a320 family general data - black rock global services - diversify
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1
A320 FamilyTechnical appendices
All Aboutthe
2
Technical appendices
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Page 3 May 2009
Technical appendices - Contents
A320 Family general dataKey data Page 4
Standard cabin layouts Page 8
Lower deck Page 11
Additional fuel capacity Page 14
A320 Family technology featuresFlight deck Page 16
Centralised Fault Display System Page 22
Fly-by-wire system Page 25
Wing movable surfaces Page 27
Engines Page 28
A320 Family performanceRange capability Page 31
Take-off performance Page 39
Landing performance Page 47
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Page 4 May 2009
A318 Key data
Span 111ft 10in 34.10mLength 103ft 2in 31.44mHeight 41ft 1in 12.51mFuselage width 13ft 3.95m
Maximum take-off weight: -basic-options
59 000 kg61 500 kg63 000 kg64 500 kg66 000 kg68 000 kg
130 070 lb135 580 lb138 890 lb142 200 lb145 500 lb149 900 lb
Maximum landing weight: -basic-option
56 000 kg57 500 kg
123 460 lb126 770 lb
Maximum zero-fuel weight: -basic-option
53 000 kg54 500 kg
116 840 lb120 150 lb
Fuel capacity: -basic 24 210 litres 6 400 USG
Operating weight empty (typical): 39 500 kg 87 080 lb
Seats: - typical two-class- maximum
107132 (exit limit 145)
Underfloor capacity: - basic 21.21 m3 749 ft3
Powerplants: - PW6000A- CFM56-5B
22 100 lb to 23 800 lb slst21 600 lb to 23 300 lb slst
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Page 5 May 2009
A319 Key data
Span 111ft 10in 34.10mLength 111ft 33.84mHeight 38ft 7in 11.76mFuselage width 13ft 3.95m
* with double overwing exit
Maximum take-off weight: -basic-options
64 000 kg68 000 kg70 000 kg75 500 kg
141 100 lb149 920 lb154 330 lb166 450 lb
Maximum landing weight: -basic-option
61 000 kg62 500 kg
134 480 lb137 790 lb
Maximum zero-fuel weight: -basic-option
57 000 kg58 500 kg
125 660 lb128 970 lb
Fuel capacity: - basic- options
24 210 litresup to 30 190 litres
6 400 USGup to 7 980 USG
Operating weight empty (typical): 40 800 kg 89 950 lb
Seats: - typical two-class- maximum*
124160
Underfloor capacity: -basic- option
27.62 m3 976 ft3
4 LD3-45(W) + 7.22 m3/255 ft3
Powerplants: - CFM56-5B- V2500-A5
22 000 lb to 27 000 lb slst22 000 lb to 26 500 lb slst
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Page 6 May 2009
A320 Key data
Span 111ft 10in 34.10mLength 123ft 3in 37.57mHeight 38ft 7in 11.76mFuselage width 13ft 3.95m
Maximum take-off weight: -basic-options
73 500 kg75 500 kg77 000 kg78 000 kg
162 040 lb166 450 lb169 750 lb171 960 lb
Maximum landing weight: -basic-option
64 500 kg66 000 kg
142 200 lb145 500 lb
Maximum zero-fuel weight: -basic-option
61 000 kg62 500 kg
134 480 lb137 780 lb
Fuel capacity: - basic- options
24 210 litresup to 30 190 litres
6 400 USGup to 7 980 USG
Operating weight empty (typical): 42 600 kg 93 920 lb
Seats: - typical two-class- maximum
150180
Underfloor capacity: -basic- option
37.41 m3 1 322 ft3
7 LD3-45(W) + 5.89 m3/208 ft3
Powerplants: - CFM56-5B- V2500-A5
22 000 lb to 27 000 lb slst26 500 lb slst
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Page 7 May 2009
A321 Key data
Span 111ft 10in 34.10mLength 146ft 44.51mHeight 38ft 7in 11.76mFuselage width 13ft 3.95m
Maximum take-off weight: -basic-options
89 000 kg93 000 kg93 500 kg
196 200 lb205 000 lb206 130 lb
Maximum landing weight: -basic-option
75 500 kg77 800 kg
166 450 lb171 520 lb
Maximum zero-fuel weight: -basic-option
71 500 kg73 800 kg
157 630 lb162 700 lb
Fuel capacity: - basic- options
24 050 litresup to 30 030 litres
6 350 USGup to 7 930 USG
Operating weight empty (typical): 48 500 kg 106 920 lb
Seats: - typical two-class- maximum
185220
Underfloor capacity: -basic- option
