75 900 kg, CG 36 %
CHAPTER 8
Subject 8-0-0
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
L.E.C.
Page 15
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT
CHG
LAST REVISION
CODE
DATE
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 01/15
FIGURE Aircraft Ground Clearances
R
May 01/16
FIGURE Structural Break-in Points
May 01/14
L.E.C.
Page 16
May 01/16
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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.
Page 1
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@A319
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
@A319
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0
Introduction
**ON A/C A319-100 A319neo
Purpose
1.
General
The A319 AIRCRAFT CHARACTERISTICS -- AIRPORT AND MAINTENANCE PLANNING (AC)
manual is issued for the A319-100 series aircraft equipped with wing-tip fences or sharklets, to
provide necessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO)
for airport and maintenance facilities planning.
Preliminary information on neo (New Engine Option) given in this document can be subject to
change, pending completion of the flight test phase.
This document is not customized and must not be used for training purposes. No information within
may constitute a contractual commitment.
The A320 Family is the world’s best-selling single-aisle aircraft. An A320 takes off or lands
somewhere in the world every 2.5 seconds of every day, the family has logged more than 50 million
cycles since entry-into-service and records a best-in-class dispatch reliability of 99.7%.
To ensure this true market leadership, Airbus continues to invest in improvements in the A320
Family: enhancements to aerodynamics such as the sharklet wingtip devices, upgrades to the widest
passenger cabin in its class, the A320 Family neo. The latter combines top-of-class engine efficiency
offered by two new engine options: the PW1100G PurePower from Pratt&Whitney and the LEAP-1A
from CFM International with superior aerodynamics offered by the new sharklet devices.
The neo will offer a minimum of 15% fuel savings and an additional flight range of about 500 nm
(926 km). For the environment, the neo fuel savings will translate into some 3 600 t (7 936 639 lb)
less CO2 per aircraft per year, together with a double-digit reduction in NOx emissions and reduced
engine noise.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
1, Rond Point Maurice BELLONTE
31707 BLAGNAC CEDEX
FRANCE
Page 1
May 01/16
1-1-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1-2-0
Glossary
**ON A/C A319-100 A319neo
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
@A319
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-1
General Aircraft Characteristics Data
**ON A/C A319-100 A319neo
General Aircraft Characteristics Data
**ON A/C A319-100
1.
The following table provides characteristics of A319-100 Models, these data are specific to each
Weight Variant:
Aircraft Characteristics
WV000
WV001
WV002
WV003
WV004
Maximum Ramp Weight
64 400 kg
70 400 kg
75 900 kg
68 400 kg
68 400 kg
(MRW)
(141 978 lb)
(155 205 lb)
(167 331 lb)
(150 796 lb)
(150 796 lb)
Maximum Taxi Weight (MTW)
Maximum Take-Off Weight
64 000 kg
70 000 kg
75 500 kg
68 000 kg
68 000 kg
(MTOW)
(141 096 lb)
(154 324 lb)
(166 449 lb)
(149 914 lb)
(149 914 lb)
Maximum Landing Weight
61 000 kg
61 000 kg
62 500 kg
61 000 kg
62 500 kg
(MLW)
(134 482 lb)
(134 482 lb)
(137 789 lb)
(134 482 lb)
(137 789 lb)
Maximum Zero Fuel Weight
57 000 kg
57 000 kg
58 500 kg
57 000 kg
58 500 kg
(MZFW)
(125 663 lb)
(125 663 lb)
(128 970 lb)
(125 663 lb)
(128 970 lb)
Aircraft Characteristics
WV005
WV006
WV007
WV008
WV009
Maximum Ramp Weight
70 400 kg
73 900 kg
75 900 kg
64 400 kg
66 400 kg
(MRW)
(155 205 lb)
(162 922 lb)
(167 331 lb)
(141 978 lb)
(146 387 lb)
Maximum Taxi Weight (MTW)
Maximum Take-Off Weight
70 000 kg
73 500 kg
75 500 kg
64 000 kg
66 000 kg
(MTOW)
(154 324 lb)
(162 040 lb)
(166 449 lb)
(141 096 lb)
(145 505 lb)
Maximum Landing Weight
62 500 kg
62 500 kg
61 000 kg
62 500 kg
62 500 kg
(MLW)
(137 789 lb)
(137 789 lb)
(134 482 lb)
(137 789 lb)
(137 789 lb)
Maximum Zero Fuel Weight
58 500 kg
58 500 kg
57 000 kg
58 500 kg
58 500 kg
(MZFW)
(128 970 lb)
(128 970 lb)
(125 663 lb)
(128 970 lb)
(128 970 lb)
Aircraft Characteristics
WV010
WV011
WV012
WV013
Maximum Ramp Weight (MRW)
76 900 kg
66 400 kg
62 400 kg
75 900 kg
Maximum Taxi Weight (MTW)
(169 535 lb)
(146 387 lb)
(137 568 lb)
(167 331 lb)
Page 1
May 01/16
2-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics
WV010
WV011
WV012
WV013
Maximum Take-Off Weight
76 500 kg
66 000 kg
62 000 kg
75 500 kg
(MTOW)
(168 653 lb)
(145 505 lb)
(136 686 lb)
(166 449 lb)
Maximum Landing Weight (MLW)
62 500 kg
61 000 kg
61 000 kg
62 500 kg
(137 789 lb)
(134 482 lb)
(134 482 lb)
(137 789 lb)
Maximum Zero Fuel Weight
58 500 kg
57 000 kg
57 000 kg
52 000 kg
(MZFW)
(128 970 lb)
(125 663 lb)
(125 663 lb)
(114 640 lb)
**ON A/C A319neo
2.
The following table provides characteristics of A319neo Models, these data are specific to each
Weight Variant:
Aircraft Characteristics
WV050
WV051
WV052
Maximum Ramp Weight (MRW)
64 400 kg
64 400 kg
70 400 kg
Maximum Taxi Weight (MTW)
(141 978 lb)
(141 978 lb)
(155 205 lb)
Maximum Take-Off Weight (MTOW)
64 000 kg
64 000 kg
70 000 kg
(141 096 lb)
(141 096 lb)
(154 323 lb)
Maximum Landing Weight (MLW)
62 800 kg
63 900 kg
62 800 kg
(138 450 lb)
(140 875 lb)
(138 450 lb)
Maximum Zero Fuel Weight (MZFW)
58 800 kg
60 300 kg
58 800 kg
(129 632 lb)
(132 939 lb)
(129 632 lb)
Aircraft Characteristics
WV053
WV054
WV055
Maximum Ramp Weight (MRW)
70 400 kg
75 900 kg
75 900 kg
Maximum Taxi Weight (MTW)
(155 205 lb)
(167 331 lb)
(167 331 lb)
Maximum Take-Off Weight (MTOW)
70 000 kg
75 500 kg
75 500 kg
(154 323 lb)
(166 449 lb)
(166 449 lb)
Maximum Landing Weight (MLW)
63 900 kg
62 800 kg
63 900 kg
(140 875 lb)
(138 450 lb)
(140 875 lb)
Maximum Zero Fuel Weight (MZFW)
60 300 kg
58 800 kg
60 300 kg
(132 939 lb)
(129 632 lb)
(132 939 lb)
Page 2
May 01/16
2-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
3.
The following table provides characteristics of A319-100 and A319neo Models, these data are
common to each Weight Variant:
Aircraft Characteristics
Standard Seating Capacity
156
(Single-Class)
Usable Fuel Capacity
23 859 l
(density = 0.785 kg/l)
(6 303 US gal)
18 729 kg
(41 290 lb)
Pressurized Fuselage Volume
285 m3
(A/C non equipped)
(10 065 ft3)
Passenger Compartment
120 m3
Volume
(4 238 ft3)
Cockpit Volume
9m3
(318 ft3)
Usable Volume, FWD CC
8.52 m3
(301 ft3)
Usable Volume, AFT CC
11.92 m3
(421 ft3)
Usable Volume, Bulk CC
7.22 m3
(255 ft3)
Water Volume, FWD CC
10.63 m3
(375 ft3)
Water Volume, AFT CC
13.91 m3
(491 ft3)
Water Volume, Bulk CC
7.51 m3
(265 ft3)
Page 3
May 01/16
2-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0
General Aircraft Dimensions
**ON A/C A319-100 A319neo
General Aircraft Dimensions
1.
This section provides general aircraft dimensions.
Page 1
May 01/16
2-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
5.87 m
(19.26 ft)
4.14 m
(13.58 ft)
OPTIONAL
11.04 m
(36.22 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_0020101_01_04
General Aircraft Dimensions
Wing Tip Fence (Sheet 1 of 4)
FIGURE-2-2-0-991-002-A01
Page 2
May 01/16
2-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
33.84 m
(111.02 ft)
6.07 m
(19.91 ft)
5.75 m
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)
9.59 m
CFM56
(31.46 ft)
4.87 m
(15.98 ft)
9.52 m
V2500
(31.23 ft)
1.50 m
0.76 m
(4.92 ft)
(2.49 ft)
1.82 m
(5.97 ft)
20.86 m
(68.44 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0020103_01_02
General Aircraft Dimensions
Wing Tip Fence (Sheet 2 of 4)
FIGURE-2-2-0-991-002-A01
Page 3
May 01/16
2-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
5.87 m
(19.26 ft)
4.14 m
(13.58 ft)
OPTIONAL
11.04 m
(36.23 ft)
5.07 m
(16.63 ft)
35.80 m
(117.45 ft)
12.45 m
(40.85 ft)
2.43 m
(7.97 ft)
3.79 m
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_0020102_01_02
General Aircraft Dimensions
Sharklet (Sheet 3 of 4)
FIGURE-2-2-0-991-002-A01
Page 4
May 01/16
2-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
33.84 m
(111.02 ft)
6.07 m
(19.91 ft)
5.75 m
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
9.59 m
CFM56
(53.44 ft)
(31.46 ft)
4.87 m
(15.98 ft)
9.52 m
V2500
(31.23 ft)
1.64 m
1.61 m
(5.38 ft)
3.22 m
(5.28 ft)
(10.56 ft)
21.85 m
(71.69 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0020104_01_02
General Aircraft Dimensions
Sharklet (Sheet 4 of 4)
FIGURE-2-2-0-991-002-A01
Page 5
May 01/16
2-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
5.87 m
(19.26 ft)
4.14 m
(13.58 ft)
OPTIONAL
11.04 m
(36.23 ft)
5.07 m
(16.63 ft)
35.80 m
(117.45 ft)
12.45 m
(40.85 ft)
2.43 m
(7.97 ft)
3.79 m
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_0080101_01_01
General Aircraft Dimensions
(Sheet 1 of 2)
FIGURE-2-2-0-991-008-A01
Page 6
May 01/16
2-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
33.84 m
(111.02 ft)
6.07 m
(19.91 ft)
5.75 m
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/
9.54 m
(53.44 ft)
PW 1100G
(31.30 ft)
4.87 m
(15.98 ft)
1.64 m
1.61 m
(5.38 ft)
3.22 m
(5.28 ft)
(10.56 ft)
21.85 m
(71.69 ft)
NOTE:
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
N_AC_020200_1_0080102_01_01
General Aircraft Dimensions
(Sheet 2 of 2)
FIGURE-2-2-0-991-008-A01
Page 7
May 01/16
2-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0
Ground Clearances
**ON A/C A319-100 A319neo
Ground Clearances
1.
This section provides the height of various points of the aircraft, above the ground, for different
aircraft configurations.
Dimensions in the tables are approximate and will vary with tire type, weight and balance and other
special conditions.
The dimensions are given for:
-
A light weight, for an A/C in maintenance configuration with a mid CG,
-
An aircraft at Maximum Ramp Weight with a FWD CG and an AFT CG,
-
Aircraft on jacks, FDL at 4.60 m (15.09 ft).
NOTE : Passenger and cargo door ground clearances are measured from the center of the door sill
and from floor level.
Page 1
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
CP1
D1
D2
W2 W1
D3
AP
N1
VT
HT
C2 F2
BF1
C1 F1
F4
F3
40 000 kg
MRW
(88 185 lb)
A/C JACKED
A/C CONFIGURATION
FDL = 4.60 m (15.09 ft)
FWD CG (21%)
AFT CG (36%)
CG (28%)
m
ft
m
ft
m
ft
m
ft
D1
3.38
11.09
3.43
11.25
3.47
11.38
4.13
13.55
D2
3.88
12.73
3.88
12.73
3.97
13.02
4.54
14.89
DOORS
D3
3.61
11.84
3.54
11.61
3.71
12.17
4.13
13.55
C1
1.99
6.53
2.03
6.66
2.09
6.86
2.71
8.89
C2
2.12
6.96
2.09
6.86
2.22
7.28
2.71
8.89
F1
1.73
5.68
1.76
5.77
1.83
6.00
2.43
7.97
F2
1.84
6.04
1.81
5.94
1.94
6.36
2.43
7.97
F3
5.88
19.29
5.90
19.36
5.97
19.59
6.58
21.59
FUSELAGE
F4
5.99
19.65
5.95
19.52
6.09
19.98
6.58
21.59
BF1
1.63
5.35
1.62
5.31
1.73
5.68
2.26
7.41
CP1
4.16
13.65
4.24
13.91
4.26
13.98
4.96
16.27
W1
4.78
15.68
4.74
15.55
4.87
15.98
5.35
17.55
WINGS
W2
3.81
12.50
3.77
12.37
3.90
12.80
4.38
14.37
HT
5.48
17.98
5.37
17.62
5.58
18.31
5.93
19.46
TAILPLANE
AP
4.78
15.68
4.65
15.26
4.87
15.98
5.20
17.06
VT
12.01
39.40
11.89
39.01
12.11
39.73
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)
0.76
2.49
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_0020101_01_06
Ground Clearances
Wing Tip Fence
FIGURE-2-3-0-991-002-A01
Page 2
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
CP1
D1
D2
W2
W1
D3
AP
N1
VT
HT
C2F2
BF1
C1 F1
F4
F3
40 000 kg
MRW
(88 185 lb)
A/C JACKED
A/C CONFIGURATION
FDL = 4.60 m (15.09 ft)
FWD CG (21%)
AFT CG (36%)
CG (28%)
m
ft
m
ft
m
ft
m
ft
D1
3.38
11.09
3.43
11.25
3.47
11.38
4.13
13.55
D2
3.88
12.73
3.88
12.73
3.97
13.02
4.54
14.89
DOORS
D3
3.61
11.84
3.54
11.61
3.71
12.17
4.13
13.55
C1
1.99
6.53
2.03
6.66
2.09
6.86
2.71
8.89
C2
2.12
6.96
2.09
6.86
2.22
7.28
2.71
8.89
F1
1.73
5.68
1.76
5.77
1.83
6.00
2.43
7.97
F2
1.84
6.04
1.81
5.94
1.94
6.36
2.43
7.97
F3
5.88
19.29
5.90
19.36
5.97
19.59
6.58
21.59
FUSELAGE
F4
5.99
19.65
5.95
19.52
6.09
19.98
6.58
21.59
BF1
1.63
5.35
1.62
5.31
1.73
5.68
2.26
7.41
CP1
4.16
13.65
4.24
13.91
4.26
13.98
4.96
16.27
W1
6.72
22.05
6.68
21.92
6.81
22.34
7.29
23.92
WINGS
W2
4.08
13.39
4.04
13.25
4.17
13.68
4.65
15.26
HT
5.48
17.98
5.37
17.62
5.58
18.31
5.93
19.46
TAILPLANE
AP
4.78
15.68
4.65
15.26
4.87
15.98
5.20
17.06
VT
12.01
39.40
11.89
39.01
12.11
39.73
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)
0.76
2.49
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_0280101_01_02
Ground Clearances
Sharklet
FIGURE-2-3-0-991-028-A01
Page 3
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
CP1
D1
D2
W2
W1
D3
AP
N1
VT
HT
C2F2 BF1
C1 F1
F4
F3
40 000 kg
MRW
(88 185 lb)
A/C JACKED
A/C CONFIGURATION
FDL = 4.60 m (15.09 ft)
FWD CG (21%)
AFT CG (36%)
CG (28%)
m
ft
m
ft
m
ft
m
ft
D1
3.38
11.09
3.43
11.25
3.47
11.38
4.13
13.55
D2
3.88
12.73
3.88
12.73
3.97
13.02
4.54
14.89
DOORS
D3
3.61
11.84
3.54
11.61
3.71
12.17
4.13
13.55
C1
1.99
6.53
2.03
6.66
2.09
6.86
2.71
8.89
C2
2.12
6.96
2.09
6.86
2.22
7.28
2.71
8.89
F1
1.73
5.68
1.76
5.77
1.83
6.00
2.43
7.97
F2
1.84
6.04
1.81
5.94
1.94
6.36
2.43
7.97
F3
5.88
19.29
5.90
19.36
5.97
19.59
6.58
21.59
FUSELAGE
F4
5.99
19.65
5.95
19.52
6.09
19.98
6.58
21.59
BF1
1.63
5.35
1.62
5.31
1.73
5.68
2.26
7.41
CP1
4.16
13.65
4.24
13.91
4.26
13.98
4.96
16.27
W1
6.72
22.05
6.68
21.92
6.81
22.34
7.29
23.92
WINGS
W2
4.08
13.39
4.04
13.25
4.17
13.68
4.65
15.26
HT
5.48
17.98
5.37
17.62
5.58
18.31
5.93
19.46
TAILPLANE
AP
4.78
15.68
4.65
15.26
4.87
15.98
5.20
17.06
VT
12.01
39.40
11.89
39.01
12.11
39.73
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_0310101_01_01
Ground Clearances
FIGURE-2-3-0-991-031-A01
Page 4
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
D
C
B
A
FLAPS EXTENDED
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
2.07
6.79
1.94
6.36
1.93
6.33
FLAP 1 OUTBD
B
2.79
9.15
2.67
8.76
2.65
8.69
FLAP 2 INBD
C
2.83
9.28
2.70
8.86
2.69
8.83
FLAP 2 OUTBD
D
3.67
12.04
3.54
11.61
3.51
11.52
N_AC_020300_1_0110101_01_02
Ground Clearances
Trailing Edge Flaps - Extended
FIGURE-2-3-0-991-011-A01
Page 5
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
C
B
A
FLAP TRACKS EXTENDED
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
2.11
6.92
1.99
6.53
1.97
6.46
FLAP TRACK 3
B
2.61
8.56
2.48
8.14
2.46
8.07
FLAP TRACK 4
C
3.06
10.06
2.93
9.61
2.91
9.55
N_AC_020300_1_0380101_01_00
Ground Clearances
Flap Tracks - Extended
FIGURE-2-3-0-991-038-A01
Page 6
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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_0120101_01_02
Ground Clearances
Flap Tracks - Retracted
FIGURE-2-3-0-991-012-A01
Page 7
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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_0390101_01_00
Ground Clearances
Flap Tracks - 1 + F
FIGURE-2-3-0-991-039-A01
Page 8
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
3.86
12.66
3.73
12.24
3.71
12.17
AILERON OUTBD
B
4.20
13.78
4.06
13.32
4.04
13.25
N_AC_020300_1_0130101_01_02
Ground Clearances
Aileron Down
FIGURE-2-3-0-991-013-A01
Page 9
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
B
A
AILERON UP
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
4.38
14.37
4.25
13.94
4.23
13.88
AILERON OUTBD
B
4.58
15.03
4.44
14.57
4.42
14.50
N_AC_020300_1_0400101_01_00
Ground Clearances
Aileron Up
FIGURE-2-3-0-991-040-A01
Page 10
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
G
F
E
D
C B
A
SPOILERS EXTENDED
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
SPOILER 1 INBD
A
3.77
12.37
3.65
11.98
3.64
11.94
SPOILER 1 OUTBD
B
4.02
13.19
3.91
12.83
3.90
12.80
SPOILER 2 INBD
C
4.09
13.42
3.97
13.02
3.96
12.99
SPOILER 2/3
D
4.23
13.88
4.11
13.48
4.10
13.10
SPOILER 3/4
E
4.37
14.34
4.24
13.91
4.23
13.88
SPOILER 4/5
F
4.49
14.73
4.37
14.34
4.35
14.27
SPOILER 5 OUTBD
G
4.62
15.16
4.49
14.73
4.47
14.67
N_AC_020300_1_0140101_01_02
Ground Clearances
Spoilers - Extended
FIGURE-2-3-0-991-014-A01
Page 11
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
B C
D
E
F
G
LEADING EDGE SLATS EXTENDED
A/C IN MAINTENANCE
MAXIMUM RAMP
MAXIMUM RAMP
CONFIGURATION
WEIGHT FWD CG
WEIGHT AFT CG
DESCRIPTION
MID CG
m
ft
m
ft
m
ft
SLAT 1 INBD
A
2.57
8.43
2.47
8.10
2.49
8.17
SLAT 1 OUTBD
B
2.98
9.78
2.88
9.45
2.89
9.48
SLAT 2 INBD
C
3.07
10.07
2.97
9.74
2.97
9.74
SLAT 2/3
D
3.37
11.06
3.26
10.70
3.26
10.70
SLAT 3/4
E
3.63
11.91
3.51
11.52
3.51
11.52
SLAT 4/5
F
3.88
12.73
3.76
12.34
3.75
12.30
SLAT 5 OUTBD
G
4.12
13.52
3.99
13.09
3.97
13.02
N_AC_020300_1_0150101_01_02
Ground Clearances
Leading Edge Slats - Extended
FIGURE-2-3-0-991-015-A01
Page 12
May 01/16
2-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1
Interior Arrangements - Plan View
**ON A/C A319-100 A319neo
Interior Arrangements - Plan View
1.