51.73 m3 1 828 ft3
10 LD3-45(W) + 5.89 m3/208 ft3
Powerplants: - CFM56-5B- V2500-A5
30 000 lb to 33 000 lb slst30 000 lb to 33 000 lb slst
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Page 8 May 2009
A320 Family standard cabin layouts
Typical two-class layouts
A318: 107 seats8F at 38in + 99Y at 32in pitch
A319: 124 seats8F at 36in + 116Y at 32in pitch
A320: 150 seats12F at 36in + 138Y at 32in pitch
A321: 185 seats16F at 36in+ 169Y at 32in pitch
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Page 9 May 2009
A320 Family standard cabin layouts
Single-class layouts
A318: 117 seats117Y at 32in pitch
A319: 134 seats134Y at 32in pitch
A320: 164 seats164Y at 31/32in pitch
A321: 199 seats199Y at 32in pitch
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Page 10 May 2009
A320 Family standard cabin layouts
Single-class, high density layouts
A318: 132 seats132Y at 29/30in pitch
A319: 156 seats156Y at 28/30in pitch
A320: 180 seats180Y at 28/29in pitch(179Y under FAA regulations)
A321: 220 seats220Y at 28/29in pitch
S
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Page 11 May 2009
A320 Family lower deck Basic bulk loading configuration
A319132in
(3.35m)174in
(4.43m)128in
(3.24m)Bulk mode
Usable volume:976ft3
A320191in
(4.85m)128in
(3.24m)258in
(6.55m)Bulk mode
Usable volume:1 322ft3
A321128in
(3.24m)321in (8.15m)321in (8.15m)Bulk mode
Usable volume:1 828ft3
A318101in
(2.56m)
Bulk mode Usable volume:
749ft3132in
(3.35m)107in
(2.71m)
The wider cross-section of the A320 Family means that its cargo compartments offer more convenient working space and a larger loading area than any other single-aisle aircraft.
Manual loading advantages: no investmentmaximum available volumeno OWE impactlittle infrastructure needs
Can be easily loaded from a simple flat-bed truck
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Page 12 May 2009
A319, A320 and A321 lower deck Cargo loading system (CLS)
Turnarounds, with a full load of cargo and baggage, can be as short as 25 minutes. The container system is fully compatible with existing ground service equipment, thus reducing extra inventory costs. CLS advantages:
Faster turnaroundsIncreased revenue potentialBetter bad-weather operationsReduced damage to payloadReduced labour costsImproved working environmentWidebody interline capacity
CLS in action
A319
Optional LD3-40-45
Five ULDs (containers or pallets)Usable volume:
520(+ 80) ft3
+ 255ft3 bulk
A320 Seven ULDs (containers or pallets)Usable volume:
910ft3
+ 208ft3 bulk
A321 Ten ULDs (containers or pallets)Usable volume:
1 300ft3+ 208ft3 bulk
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Page 13 May 2009
Standard containers
A320 Family container system
A320 Long range-compatible unit load devices :
79in
45in 110ft3
61.5in 60.4in
LD3-45 container (one door)
45in 130ft3
61.5in 60.4in
96.5in
LD3-45W container or pallet (one or two doors)
LD3-45 rectangularcontainer or pallet to 45in high
60.4in
61.5in
90ft345in
LD3-45 LD3-45W LD3-45 rectangularMax. gross weight kg
lb11342500
container 11342500
pallet container 11342500
pallet
Internal volume m3
ft33.1110
3.6130
3.6130
2.590
2.484
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Page 14 May 2009
Additional fuel capacity
A319 lower deck with ACTs
Two additional centre tanks
One additional centre tank
Impact / Firewall
ACT Optional LD3-40-45
ACT
Optional LD3-40-45
Four ULDs (containers or pallets):Usable volume: 390 (+80) ft3 + 255ft3
Bulk mode:Usable volume: total 810 ft3
Three ULDs (containers or pallets):Usable volume: 260 (+80) ft3 + 255ft3
Bulk mode:Usable volume: total 664 ft3
The A319, A320 and A321 can be fitted with one or two Additional Centre Tanks (ACTs) each holding around 3000 litres, providing operators with extra range.