This section provides the typical interior configuration.
Page 1
May 01/16
2-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
GALLEY
LAVATORY
ATTENDANT SEAT
AFT PASSENGER
AFT PASSENGER
/CREW DOOR
/CREW DOOR
ATTENDANT SEAT
PASSENGER SEATS (156 TOTAL)
ECONOMY CLASS 156 SEATS
(6 ABREAST − 28/30 in PITCH)
ATTENDANT SEATS 5
GALLEYS 2
LAVATORIES 2
ECONOMY
CLASS SEATS
EMERGENCY EXIT
EMERGENCY EXIT
EMERGENCY EXIT
EMERGENCY EXIT
ATTENDANT SEAT
FWD PASSENGER
FWD PASSENGER
/CREW DOOR
/CREW DOOR
GALLEY
LAVATORY
N_AC_020401_1_0020101_01_03
Interior Arrangements - Plan View
Typical Configuration - Single-Class, High Density
FIGURE-2-4-1-991-002-A01
Page 2
May 01/16
2-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
GALLEY
LAVATORY
AFT PASSENGER
AFT PASSENGER
/CREW DOOR
/CREW DOOR
LAVATORY
PASSENGER SEATS (124 TOTAL)
ATTENDANT SEAT
FIRST CLASS 8 SEATS
(4 ABREAST − 36 in PITCH)
ECONOMY CLASS 116 SEATS
(6 ABREAST − 32 in PITCH)
ATTENDANT SEATS 3
GALLEYS 2
ECONOMY
CLASS SEATS
LAVATORIES 3
EMERGENCY EXIT
EMERGENCY EXIT
ATTENDANT SEAT
FIRST
CLASS SEATS
FWD PASSENGER
FWD PASSENGER
/CREW DOOR
/CREW DOOR
GALLEY
LAVATORY
N_AC_020401_1_0080101_01_01
Interior Arrangements - Plan View
Typical Configuration - Two-Class
FIGURE-2-4-1-991-008-A01
Page 3
May 01/16
2-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0
Interior Arrangements - Cross Section
**ON A/C A319-100 A319neo
Interior Arrangements - Cross Section
1.
This section provides the typical configuration.
Page 1
May 01/16
2-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
6 ABREAST−WIDER AISLE
0.43 m
(17 in)
1.50 m
(59 in)
0.64 m
(25 in)
3.63 m
(143 in)
N_AC_020500_1_0050101_01_01
Interior Arrangements - Cross Section
Economy Class, 6 Abreast - Wider Aisle (Sheet 1 of 2)
FIGURE-2-5-0-991-005-A01
Page 2
May 01/16
2-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
6 ABREAST−WIDER SEAT
0.46 m
(18 in)
1.58 m
(62 in)
0.48 m
(19 in)
3.63 m
(143 in)
N_AC_020500_1_0050102_01_03
Interior Arrangements - Cross Section
Economy Class, 6 Abreast - Wider Seat (Sheet 2 of 2)
FIGURE-2-5-0-991-005-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
4 ABREAST−FIRST CLASS
0.57 m
(22.6 in)
1.45 m
(57 in)
0.69 m
(27 in)
3.58 m
(141 in)
N_AC_020500_1_0060101_01_01
Interior Arrangements - Cross Section
First-Class
FIGURE-2-5-0-991-006-A01
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-0
Cargo Compartments
**ON A/C A319-100 A319neo
Cargo Compartments
1.
This section provides the cargo compartments locations, dimensions and loading combinations.
Page 1
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_020600_1_0020101_01_00
Cargo Compartments
Locations and Dimensions
FIGURE-2-6-0-991-002-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_020600_1_0050101_01_00
Cargo Compartments
Loading Combinations
FIGURE-2-6-0-991-005-A01
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2-6-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0
Door Clearances and Location
**ON A/C A319-100 A319neo
Door Clearances
1.
This section provides door identification and location.
NOTE : Dimensions of the ground clearances are approximate and will vary with tire type, weight
and balance and other special conditions.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
OVERWING
FWD
EMERGENCY
OVERWING
AFT
PASSENGER/CREW
EXIT DOOR (LH)
EMERGENCY
PASSENGER/CREW
DOOR (LH)
(OPTIONAL)
EXIT DOOR (LH)
DOOR (LH)
OVERWING
AFT
OVERWING
EMERGENCY
FWD
PASSENGER/CREW
EMERGENCY
EXIT DOOR (RH)
PASSENGER/CREW
DOOR (RH)
EXIT DOOR (RH)
(OPTIONAL)
DOOR (RH)
AFT CARGO
FWD CARGO
COMPARTMENT
COMPARTMENT
DOOR
DOOR
N_AC_020700_1_0020101_01_00
Door Identification and Location
Door Identification (Sheet 1 of 2)
FIGURE-2-7-0-991-002-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
25.81 m
(84.68 ft)
13.68 m
(44.88 ft)
12.83 m
(42.09 ft)
5.04 m
(16.54 ft)
8.16 m
(26.77 ft)
20.56 m
(67.45 ft)
N_AC_020700_1_0020102_01_00
Door Identification and Location
Door Location (Sheet 2 of 2)
FIGURE-2-7-0-991-002-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
1.80 m
(5.91 ft)
0.48 m
0.81 m
(1.57 ft)
(2.66 ft)
C
L
0.61 m
(2.00 ft)
2.54 m
(8.33 ft)
CRITICAL CLEARANCE
LIMIT
5.02 m
(16.47 ft)
2.38 m
(7.81 ft)
1.85 m
(6.07 ft)
C
C
L
L
SEE
CHAPTER
0.03 m
2−3
(0.10 ft)
N_AC_020700_1_0130101_01_00
Doors Clearances
Forward Passenger/Crew Doors
FIGURE-2-7-0-991-013-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
OPTIONAL
C
L
FWD
0.85 m
(FROM NOSE) 12.83 m
(2.79 ft)
(42.09 ft)
0.50 m
(1.64 ft)
A
B
SEE
SECTION
2−3
0.20 m
(0.66 ft)
0.47 m
A
B
(1.54 ft)
1.23 m
(4.04 ft)
0.90 m
(2.95 ft)
0.12 m
(0.39 ft)
0.50 m
(1.64 ft)
(TOP OF FLOOR)
B B
A A
(FRAME 47)
NOTE:
ESCAPE SLIDE COMPARTMENT DOOR OPENS ON WING UPPER SURFACE.
N_AC_020700_1_0140101_01_00
Doors Clearances
Emergency Exits
FIGURE-2-7-0-991-014-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
1.79 m
(5.87 ft)
0.81 m
(2.66 ft)
FWD
A
CRITICAL
CLEARANCE
0.58 m
LIMIT
(1.90 ft)
A
2.44m
(8.01 ft)
(FROM NOSE)
25.91 m
(85.01 ft)
SEE
1.85 m
CHAPTER
(6.07 ft)
0.60 m
2−3
(1.97 ft)
0.03 m
(0.10 ft)
A A
N_AC_020700_1_0150101_01_00
Doors Clearances
Aft Passenger/Crew Doors
FIGURE-2-7-0-991-015-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
8.16 m
(26.77 ft)(FROM NOSE)
1.50 m
1.24 m
(4.92 ft)
(4.07 ft)
FWD
SEE
CHAPTER
2−3
3.95 m
A
(12.96 ft)
1.82 m
(5.97 ft)
A A
2.71 m
(8.89 ft)
CFM56 = 0.58 m (1.90 ft)
IAE V2500 = 0.51 m (1.67 ft)
N_AC_020700_1_0160101_01_00
Doors Clearances
Forward Cargo Compartment Door
FIGURE-2-7-0-991-016-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
A
8.16 m
(FROM NOSE)
(26.77 ft)
1.50 m
1.24 m
(4.92 ft)
(4.07 ft)
FWD
SEE
CHAPTER
2−3
3.95 m
A
(12.96 ft)
1.82 m
(5.97 ft)
A A
CFM ENGINE = 2.47 m (8.10 ft)
PW ENGINE = 2.43 m (7.97 ft)
CFM/PW ENGINE = 0.45 m (1.48 ft)
N_AC_020700_1_0170101_01_00
Doors Clearances
Forward Cargo Compartment Door
FIGURE-2-7-0-991-017-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
20.58 m
(FROM NOSE)
(67.52 ft)
1.43 m
(4.69 ft)
FWD
1.23 m
SEE
CHAPTER
(4.04 ft)
2−3
A
3.95 m
1.82 m
(12.96 ft)
(5.97 ft)
A A
FWD
1.60 m
(5.25 ft)
N_AC_020700_1_0180101_01_00
Doors Clearances
Aft Cargo Compartment Door
FIGURE-2-7-0-991-018-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
14.76 m
1.83 m
(48.43 ft)
(6.00 ft)
AIRCRAFT
1.94 m
(6.36 ft)
0.49 m
(1.61 ft)
0.21 m
(0.69 ft)
84°
1.76 m
(5.77 ft)
1.23 m
(4.04 ft)
GROUND LINE
0.14 m
(0.46 ft)
NOTE:
A
VALUE OF CG: 25% RC.
N_AC_020700_1_0190101_01_00
Doors Clearances
Main Landing Gear Doors
FIGURE-2-7-0-991-019-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
0.63 m
(2.07 ft)
FR1
1.54 m
(5.05 ft)
65°
N_AC_020700_1_0200101_01_00
Doors Clearances
Radome
FIGURE-2-7-0-991-020-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FR80
FR84
3.86 m
3.23 m
(12.66 ft)
(10.60 ft)
1.50 m
(4.92 ft)
1.40 m
NOTE:
(4.59 ft)
VALUE OF CG: 25% RC.
N_AC_020700_1_0210101_01_00
Doors Clearances
APU and Nose Landing Gear Doors
FIGURE-2-7-0-991-021-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0
Escape Slides
**ON A/C A319-100 A319neo
Escape Slides
1.
General
This section provides location of cabin escape facilities and related clearances.
2.
Location
Escape facilities are provided at the following locations:
-
One escape slide at each passenger/crew door (total four)
-
One escape slide for each emergency exit door (total two). Dual lane offwing escape slides are
installed above the wings in the left and right wing-to-fuselage fairings for off-the-wing
evacuation.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
AFT CABIN ESCAPE SLIDE
OFF WING ESCAPE SLIDE
COCKPIT ESCAPE
FWD CABIN ESCAPE SLIDE
ROPE
NOTE:
LH SHOWN, RH SYMMETRICAL.
N_AC_020800_1_0030101_01_03
Escape Slides
Location
FIGURE-2-8-0-991-003-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_020800_1_0040101_01_02
Escape Slides
Dimensions
FIGURE-2-8-0-991-004-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0
Landing Gear
**ON A/C A319-100 A319neo
Landing Gear
1.
General
The landing gear is of the conventional retractable tricycle type comprising:
-
Two main gears with twin-wheel,
-
A twin-wheel nose gear.
The main landing gears are located under the wing and retract sideways towards the fuselage
centerline.
The nose landing gear retracts forward into a fuselage compartment located between FR9 and FR20.
The landing gears and landing gear doors are operated and controlled electrically and hydraulically.
In abnormal operation, the landing gear can be extended by gravity.
For landing gear footprint and tire size, refer to 07-02-00.
2.
Main Landing Gear
A. Twin-Wheel
Each of the two main landing gear assemblies consists of a conventional two-wheel direct type
with an integral shock absorber supported in the fore and aft directions by a fixed drag strut
and laterally by a folding strut mechanically locked when in the DOWN position.
3.
Nose Landing Gear
The nose landing gear consists of a leg with a built-in shock absorber strut, carrying twin wheels with
adequate shimmy damping and a folding strut mechanically locked when in the DOWN position.
4.
Nose Wheel Steering
Steering is controlled by two hand wheels in the cockpit. For steering angle controlled by the hand
wheels, refer to AMM 32-51-00.
For steering angle limitation, refer to AMM 09-10-00.
A steering disconnection box is installed on the nose landing gear to allow steering deactivation for
towing purposes.
5.
Landing Gear Servicing Points
A. General
Filling of the landing-gear shock absorbers is done through MIL-PRF-6164 standard valves.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Charging of the landing-gear shock absorbers is accomplished with nitrogen through MIL-
PRF-6164 standard valves.
B. Charging Pressure
For charging of the landing-gear shock absorbers, refer to AMM 12-14-32.
6.
Braking
A. General
The four main wheels are equipped with carbon multidisc brakes.
The braking system is electrically controlled and hydraulically operated.
The braking system has four braking modes plus autobrake and anti-skid systems:
-
Normal braking with anti-skid capability,
-
Alternative braking with anti-skid capability,
-
Alternative braking without anti-skid capability,
-
Parking brake with full pressure application capability only.
B. In-Flight Wheel Braking
The main gear wheels are braked automatically before the wheels enter the wheel bay.
The nose gear wheels are stopped by the wheels contacting a rubbing strip (the brake band)
when the gear is in the retracted position.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
HINGED FAIRING
(MECHANICALLY OPERATED)
HINGED
FAIRING
FIXED
DOOR ACTUATING CYLINDER
FAIRING
B
A
C
ADJUSTABLE
RAMP
PROXIMITY SENSORS
STEPS
UPLOCK
ACTUATING
ROLLER
CYLINDER
FIXED
MAIN DOOR
RAMPS
(HYDRAULICALLY OPERATED)
LOCK STAY
UNLOCK
E
ACTUATOR
MAIN
FITTING
SIDE STAY
SHOCK
ABSORBER
TORQUE
LINK
D
A
N_AC_020900_1_0060101_01_00
NOTE: MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION.
Landing Gear
Main Landing Gear - Twin-Wheel (Sheet 1 of 2)
FIGURE-2-9-0-991-006-A01
Page 3
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
DOOR
LOCKSTAY
LOCKING
GROUND LOCK SLEEVE
ACTUATING
ACTUATING
PIN
CYLINDER
CYLINDER
LOCKING
PIN
FLAG
FLAG
B
C
BOTTOM FILLING AND
CHARGING CONNECTION
TOP FILLING AND CHARGING
CONNECTION
E
D
EXAMPLE
N_AC_020900_1_0060102_01_01
Landing Gear
Main Landing Gear - Twin-Wheel (Sheet 2 of 2)
FIGURE-2-9-0-991-006-A01
Page 4
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
2 265 mm
(89.17 in)
2 868.70 mm
(112.94 in)
3 795 mm
Y=
COMPRESSED
(149.41 in)
EXTENDED
469.90 mm
(18.50 in)
3 453 mm
80°30
(135.94 in)
20 252.50 mm
RETRACTION
X=
(797.34 in)
ANGLE
927.10 mm
(36.50 in)
N_AC_020900_1_0070101_01_00
Landing Gear
Main Landing Gear Dimensions - Twin-Wheel
FIGURE-2-9-0-991-007-A01
Page 5
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
DOOR UPLOCK
BELL
FR9
ASSEMBLY
GEAR UPLOCK
CRANK
DRAG STRUT
ASSEMBLY
DOOR
ASSEMBLY
FR20
ACTUATING
CYLINDER
CONTROL ROD
B
C
ROTATING ROD
FITTING
ASSEMBLY
FWD DOORS
AFT DOORS
LEG DOOR
A
ACTUATING
CYLINDER
D
DOWNLOCK
PROXIMITY
DETECTORS
NOSE WHEEL
STEERING
SERVO CONTROL
STEERING
E
ACTUATING
CYLINDER
SHOCK
TORQUE
ABSORBER
LINK
TOWING
FITTING
A
N_AC_020900_1_0080101_01_00
Landing Gear
Nose Landing Gear (Sheet 1 of 2)
FIGURE-2-9-0-991-008-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
LOCKSTAY
NLG DOOR
SAFETY PIN
DOWNLOCK
SAFETY PIN
DOOR HINGE
NLG DOOR
FLAG
FLAG
B
C
RH SHOWN
LH SYMMETRICAL
TOWING LEVER
FILLING AND CHARGING
CONNECTION
NORMAL POSITION
(NOSE WHEEL STEERING
OPERATIONAL)
TOWING POSITION
(NOSE WHEEL STEERING DEACTIVATED)
SAFETY PIN
D
E
(TOWING POSITION)
N_AC_020900_1_0080102_01_01
Landing Gear
Nose Landing Gear (Sheet 2 of 2)
FIGURE-2-9-0-991-008-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
92°
1 957.03 mm
(77.05 in)
2 338 mm
(92.05 in)
430 mm
(16.93 in)
9°
7 561 mm
X =
(297.68 in)
500 mm
(19.69 in)
N_AC_020900_1_0090101_01_00
Landing Gear
Nose Landing Gear Dimensions
FIGURE-2-9-0-991-009-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
Landing Gear Maintenance Pits
1.
Description
The minimum maintenance pit envelopes for the landing-gear shock absorber removal are shown in
FIGURE 2-9-0-991-022-A and FIGURE 2-9-0-991-023-A.
All dimensions shown are minimum dimensions with zero clearances.
The dimensions for the pits have been determined as follows:
-
The length and width of the pits allow the gear to rotate as the weight is taken off the landing
gear.
-
The depth of the pits allows the shock absorber to be removed when all the weight is taken off
the landing gear.
Dimensions for elevators and associated mechanisms must be added to those in FIGURE
2-9-0-991-022-Aand FIGURE 2-9-0-991-023-A.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FROM X0
N_AC_020900_1_0220101_01_00
Landing Gear Maintenance Pits
Maintenance Pit Envelopes
FIGURE-2-9-0-991-022-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FROM X0
N_AC_020900_1_0230101_01_00
Landing Gear Maintenance Pits
Maintenance Pit Envelopes
FIGURE-2-9-0-991-023-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0
Exterior Lighting
**ON A/C A319-100 A319neo
Exterior Lighting
1.