Operators can match various market requirements for more range or more cargo with a single aircraft.
For example, an airline can use the cargo capacity on its network during the winter and then take advantage of the ACTs and increase range to make charter operations viable during the summer.
The ACTs can be installed either in bulk and / or CLS mode.
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Page 15 May 2009
Additional fuel capacity
A320 lower deck with ACTs
A321 lower deck with ACTs
Six ULDs (containers or pallets):Usable volume: 780 ft3 + 208ft3
Bulk mode:Usable volume: total 1156 ft3
Five ULDs (containers or pallets):Usable volume: 650 ft3 + 208ft3
Bulk mode:Usable volume: total 990 ft3
Nine ULDs (containers or pallets):Usable volume: 1170 ft3 + 208ft3
Bulk mode:Usable volume: total 1662 ft3
Height ULDs (containers or pallets):Usable volume: 1040 ft3 + 208ft3
Bulk mode:Usable volume: total 1496 ft3
Two additional centre tanks
One additional centre tank
Impact / Firewall
ACT
ACT
Two additional centre tanks
One additional centre tank
Impact / Firewall
ACT
ACT
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Page 16 May 2009
A320 Family flight deck
The advanced flight deck of the A320 Family is virtually identical to that of the A330 and A340 Families and has a very high commonality with the one of the A350 XWB and A380 Families.
An optimised layout of six LCD (Liquid Crystal Display) screens ensures that the two-person crew can easily assimilate all relevant data
EFIS displays, for flight informationECAM displays, for systems, engine and warnings informationAll six LCDs are interchangeable, functionally andby part number.
The absence of heavy, bulky control columns between the pilotsand their instruments, ensures an unimpeded view.
Two Multipurpose Control and Display Units (MCDU) on thepedestal, in addition to accessing the Flight Management System (FMS), are used to give systems maintenance data,in the air and on the ground, upon request.
The system is coupled to a printer and can also be coupled to an optional Aircraft Communication Addressing and Reporting System (ACARS) link.
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Page 17 May 2009
Main instrument panel
Real time flight and systems data are displayed to the pilots on six LCDs.
Flight information is provided by the Electronic Flight Instrument System (EFIS) comprising:Primary Flight Display (PFD)Navigation Display (ND) in front of each pilot.
Systems information is provided by the Electronic Centralised Aircraft Monitor (ECAM) comprising:Engine instrumentation and warnings on the upper screenAircraft systems on the lower screen.
The EFIS-ECAM six-LCD design brings:Lower spares investmentHigher dispatch reliability and enhanced safetyLower crew workload.
Features Integrated Stand-by Instrumentation System (ISIS) on one additional LCD screen.
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Page 18 May 2009
Main instrument panel
Design features :Only 12 main-panel instrumentsLCDs identical and interchangeableAutomatic display reconfiguration in event of CRT failureExcellent ergonomics ease interface between pilot and machine
Retractable tables
Retractable foot rests
Sidestick controllers
ISIS Systems Display
Engine / WarningDisplay
ECAMSystems information
FMS CFDS
MCDUFlight management
Fault display
PFDND
EFISFlight information
PFD ND
EFISFlight information
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Page 19 May 2009
Primary Flight Display
The Primary Flight Displays provide clear and accurate information on a range of parameters including air speed, altitude, attitude and guidance information and heading of the aircraft.
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Page 20 May 2009
Navigation Display
The Navigation Displays are located inboard of each Primary Flight Display and provide the pilots with data on the aircraft’s position and course.
The ND has three selectable modes:Arc mode: Heading up, horizon limited to a 90° forward sector, with weather radar availableRose mode: (ILS, VOR, or NAV): Heading up, aircraft symbol in screen centre, with weather radar availablePlan mode: Display is centred on the selected waypoint, north up.
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Page 21 May 2009
Electronic Centralised Aircraft Monitor (ECAM)
Systems information is presented by the ECAM on two screens on the centre console. Sensors throughout the aircraft continuously monitor the systems and, if a parameter moves out of the normal range, automatically warn the pilot. The ECAM system is unique to Airbus aircraft.
Upper display Lower display
Engine / warning displayPrimary engine parameters operational status
N1 limit mode, fuel quantity,flap/slat settings
Memo and warning information
System displayFlight phase related systems data System pages selectable on demandAutomatic display of a system page in the event of a malfunction
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Page 22 May 2009
Centralised Fault Display System (CFDS)
CFDIUSystemcomputers
Printer
ACARS
The Centralised Fault Display Interface Unit (CFDIU), can be interrogated from the cockpit through the Multi purpose Control and Display Unit (MCDU) and the information provided on the on-board printer
The MCDU is the interactive interface between the maintenance crew and the systems
The computers in each system have Built-In Test Equipment (BITE) which send the results of their tests to an interface unit, the CFDIU
The CFDIU can also be interrogated from a ground station and the information transmitted via Aircraft Communication and Reporting System (ACARS)
The A320 demonstrates class leading reliability and has the lowest maintenance costs in its class
CFDS functions and advantages: Identification of failed componentsDisplay / print-out of dataReal-time reporting of data to ground facilitiesUnjustified removal of components minimisedImproved troubleshootingQuicker turnaroundsSimple to useFirst-time fault-finding
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Page 23 May 2009
AIRMAN
Integrated electronic documentation:AIRMAN provides direct Access to Airn@v (AMM, TSM, IPC, MEL…) through hyperlinks.
Airline network
Maintenancefault message
Aircraft: downloadedreal-time fault data
Operator logbook entries
ACARSACARS
CentralFault
Display System
Post Flight Report
CFDS is connected with the ACARS system
Information can be transmitted to the ground in real time
Fault analysis and parts logistics done before the aircraft lands
The CFDS is complemented by AIRMAN(AIRcraft Maintenance ANalysis):
A ground-based software tool dedicated to the identification andthe management of unscheduled maintenanceIt allows fast, efficient and simple trouble-shooting reducing costs
AIRMAN is the definitive tool for fast, efficient trouble-shooting
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Page 24 May 2009
Maintenance optimisation
The A320 Maintenance check intervals have been escalated several times since entry into service. This is proof of the low-level of non-routine findings in A320 maintenance.A more flexible maintenance program (non “letter check”) is available to all operators since Jan 2005. Usage parameters (days or months/ Flight hours/Flight cycles) are now used in order to optimise the resulting intervals for each Operator’ utilisation.The tasks of former A and C checks are split between 3 different sub-groups which have their interval expressed in the corresponding usage parameter (calendar / hourly / cyclic).Each Operator is therefore able to optimise the Checks intervals depending on their own aircraft utilisation.