General
This section provides the location of the aircraft exterior lighting.
EXTERIOR LIGHTING
ITEM
DESCRIPTION
1
RIGHT NAVIGATION LIGHT (GREEN)
2
TAIL NAVIGATION LIGHT (WHITE)
3
LEFT NAVIGATION LIGHT (RED)
4
RETRACTABLE LANDING LIGHT
5
RUNWAY TURN OFF LIGHT
6
TAXI LIGHT
7
TAKE-OFF LIGHT
8
LOGO LIGHT
9
UPPER ANTI-COLLISION LIGHT/BEACON (RED)
10
LOWER ANTI-COLLISION LIGHT/BEACON (RED)
11
WING STROBE LIGHT (HIGH INTENSITY, WHITE)
12
TAIL STROBE LIGHT (HIGH INTENSITY, WHITE)
13
WING/ENGINE SCAN LIGHT
14
WHEEL WELL LIGHT (DOME)
15
CARGO COMPARTMENT FLOOD LIGHT
Page 1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
2
8
12
9
8
11
1
RH
3
LH
10
13
11
RH
1
LH
3
6
5
7
4
N_AC_021000_1_0050101_01_00
Exterior Lighting
FIGURE-2-10-0-991-005-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
2
1
3
5
5
7
N_AC_021000_1_0060101_01_00
Exterior Lighting
FIGURE-2-10-0-991-006-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
12
9
10
11
11
13
13
4
6
N_AC_021000_1_0070101_01_00
Exterior Lighting
FIGURE-2-10-0-991-007-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
8
8
15
15
14
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
N_AC_021000_1_0180101_01_00
Exterior Lighting
FIGURE-2-10-0-991-018-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0
Antennas and Probes Location
**ON A/C A319-100 A319neo
Antennas and Probes Location
1.
This section gives the location of antennas and probes.
Page 1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
WEATHER RADAR
EMERGENCY STATIC PROBE
AOA SENSOR(3) STBY
VHF(1)
ATC(4)
GPS(2)
VHF(3)
AOA SENSOR(1)
HF
GPS(1)
ELT
TCAS TOP
LOC
GLIDE
RADIO ALTIMETER(2)
DME(1)
TAT PROBE
RADIO ALTIMETER(1)
TCAS BOTTOM
PITOT PROBE(3)
VHF(2)
MARKER
PITOT PROBE(1)
DME(2)
ATC(1)
STATIC PROBE(1)
STATIC PROBE(2)
VOR
EMERGENCY STATIC PROBE
ATC(3)
ADF(1)
AOA SENSOR(2)
TAT PROBE
PITOT PROBE(2)
ATC(2)
STATIC PROBE(1)
STATIC PROBE(2)
NOTE: DEPENDING ON AIRCRAFT CONFIGURATION
N_AC_021100_1_0020101_01_00
Antennas and Probes
Location
FIGURE-2-11-0-991-002-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0
Power Plant
**ON A/C A319-100 A319neo
Auxiliary Power Unit
1.
General
The APU is installed at the rear part of the fuselage in the tail cone. An air intake system with a
flap-type door is installed in front of the APU compartment. The exhaust gases pass overboard at the
end of the fuselage cone.
2.
Controls and Indication
The primary APU controls and indications are installed on the overhead panel, on the center pedestal
and on the center instrument panel. Additionally, an external APU panel is installed on the nose
landing gear to initiate an APU emergency shutdown.
Page 1
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FR77
FR87
A B
Z310
FR70
UPPER
FIREWALL
FRONT
FR80
FIREWALL
FIREWALL RH
LOUVER LH
CUT OUT SEALED WITH
LABYRINTH GASKET
RH ACCESS DOOR
316AR
REAR
FIREWALL
FR84
CUT OUT SEALED WITH
LABYRINTH GASKET
AIR INTAKE FIXED
ON ACCESS DOOR
A
NOTE:
LH ACCESS DOOR 315AL NOT SHOWN FOR CLARITY.
N_AC_021200_1_0030101_01_01
Auxiliary Power Unit
Access Doors
FIGURE-2-12-0-991-003-A01
Page 2
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FIRE OVERHEAT DETECTOR
APU
APU SUSPENSION
(7 RODS)
GENERATOR
FIRE EXTINGUISHING BOTTLE
BLEED AIR LINE
FR87
EXHAUST
MUFFLER
APU SUSPENSION
(7 RODS)
FR84
OIL COOLER OUTLET
AIR INTAKE DUCT
APU−FUEL−LINE
FR80
FRONT FIRE
WALL
AIR INTAKE HOUSING
FR78
FR77
DIVERTER
B
N_AC_021200_1_0040101_01_01
Auxiliary Power Unit
General Layout
FIGURE-2-12-0-991-004-A01
Page 3
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2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
Engine and Nacelle
**ON A/C A319-100
1.
Engine and Nacelle - CFM Engine
A.
Engine
The engine is a dual-rotor, variable stator, high bypass ratio turbo fan power plant for subsonic
services. The principal modules of the engine are:
-
low pressure compressor (fan stator and fan rotor)
-
high pressure compressor
-
turbine frame
-
combustion chamber
-
high pressure turbine
-
low pressure turbine
-
accessory drives (gear box).
The 9 stage high pressure compressor is driven by 1 stage high pressure turbine, and the
integrated front fan and booster is driven by 4 stage low pressure turbine. An annular combustor
converts fuel and compressor discharge air into energy to provide engine thrust part through
primary exhaust and to drive the turbines. The accessory drive system extracts energy from the
high pressure rotor to drive the engine accessories and the engine mounted aircraft accessories.
Reverse thrust for braking the aircraft after landing is supplied by an integrated system which
acts on the fan discharge airflow.
B.
Nacelle
The cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine is
housed in a nacelle suspended from a pylon attached to the wing lower surface. The nacelle
consists of the demountable powerplant, the fan cowls and the thrust reverser cowls.
The nacelle installation is designed to provide cooling and ventilation air for engine accessories
mounted along the fan and core casing. The nacelle provides:
-
protection for the engine and the accessories
-
airflow around the engine during its operation
-
lighting protection
-
HIRF and EMI attenuation.
2.
Engine and Nacelle - IAE Engine
A. Engine
The engine is a two spool, axial flow, high bypass ratio turbofan powerplant for subsonic sevice.
The main modules of the engine are:
Page 4
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
-
low pressure compressor (fan and booster) assembly
-
LP compressor/intermediate case
-
No. 4 bearing and combustion section
-
high pressure compressor
-
HP turbine section
-
LP turbine section
-
accessory drives (gear box).
The four stage Low Pressure Compressor (LPC) is driven by a five stage Low Pressure Turbine
(LPT) and the ten stage High Pressure Compressor (HPC) by a two stage High Pressure
Turbine (HPT). The HPT also drives a gearbox which, in turn drives the engines and aircraft
mounted accessories. The two shafts are supported by five main bearings.
The V2500 incorporates a Full Authority Digital Engine Control (FADEC) which governs all
engine functions, including power management. Reverse thrust for braking the aircraft after
landing is supplied by an integrated system which acts on the fan discharge airflow.
B.
Nacelle
The cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine is
housed in a nacelle suspended from a pylon attached below the wing.
The nacelle installation is designed to provide cooling and ventilation air for engine accessories
mounted along the fan and core casing. The nacelle provides:
-
protection for the engine and the accessories
-
airflow around the engine during its operation
-
lighting protection
-
HIRF and EMI attenuation.