Entry into Entry into serviceservice
Until Dec Until Dec 20042004 Current positionCurrent position
DailyWeekly
36 hours36 hours8 cal. days8 cal. days
36 hours36 hours8 cal. Days8 cal. Days
36 hours36 hours8 cal. Days8 cal. Days
A checkC check
350 FH350 FH15 mths15 mths
500 FH500 FH15 mths15 mths
600FH/750FC/100 days600FH/750FC/100 days20 mths/4500FC/6000FH20 mths/4500FC/6000FH
Zonal/Structure 4/8 years4/8 years 5/10 years5/10 years 6/12 years6/12 years
Fatigue threshold 20 000 FC20 000 FC 24 000 FC24 000 FC 24 000 FC24 000 FC
Landing gear overhaul 10 years / 20 000 FC
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Page 25 May 2009
Fly-by-wire flight controls
A320 Family fly-by-wire advantages: Incorporates flight envelope protectionReduces costsReduces pilot workloadImproves aircraft performance
Airbus was the pioneer in electrical flight control systems on commercial aircraft. The advantages of this method of control are such that it is a feature of all current major passenger aircraft - except the 737 NG.
Basic architecture of Basic architecture of Fly-by-wire
Spoiler and ElevatorSpoiler and Elevator ComputersComputers
(SEC)(SEC)
Flight AugmentationFlight Augmentation ComputersComputers
(FAC)(FAC)
Elevator and Elevator and Aileron ComputersAileron Computers
(ELAC)(ELAC)
ElevatorsAilerons
Rudder
Spoilers
ElevatorsStabiliser
trim
Rudder pedals
(1)
(2)(3)
(1)
(2)
(1)
(2)
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Page 26 May 2009
Fly-by-wire flight controls
Safety concepts: High level of redundancyUse of dissimilar redundancy (different computer types, different micro-processor types, different vendors)Each computer divided into two physically separate unitsSegregated power supply sourcesMaximum physical segregation in signalling lanes
Seven computers:2 ELAC (Elevator and Aileron Computer)2 FAC (Flight Augmentation Computer)3 SEC (Spoiler and Elevator Computer)Three hydraulic systems, Blue, Green and Yellow are used to control the flight control surfaces
Flight controls - Schematic
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Page 27 May 2009
Wing movable surfaces
The A320 Family wing features state-of-the-artleading and trailing edge devices :
Inner and outer flaps, of composite materialRemovable without requiring access to integral fuel tankDeployment up to 40 degrees
Full span slats in five sections, of aluminum alloy materialDeployment up to 27 degrees
Five composite air brakes for roll control and braking
Electrically signaled aileron, of composite material
Removable wing tip
Advanced drag-reducing wingtipdevices are standard
Inner Flap
Flap Track 4
Flap Track 3
Flap Track 2Outer Flap
Aileron
Slat 5
Slat 4
Slat 3
Slat 2
Slat 1
Air Brake
54
3
12
A318/A319/A320 wing shown
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Page 28 May 2009
Competitive choice of engines on A320 Family
The A320 was designed from the beginning to have the most advanced high by-pass-ratio fan engines, from two manufacturers, CFM International or International Aero Engines. Now, Pratt & Whitney have joined the family with the PW6000A for the A318.
The uncompromised design of the engine installation combined with the advanced aerodynamic design of the wings means that the A320 Family uses less fuel per seat than its nearest competitors, conserving fuel and at the same time generating less pollution.
PW6000A CFM56-5B V2500-A5
Aircraft applications A318 A318/A319/A320/A321 A319/A320/A321
Nominal thrust range-lbt 22100/23800 21600/33000 22000/33000
Fan diameter-in 56.5 68.3 63.5
Configuration 1.4.5.C.1.3 1.4.9.C.1.4 1.4.10.C.2.5
Nacelle Mixed flow Separate flow Mixed flow
Thrust reverserReverser actuationGearbox
ClamshellHydraulic
Fan mounted
Pivoting doorHydraulic
Fan mounted
CascadesHydraulic
Fan mounted
Controls FADEC FADEC FADEC
Engine characteristics
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Page 29 May 2009
Full Authority Digital Engine Control (FADEC) functions:Full engine fuel controlThrust setting computationEngine limit protectionAutomatic start sequencing / monitoringThrust reverser control / feedbackFlight deck indicationsEngine health monitoring
Advanced engine control
FADEC advantages: Substitution of hydromechanical control system
reduced weight and fuel burnIncreased automation
reduced pilot workloadOptimised engine control
reduced maintenance cost
FADEC lowers costs and increases engine life
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Page 30 May 2009
A320 Family APU
The Auxiliary Power Unit (APU) provides:Electrical power on ground and in flight Bleed air to the pneumatic system for engine start and / or cabin controlFree park-group ground operations capabilityIn flight relight capability
The A320 Family provides competition for the APU. Three APUs are available:Honeywell GTCP36-300A (standard)APIC APS 3200 (standard option)Honeywell GTCP131-9A (standard option).