Page 5
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2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2 943 mm
(115.87 in)
2 600 mm
(102.36 in)
1 125 mm
(44.28 in)
FAN AND
BOOSTER
COMPRESSOR
FWD HANDLING
A
POINT
COMBUSTOR
FWD HOISTING
POINT
TURBINE FRAME
DIA
986 mm
B
(38.82 in)
LP
TURBINE
HP
TURBINE
1 820 mm
AGB TGB
(71.65 in)
AFT HOISTING AND
ACCESSORY
HANDLING POINT
DRIVE
A
2 145 mm
(84.45 in)
1 130 mm
(44.49 in)
989 mm
(38.94 in)
1 978 mm
(77.87 in)
B
N_AC_021200_1_0190101_01_00
Power Plant Handling
Major Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-019-A01
Page 6
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2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
DISTANCE FROM
0.33 m
THE NOSE
(1.1 ft)
9.6 m
0.93 m
1.3 m
1.2 m
1.2 m
(31.5 m)
(3.1 ft)
(4.3 ft)
(3.9 ft)
(3.9 ft)
D
A
B
C
PRIMARY
NOZZLE
6°
2.3 m
1.6 m
(7.5 ft)
(5.2 ft)
CENTERBODY
2.1 m
C
A
B
(6.9 ft)
D
ENGINE AIR
FAN COWL
FAN
0.57 m
REVERSER
INLET COWL
(1.9 ft)
BLOCKER DOOR
A A
EXTENDED
2.07 m
1.9 m
1.8 m
(6.8 ft)
(6.2 ft)
(5.9 ft)
1.2 m
(3.9 ft)
B B
D D
C C
N_AC_021200_1_0200101_01_00
Power Plant Handling
Major Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-020-A01
Page 7
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2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
B
C
0.55 m
(1.8 ft)
m (ft)
A
B
C
VIEW
42°27
1.8
(5.9)
1.5
(4.9)
1.3
(4.3)
COWLING
AFT
55°15
2.0
(6.6)
1.8
(5.9)
1.7
(5.6)
VIEW
40°40
1.8
(5.9)
1.4
(4.6)
1.3
(4.3)
COWLING
FWD
52°56
2.0
(6.6)
1.7
(5.6)
1.6
(5.2)
NOTE: APPROXIMATE DIMENSIONS
N_AC_021200_1_0210101_01_00
Power Plant Handling
Fan Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-021-A01
Page 8
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2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
3.7 m
(12.1 ft)
3.3 m
(10.8 ft)
1 m
(3.3 ft)
0.9 m
(3 ft)
1 m
35°
0.7 m
(3.3 ft)
45°
0.5 m
(2.3 ft)
(1.6 ft)
GROUND
NOTE: APPROXIMATE DIMENSIONS
CAUTION
DO NOT ACTUATE SLATS:
− WITH THRUST REVERSER COWLS 45° OPEN POSITION
− WITH BLOCKER DOORS OPEN AND THRUST REVERSER
COWLS AT 35° AND 45° OPEN POSITION
N_AC_021200_1_0220101_01_00
Power Plant Handling
Thrust Reverser Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-022-A01
Page 9
May 01/16
2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
3 101 mm
(122.1 in)
FAN AND BOOSTER
COMPRESSOR COMBUSTOR HP
LP
TURBINE
TURBINE
TURBINE
FRAME
1 715 mm
(67.5 in)
1 067 mm
(42.0 in)
ACCESSORY
DRIVE
A
FWD
N_AC_021200_1_0230101_01_00
Power Plant Handling
Major Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-023-A01
Page 10
May 01/16
2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
DISTANCE FROM
THE NOSE
9.52 m
5.25 m
(31.23 ft)
(17.23 ft)
D
C
F
A
W
B
E
6°
0.5°
U
V
1.50 m
(4.95 ft)
B
E
A
F
C
D
5.26 m
(17.27 ft)
W
U
V
PPS
AT
COMPONENT
m
ft
m
ft
m
ft
m
ft
INLET
A−A
2.01
6.58
0.99
3.25
1.10
3.63
1.41
4.62
ATTACH FLG
TORQUE BOX
B−B
2.01
6.58
1.00
3.29
1.11
3.64
2.59
8.50
"V" BLADE
COMB. CHAMBER
C−C
1.98
6.50
0.97
3.19
1.07
3.52
3.26
10.70
ENTRY FLG
COMB. CHAMBER
D−D
1.93
6.32
0.93
3.06
1.03
3.39
3.63
11.90
EXIT FLG
TEC FLG
E−E
1.64
5.38
0.78
2.57
0.86
2.83
4.60
15.10
TURB. EXIT CASE
AFT END
F−F
1.24
4.07
0.60
1.96
0.64
2.11
−−−−
−−−−
CNA
NOTE: ALL SIZES GIVEN ON THIS ILLUSTRATION ARE APPROXIMATE
N_AC_021200_1_0240101_01_00
Power Plant Handling
Major Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-024-A01
Page 11
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2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FWD VIEW
2 m
(6.6 ft)
WL100
CLOSED
3.9 m
(12.8 ft)
WL100
FAN COWL
OPEN 50°
1.6 m
(5.2 ft)
1.2 m
(3.9 ft)
0.67 m
(2.2 ft)
GROUND
NOTE: APPROXIMATE DIMENSIONS
N_AC_021200_1_0250101_01_00
Power Plant Handling
Fan Cowls - IAE V2500 Series Engine
FIGURE-2-12-0-991-025-A01
Page 12
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2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AFT VIEW
2 m
(6.6 ft)
WL100
CLOSED
3.6 m
(11.8 ft)
WL100
0.9 m
THRUST REVERSER
(3 ft)
OPEN 45°
1.1 m
(3.6 ft)
1 m
(3.3 ft)
0.67 m
(2.2 ft)
NOTE: APPROXIMATE DIMENSIONS
N_AC_021200_1_0260101_01_00
Power Plant Handling
Thrust Reverser Halves - IAE V2500 Series Engine
FIGURE-2-12-0-991-026-A01
Page 13
May 01/16
2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
FAN COWL THRUST
NOSE COWL
REVERSER
PRIMARY
NOZZLE
A
PLUG
0.46 m
(1.51 ft)
0.66 m
(2.17 ft)
1.46 m
1.53 m
1.44 m
(4.79 ft)
(5.02 ft)
(4.72 ft)
FWD
2.60 m
(8.53 ft)
2.67 m
(8.76 ft)
0.46 m
(1.51 ft)
A
N_AC_021200_1_0430101_01_00
Power Plant Handling
Major Dimensions - PW 1100G Engine
FIGURE-2-12-0-991-043-A01
Page 14
May 01/16
2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
A
A
4.70 m
(15.42 ft)
1
1
1.22 m
(4.00 ft)
OPEN POSITION:
FULL: 50°
50°
1: FAN COWL
0.46 m
(1.51 ft)
A
N_AC_021200_1_0440101_01_00
Power Plant Handling
Fan Cowls - PW 1100G Engine
FIGURE-2-12-0-991-044-A01
Page 15
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
A
A
A
A
1
1
1
1
B
B
43°
45°
C
C
1: THRUST REVERSER
A
OPEN
B
A
C
POSITION
MIN.
MAX.
4.26 m
0.80 m
0.90 m
43°
(13.98 ft)
(2.62 ft)
(2.95 ft)
SEE AC SECTION
2−3−0
4.33 m
0.84 m
0.95 m
45°
(14.21 ft)
(2.76 ft)
(3.12 ft)
NOTE:
B AND C DEPENDING ON AIRCRAFT CONFIGURATION.
N_AC_021200_1_0450101_01_00
Power Plant Handling
Thrust Reverser Halves - PW 1100G Engine
FIGURE-2-12-0-991-045-A01
Page 16
May 01/16
2-12-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
3548 mm
(139.68 in)
3327 mm
(130.98 in)
1352 mm
(53.23 in)
FAN AND
BOOSTER
COMPRESSOR
A
FWD
COMBUSTOR
HANDLING
TURBINE
POINT
FRAME
DIA 1084 mm
B
(42.68 in)
HP
LP
AGB TGB
TURBINE
TURBINE
ACCESSORY
DRIVE
2152 mm
(84.72 in)
FWD
A
2242 mm
(88.27 in)
1165 mm
(45.87 in)
1236 mm
(48.66 in)
2487 mm
(97.91 in)
B
N_AC_021200_1_0520101_01_00
Power Plant Handling
Major Dimensions - CFM LEAP-1A Engine
FIGURE-2-12-0-991-052-A01
Page 17
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
THRUST
NOSE COWL
FAN COWL
REVERSER
PRIMARY
NOZZLE
PLUG
A
0.98 m
(3.22 ft)
0.49 m
(1.61 ft)
0.67 m
(2.20 ft)
1.58 m
1.98 m
(5.18 ft)
(6.50 ft)
0.23 m
(0.75 ft)
FWD
2.52 m
(8.27 ft)
2.60 m
(8.53 ft)
A
0.46 m
(1.51 ft)
N_AC_021200_1_0530101_01_00
Power Plant Handling
Major Dimensions - CFM LEAP-1A Engine
FIGURE-2-12-0-991-053-A01
Page 18
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0
Leveling, Symmetry and Alignment
**ON A/C A319-100 A319neo
Leveling, Symmetry and Alignment
1.
Quick Leveling
There are three alternative procedures to level the aircraft:
-
Quick leveling procedure with Air Data/Inertial Reference Unit (ADIRU).
-
Quick leveling procedure with a spirit level in the passenger compartment.
-
Quick leveling procedure with a spirit level in the FWD cargo compartment.
2.
Precise Leveling
For precise leveling, it is necessary to install sighting rods in the receptacles located under the
fuselage (points 11 and 12 for longitudinal leveling) and under the wings (points 2LH and 2RH for
lateral leveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until the
reference marks on the sighting rods are aligned in the sighting plane (aircraft level).
3.
Symmetry and Alignment Check
Possible deformation of the aircraft is measured by photogrammetry.
Page 1
May 01/16
2-13-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
RIB10
FR54
FR57
2LH
12
2RH
11
RIB10
FR28
FR34
N_AC_021300_1_0020101_01_00
Location of the Leveling Points
FIGURE-2-13-0-991-002-A01
Page 2
May 01/16
2-13-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0
Jacking
**ON A/C A319-100 A319neo
Jacking for Maintenance
1.
Aircraft Jacking Points for Maintenance
A.
General
(1) The A319 can be jacked:
-
At not more than 57 000 kg (125 663 lb),
-
Within the limits of the permissible wind speed when the aircraft is not in a closed
environment.
B.
Primary Jacking Points
(1) The aircraft is provided with three primary jacking points:
-
One located under the forward fuselage (FR8),
-
Two located under the wings (one under each wing, located at the intersection of RIB9
and the datum of the rear spar).
(2) Three jack adapters are used as intermediary parts between the aircraft and the jacks:
-
One male spherical jack adapter of 19 mm (0.75 in) radius, forming part of the aircraft
structure (FR8),
-
Two wing jack pads (one attached to each wing at RIB9 with 2 bolts) for the location
of the jack adaptor.
Wing jack pads are ground equipment.
C.
Auxiliary Jacking Points (Safety Stay)
(1) When the aircraft is on jacks, it is recommended that a safety stay be placed under the
fuselage, between FR73 and FR74, to prevent tail tipping caused by accidental
displacement of the center of gravity.
(2) The safety stay must not be used to lift the aircraft.
(3) A male spherical ball pad with a 19 mm (0.75 in) radius, forming part of the aircraft
structure, is provided for using the safety stay.
2.
Jacks and Safety Stay
A. Jack Design
(1) The maximum permitted loads given in the table in FIGURE 2-14-0-991-005-A are the
maximum loads applicable on jack fittings.
(2) In the fully retracted position (jack stroke at minimum), the height of the jack is such that
the jack may be placed beneath the aircraft in the most adverse conditions, namely, tires
deflated and shock absorbers depressurized. In addition, there must be a clearance of
approximately 50 mm (1.97 in) between the aircraft jacking point and the jack upper end.
Page 1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(3) The lifting jack stroke enables the aircraft to be jacked up so that the fuselage longitudinal
datum line (aircraft center line) is parallel to the ground, with a clearance of 100 mm (3.94
in) between the main landing gear wheels and the ground. This enables the landing gear
extension/retraction tests to be performed.