Commonality and interchangeabilityA321 APU standard can be used without conversion on A320, A319 or A318 and vice versa.APIC and Honeywell APUs, including their ECBs, are interchangeable on A318/A319/A320/A321.APU change does not require modification of any other system (Drop-In interchangeability).Total modification is contained within the APU/ECB system.The Honeywell APU 131-9A is Drop-In equipment for the A318/A319/A320/A321 with no change tothe aircraft structure.
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Page 31 May 2009
1400 nm 3100 nm
0
5
10
15
20
0 500 1000 1500 2000 2500 3000 3500 4000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
Payl
oad
(100
0 lb
)
MTOW68.0t / 149900lb
MTOW59.0t / 130050lb
107 passengers + baggage
107 passengers + 5.1 t (11200lb) cargo
A318 range capability
CFMI enginesJAR3% flight profile
200nm alternate
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Page 32 May 2009
1350 nm 3000 nm
0
5
10
15
20
0 500 1000 1500 2000 2500 3000 3500 4000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
Payl
oad
(100
0 lb
)
MTOW68.0t / 149900lb
MTOW59.0t / 130050lb
107 passengers + baggage
107 passengers + 5.3 t (11600lb) cargo
A318 range capability
PW enginesJAR3% flight profile
200nm alternate
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Page 33 May 2009
3600 nm1800 nm
0
5
10
15
20
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
Payl
oad
(100
0 lb
)
MTOW75.5t / 166500lb
MTOW64.0t / 141100lb
124 passengers + baggage
124 passengers + 5.4 t (11800lb) cargo
Supplementary fuel options
A319 range capability
CFMI enginesJAR3% flight profile
200nm alternate
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3600 nm1800 nm
0
5
10
15
20
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
Payl
oad
(100
0 lb
)
MTOW75.5t / 166500lb
MTOW64.0t / 141100lb
124 passengers + baggage
124 passengers + 5.3 t (11600lb) cargo
Supplementary fuel options
A319 range capability
IAE enginesJAR3% flight profile
200nm alternate
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Page 35 May 2009
2600 nm
2900 nm
3200 nm
0
5
10
15
20
25
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
50
Payl
oad
(100
0 lb
)
150 passengers + baggage
150 passengers + 6.3 t (13800lb) cargo
MTOW73.5t / 162050lb
MTOW78t / 171950lb
Supplementary fuel option
A320 range capability
CFMI enginesJAR3% flight profile
200nm alternate
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Page 36 May 2009
2900 nm
3200 nm2600 nm
0
5
10
15
20
25
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
50
Payl
oad
(100
0 lb
)
150 passengers + baggage
150 passengers + 6.2 t (13600lb) cargo
MTOW73.5t / 162050lb
MTOW78t / 171950lb
Supplementary fuel option
A320 range capability
IAE enginesJAR3% flight profile
200nm alternate
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Page 37 May 2009
2400 nm
2700 nm
3000 nm
0
5
10
15
20
25
30
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
50
60
Payl
oad
(100
0 lb
)
185 passengers + baggage
185 passengers + 8.5 t (18700lb) cargoMTOW
89t / 196200lb
MTOW93.5t / 206100lb
Supplementary fuel options
A321 range capability
CFMI enginesJAR3% flight profile
200nm alternate
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Page 38 May 2009
2700 nm
3000 nm2400 nm
0
5
10
15
20
25
30
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000
Distance (nm)
Payl
oad
(t)
0
10
20
30
40
50
60
Payl
oad
(100
0 lb
)
185 passengers + baggage
185 passengers + 8.4 t (18500lb) cargoMTOW
89t / 196200lb
MTOW93.5t / 206100lb
Supplementary fuel options
A321 range capability
IAE enginesJAR3% flight profile
200nm alternate
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Page 39 May 2009