3.
Shoring Cradles
When it is necessary to support the aircraft in order to relieve the loads on the structure to do
modifications or major work, shoring cradles shall be placed under each wing and the fuselage as
necessary.
NOTE : The aircraft must not be lifted or supported by the wings or fuselage alone without
adequate support of the other.
Page 2
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
WING JACKING
POINT
RIB9
B
FR74
X
FR73
A
C
FR8
Y
FWD JACKING
SAFETY
POINT
STAY
B’
RIB9
WING JACKING
POINT
MAXIMUM
X
Y
LOAD ELIGIBLE
m
ft
m
ft
daN
FORWARD FUSELAGE
2.74
8.99
0
0
6 800
JACKING POINT
A
B
15.97
52.40
6.50
21.33
28 500
WING JACKING
POINT
B’
15.97
52.40
−6.50
−21.33
28 500
SAFETY STAY
C
28.83
94.59
0
0
2 000
NOTE:
SAFETY STAY IS NOT USED FOR JACKING.
N_AC_021400_1_0050101_01_02
Jacking for Maintenance
Jacking Point Locations
FIGURE-2-14-0-991-005-A01
Page 3
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2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
FR8
POINT A DETAIL
Z−1 979.8
Z−1 987
B
A
SPHERICAL RADIUS
19 mm (0.75 in)
B
N_AC_021400_1_0060101_01_00
Jacking for Maintenance
Forward Jacking Point
FIGURE-2-14-0-991-006-A01
Page 4
May 01/16
2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
WING JACK PAD
A
LOWER SURFACE
B
POINT BB’ DETAIL
RIB9INTERSECTION WITH REAR
SPAR DATUM
Z−828.35
A
Z−895
EXAMPLE
SPHERICAL RADIUS
32 mm (1.26 in)
B
N_AC_021400_1_0070101_01_00
Jacking for Maintenance
Wing Jacking Points
FIGURE-2-14-0-991-007-A01
Page 5
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2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FR74
FR73
A
Z−729.441
Z−744.932
SPHERICAL RADIUS 19 mm (0.75 in)
(19 D535−71 595)
126.15 mm
(4.97 in)
A
FWD
N_AC_021400_1_0080101_01_01
Jacking for Maintenance
Safety Stay
FIGURE-2-14-0-991-008-A01
Page 6
May 01/16
2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FR8
FR73 FR74
FUSELAGE
DATUM LINE
FORWARD JACK
WING JACK
SAFETY STAY
N
L
RIB9
RIB9
WING JACK
FORWARD WING JACK
M
JACK
TYPICAL JACK INSTALLATION SHOWN
DISTANCE BETWEEN
JACKING/SAFETY POINTS
AND THE GROUND
CONFIGURATION
DESCRIPTION
L
M
N
(FORWARD
(WING
(SAFETY
JACK)
JACK)
STAY)
− NLG SHOCK ABSORBER DEFLATED AND
NLG TIRES FLAT
1 576 mm
3 119 mm
3 672 mm
− MLG STANDARD TIRES, WITH STANDARD
(62.05 in)
(122.80 in)
(144.57 in)
SHOCK ABSORBERS
− AIRCRAFT ON WHEELS
TIRES FLAT
1 659 mm
2 736 mm
2 834 mm
SHOCK ABSORBERS DEFLATED
(65.31 in)
(107.72 in)
(111.57 in)
STANDARD TIRES
1 859 mm
3 121 mm
3 400 mm
STANDARD SHOCK ABSORBERS
(73.19 in)
(122.87 in)
(133.86 in)
STANDARD TIRES
−AIRCRAFT ON JACKS
MLG SHOCK ABSORBERS EXTENDED WITH
2 554 mm
3 655 mm
3 779 mm
(FORWARD JACK AND
WHEEL CLEARANCE OF 120 mm (4.72 in)
(100.55 in)
(143.90 in)
(148.78 in)
WING JACKS)
FOR MLG RETRACTION OR EXTENSION
− FUSELAGE DATUM LINE
PARALLEL TO THE GROUND
STANDARD TIRES
MLG SHOCK ABSORBERS EXTENDED WITH
3 204 mm
4 305 mm
4 429 mm
WHEEL CLEARANCE OF 770 mm (30.31 in)
(126.14 in)
(169.49 in)
(174.37 in)
FOR REPLACEMENT OF THE MLG
− AIRCRAFT ON FORWARD
STANDARD TIRES
JACK
NLG SHOCK ABSORBERS EXTENDED WITH
2 394 mm
2 882 mm
NA
−MLG WHEELS ON THE
WHEEL CLEARANCE OF 60 mm (2.36 in)
(94.25 in)
(113.46 in)
GROUND
FOR NLG RETRACTION OR EXTENSION
NOTE:
THE SAFETY STAY IS NOT USED FOR JACKING.
N_AC_021400_1_0090101_01_02
Jacking for Maintenance
Jacking Design
FIGURE-2-14-0-991-009-A01
Page 7
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2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
20
40
60
80
30
50
70
90
PERMISSIBLE WIND SPEED (km/h)
55
50
45
40
AIRCRAFT CG (%RC)
35
30
70
25
20
15
60
70
B
65
50
60
55
C
40
A
50
D
45
30
40
TIP UP
SECURITY
35
MARGIN
20
30
0
1
2
3
4
5
6
7
8
9
10
LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1000)
EXAMPLE:
ASSUME AIRCRAFT WITH GROSS WEIGHT OF 47 000 kg A AND CENTER OF GRAVITY
AT 18 % RC B . THE REACTION AT THE WING JACKING POINTS IS 41 500 kg
(20 750 kg PER SIDE)
C
AND THE REACTION AT THE FORWARD FUSELAGE
JACKING POINT IS 5 500 kg D . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE THE WIND
SPEED MUST NOT BE IN EXCESS OF 84 km/h.
N_AC_021400_1_0100101_01_00
Loads at the Aircraft Jacking Points
Wing Jacking Point and Forward Fuselage Jacking Point
FIGURE-2-14-0-991-010-A01
Page 8
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2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FR73 / FR74
(SAFETY STAY)
FR60
RIB4
RIB4
RIB22
RIB22
RIB13
RIB13
FR28
FR9
NOTE: THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
N_AC_021400_1_0110101_01_00
Jacking for Maintenance
Location of Shoring Cradles
FIGURE-2-14-0-991-011-A01
Page 9
May 01/16
2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
Jacking of the Landing Gear
1.
General
Landing gear jacking will be required to lift the landing gear wheels off the ground.
NOTE : You can lift the aircraft at Maximum Ramp Weight (MRW).
NOTE : The load at each jacking position is the load required to give a 25.4 mm (1 in) clearance
between the ground and the tire.
2.
Main Gear Jacking
The main gears are normally jacked up by placing a jack directly under the ball pad.
The ball spherical radius is 19 mm (0.75 in).
It is also possible to jack the main gear using a cantilever jack.
3.
Nose Gear Jacking
For nose gear jacking, a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shock-
absorber sliding tube. Jacking can be accomplished either by placing a jack directly under the ball
pad, or using an adapter fitting provided with an identical ball pad.
Page 10
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
49 x 19 R20
600 mm
(23.62 in)
FULLY
EXTENDED
45 x 16 R20
200 mm
218 mm
25 mm
38 mm
552 mm
(7.87 in)
(8.58 in)
(1 in)
(1.5 in)
(21.73 in)
FULLY
DIA. BALL
RETRACTED
180 mm
INFLATED TIRES
(7.09 in)
ON THE RIM
FLAT TIRES
NOTE: TWIN WHEEL TRACK IS 927 mm (36.5 in).
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK
WITH 2 FLAT TIRES.
THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)
CLEARANCE BETWEEN THE TIRE AND GROUND.
N_AC_021400_1_0170101_01_00
Jacking of the Landing Gear
MLG Jacking Point Location - Twin Wheels
FIGURE-2-14-0-991-017-A01
Page 11
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
643 mm
(25.32 in)
MLG TIRE 49 x 19 R20
CANTILEVER
ARM
552 mm
(21.73 in)
25 mm
(1 in)
FWD
TWIN WHEEL TRACK
927 mm
(36.5 in)
DOUBLE FLAT MLG TIRES
218 mm (8.58 in)
(180 mm (7.09 in)
ON RIM)
409 mm
FORK
(16.1 in)
25 mm
1 620 mm
25 mm
MIN
APPROX
MIN
(1 in)
(63.78 in)
(1 in)
CONTOUR OF TIRES ON GROUND
N_AC_021400_1_0180101_01_00
Jacking of the Landing Gear
MLG Jacking with Cantilever Jack - Twin Wheels
FIGURE-2-14-0-991-018-A01
Page 12
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2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
LOAD AT MLG
JACKING POINT
1 000 kg
40
CG
POSITION
40%
30%
35
25%
20%
14%
30
25
20
15
10
5
30
40
50
60
70
80
x1 000 kg
70
80
90
100
110
120
130
140
150
160
170
180
x1 000 lb
AIRCRAFT WEIGHT
MODEL 100
N_AC_021400_1_0190101_01_00
Jacking of the Landing Gear
Loads at MLG Jacking Points - Twin Wheels
FIGURE-2-14-0-991-019-A01
Page 13
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2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
LOAD AT MLG
JACKING POINT
1 000 kg
CG
POSITION
36
36.0% CG
34
26.0% CG
32
21.0% CG
30
28
14.0% CG
26
24
22
20
18
45
50
55
60
65
70
75
80
x1 000 kg
100
110
120
130
140
150
160
170
180
x1 000 lb
AIRCRAFT WEIGHT
N_AC_021400_1_0200101_01_00
Jacking of the Landing Gear
Loads at MLG Jacking Points - 75 500 kg
FIGURE-2-14-0-991-020-A01
Page 14
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2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
40 mm
128 mm
25 mm
38 mm
326 mm
APPROX
(1.57 in)
(5.04 in)
(1 in)
(1.5 in)
(12.83 in)
DIA. BALL
SAE AS 33559
FWD
500 mm (19.69 in)
264 mm MIN (10.39 in)
289 mm MAX (11.38 in)
198 mm
(7.8 in)
FLAT TIRES
INFLATED TIRES
A
NOTE:
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES.
THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)
CLEARANCE BETWEEN THE TIRE AND GROUND.
N_AC_021400_1_0210101_01_00
Jacking of the Landing Gear
NLG Jacking - Point Location
FIGURE-2-14-0-991-021-A01
Page 15
May 01/16
2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
LOAD AT NLG
JACKING POINT
1 000 kg
CG
POSITION
15
14
14%
13
12
20%
11
25%
10
9
30%
8
7
6
40%
5
4
3
2
1
x1 000 kg
30
40
50
60
70
80
x1 000 lb
70
80
90
100
110
120
130
140
150
160
170
180
AIRCRAFT WEIGHT
MODEL 100
N_AC_021400_1_0220101_01_00
Jacking of the Landing Gear
Loads at NLG Jacking Points
FIGURE-2-14-0-991-022-A01
Page 16
May 01/16
2-14-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
LOAD AT NLG
JACKING POINT
1 000 kg
CG
POSITION
12
14.0% CG
11
21.0% CG
10
26.0% CG
9
8
7
36.0% CG
6
5
4
3
45
50
55
60
65
70
75
80
x1 000 kg
100
110
120
130
140
150
160
170
180
x1 000 lb
AIRCRAFT WEIGHT
N_AC_021400_1_0230101_01_00
Jacking of the Landing Gear
Loads at NLG Jacking Points - 75 500 kg
FIGURE-2-14-0-991-023-A01
Page 17
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0
General Information
**ON A/C A319-100 A319neo
General Information
1.
Standard day temperatures for the altitudes shown are tabulated below:
Standard Day Temperatures for the Altitudes
Altitude
Standard Day Temperature
FEET
METERS
˚F
˚C
0
0
59.0
15.0
2 000
610
51.9
11.1
4 000
1 220
44.7
7.1
6 000
1 830
37.6
3.1
8 000
2 440
30.5
-0.8
Page 1
May 01/16
3-1-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1
Payload / Range - ISA Conditions
**ON A/C A319-100 A319neo
Payload/Range - ISA Conditions
1.
This section provides the payload/range at ISA conditions.
Page 1
May 01/16
3-2-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_030201_1_0130101_01_00
Payload/Range - ISA Conditions
FIGURE-3-2-1-991-013-A01
Page 2
May 01/16
3-2-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_030201_1_0140101_01_00
Payload/Range - ISA Conditions
Sharklet
FIGURE-3-2-1-991-014-A01
Page 3
May 01/16
3-2-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_030201_1_0150101_01_00
Payload/Range - ISA Conditions
FIGURE-3-2-1-991-015-A01
Page 4
May 01/16
3-2-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1
Take-off Weight Limitation - ISA Conditions
**ON A/C A319-100
Take-Off Weight Limitation - ISA Conditions
1.
This section gives the take-off weight limitation at ISA conditions.
Page 1
May 01/16
3-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
110
230
100
220
210
200
90
190
180
80
0
2
170
4
6
160
8
70
150
140
60
130
120
50
110
1000 ft
4
6
8
10
12
14
16
40
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030301_1_0030101_01_00
Take-Off Weight Limitation - ISA Conditions
CFM56 Series Engine
FIGURE-3-3-1-991-003-A01
Page 2
May 01/16
3-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
110
230
100
220
210
200
90
190
180
80
0
2
170
4
6
160
8
70
150
140
60
130
120
50
110
1000 ft
4
6
8
10
12
14
16
40
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030301_1_0040101_01_00
Take-Off Weight Limitation - ISA Conditions
IAE V2500 Series Engine
FIGURE-3-3-1-991-004-A01
Page 3
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3-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2
Take-off Weight Limitation - ISA +15˚C (+59˚F) Conditions
**ON A/C A319-100
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
1.
This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions.
Page 1
May 01/16
3-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
110
230
100
220
210
200
90
190
180
80
0
2
170
4
6
160
8
70
150
140
60
130
120
50
110
1000 ft
4
6
8
10
12
14
16
40
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030302_1_0030101_01_00
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
CFM56 Series Engine
FIGURE-3-3-2-991-003-A01
Page 2
May 01/16
3-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
110
230
100
220
210
200
90
190
180
80
0
2
170
4
6
160
8
70
150
140
60
130
120
50
110
1000 ft
4
6
8
10
12
14
16
40
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030302_1_0040101_01_00
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
IAE V2500 Series Engine
FIGURE-3-3-2-991-004-A01
Page 3
May 01/16
3-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1
Landing Field Length - ISA Conditions
**ON A/C A319-100
Landing Field Length - ISA Conditions
1.
This section provides the landing field length.
Page 1
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3-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
6.0
ISA CONDITIONS
PRESSURE ALTITUDE
SLATS 27 DEG.
(x 1 000 ft)
FLAPS 35 DEG.
10
8
5.5
6
4
2
SEA
LEVEL
5.0
4.5
4.0
3.5
3.0
40
60
80
100
120
140
160
GROSS WEIGHT (x 1 000 lb)
NOTE:
THESE CURVES ARE GIVEN FOR INFORMATION ONLY.
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
N_AC_030401_1_0030101_01_01
Landing Field Length - ISA Conditions
CFM56-5A Series Engine
FIGURE-3-4-1-991-003-A01
Page 2
May 01/16
3-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
5.5
ISA CONDITIONS
PRESSURE ALTITUDE
SLATS 27 DEG.
(x 1 000 ft)
FLAPS 35 DEG.
SEA
10
8
6
4
2
LEVEL
5.0
4.5
4.0
3.5
3.0
40
60
80
100
120
140
160
GROSS WEIGHT (x 1 000 lb)
NOTE:
THESE CURVES ARE GIVEN FOR INFORMATION ONLY.
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
N_AC_030401_1_0040101_01_01
Landing Field Length - ISA Conditions
IAE V2500 Series Engine
FIGURE-3-4-1-991-004-A01
Page 3
May 01/16
3-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0
Final Approach Speed
**ON A/C A319-100
Final Approach Speed
1.
This section provides the final approach speed. It is defined as the indicated airspeed at threshold in
the landing configuration, at the certificated maximum flap setting and Maximum Landing Weight
(MLW), in standard atmospheric conditions. The approach speed is used to classify the aircraft into
an Aircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.
2.
The final approach speed is 126 kt at a MLW of 62 500 kg (137 789 lb) and classifies the aircraft
into the Aircraft Approach Category C.
NOTE : This value is given for information only.
Page 1
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3-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0
General Information
**ON A/C A319-100 A319neo
General Information
1.
This section provides aircraft turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by the
geometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,
it reflects the turning capability of the aircraft in favorable operating circumstances. This data should
only be used as a guideline for the method of determination of such parameters and for the
maneuvering characteristics of this aircraft type.
In ground operating mode, varying airline practices may demand that more conservative turning
procedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airline
operating techniques will vary in the level of performance, over a wide range of operating
circumstances throughout the world. Variations from standard aircraft operating patterns may be
necessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limited
area or a high risk of jet blast damage. For these reasons, ground maneuvering requirements should
be coordinated with the airlines in question prior to layout planning.
Page 1
May 01/16
4-1-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0
Turning Radii
**ON A/C A319-100 A319neo
Turning Radii
1.
This section provides the turning radii.
Page 1
May 01/16
4-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
R3
R1
R5
50°
60°
70°
7.59 m
(24.9 ft)
R2
R6
11.04 m
(36.22 ft)
R4
NOTE:
FOR STEERING DIMENSION TABLE SEE SHEET 2.
TURN TYPE:
1. ASYMMETRIC THRUST DIFFERENTIAL
BRAKING (PIVOTTING ON ONE MAIN GEAR).
2. SYMMETRIC THRUST NO BRAKING.
N_AC_040200_1_0030101_01_02
Turning Radii, No Slip Angle
(Sheet 1)
FIGURE-4-2-0-991-003-A01
Page 2
May 01/16
4-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_040200_1_0040101_01_01
Turning Radii, No Slip Angle
(Sheet 2)
FIGURE-4-2-0-991-004-A01
Page 3
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4-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0
Minimum Turning Radii
**ON A/C A319-100 A319neo
Minimum Turning Radii
1.
This section provides the minimum turning radii.
Page 1
May 01/16
4-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
R4
11.0 m
(36 ft)
R6
OUTSIDE FACE OF TIRE
Y
EFFECTIVE
TURN
A
STEERING
ANGLE 75°
MINIMUM
PAVEMENT
WIDTH FOR
180° TURN
R3
R5
NOTE:
NOSE GEAR RADII TRACK R3,
MEASURED FROM OUTSIDE FACE OF TIRE.
MODEL 100 TURN DIMENSION SHOWN.
THEORETICAL CENTER OF TURN
FOR MINIMUM TURNING RADIUS.
SLOW CONTINUOUS TURNING.
APPROXIMATELY IDLE THRUST
ON ALL ENGINES.
NO DIFFERENTIAL BRAKING.
DRY SURFACE.
TYPE
STEERING
EFFECTIVE
R4 WING
R3
R5
R6
OF
ANGLE
STEERING
Y
A
NLG
WING TIP
NOSE
THS
SHARKLET
TURN
(DEG)
ANGLE
FENCE
m
3.6
20.1
11.7
21.1
22.0
16.5
19.6
1
75 (MAX)
71.9°
ft
12
66
38
69
72
54
64
m
3.9
20.5
11.8
21.4
22.3
16.6
19.7
2
75 (MAX)
70.3°
ft
13
67
39
70
73
54
65
NOTE: IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1
BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
N_AC_040300_1_0020101_01_02
Minimum Turning Radii
FIGURE-4-3-0-991-002-A01
Page 2
May 01/16
4-3-0
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