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 1,000 1,500 2,000 2,500 3,000
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B8/3CFM56-5B9/3PW6122PW6124
A318 Take-off performance
Sea level,ISA+15°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 40 May 2009
A318 Take-off performance
2000ft,ISA+20°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 1,000 1,500 2,000 2,500 3,000
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B8/3CFM56-5B9/3PW6122PW6124
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Page 41 May 2009
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 1,000 1,500 2,000 2,500 3,000
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B5/3CFM56-5B6/3CFM56-5B7/3V2522-A5V2524-A5V2527M-A5
A319 Take-off performance
Sea level,ISA+15°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 42 May 2009
A319 Take-off performance
2000ft,ISA+20°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 1,000 1,500 2,000 2,500 3,000
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B5/3CFM56-5B6/3CFM56-5B7/3V2522-A5V2524-A5V2527M-A5
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Page 43 May 2009
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 1,000 1,500 2,000 2,500 3,000
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B4/3
V2527-A5
A320 Take-off performance
Sea level,ISA+15°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 44 May 2009
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 1,000 1,500 2,000 2,500 3,000
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B4/3
V2527-A5
A320 Take-off performance
2000ft,ISA+20°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 45 May 2009
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 700 900 1,100 1,300 1,500 1,700 1,900 2,100 2,300 2,500
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B1/3CFM56-5B3/3V2530-A5V2533-A5
A321 Take-off performance
Sea level,ISA+15°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 46 May 2009
750
1,000
1,250
1,500
1,750
2,000
2,250
2,500
2,750
3,000
500 700 900 1,100 1,300 1,500 1,700 1,900 2,100 2,300 2,500
Distance (nm)
Take
-off
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
7,500
8,500
9,500
Take
-off
dist
ance
(ft)
CFM56-5B1/3CFM56-5B3/3V2530-A5V2533-A5
A321 Take-off performance
2000ft,ISA+20°C
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 47 May 2009
750
1000
1250
1500
1750
2000
50 52 54 56 58 60
Landing weight (t)
Land
ing
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
Land
ing
dist
ance
(ft)
CFM56-5BPW6000A
Sea level
2000 ft
Typical landing weightMLW
A318 Landing performance
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 48 May 2009
750
1000
1250
1500
1750
2000
50 52 54 56 58 60 62 64
Landing weight (t)
Land
ing
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
Land
ing
dist
ance
(ft)
CFM56-5BV2500-A5
Sea level
2000 ft
Typical landing weightMLW
A319 Landing performance
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 49 May 2009
750
1000
1250
1500
1750
2000
50 52 54 56 58 60 62 64 66 68 70
Landing weight (t)
Land
ing
dist
ance
(m)
2,500
3,500
4,500
5,500
6,500
Land
ing
dist
ance
(ft)
CFM56-5BV2500-A5
Sea level
2000 ft
Typical landing weight
MLW
A320 Landing performance
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 50 May 2009
750
1000
1250
1500
1750
2000
60 62 64 66 68 70 72 74 76 78 80
Landing weight (t)
Land
ing
dist
ance
(m)
2500
3500
4500
5500
6500
Land
ing
dist
ance
(ft)
CFM56-5BV2500-A5
Sea level
2000 ft
Typical landing weight
MLW
A321 Landing performance
JAR3% flight profile
Typ. 2-class pass. payload
200nm alternate
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Page 51 May 2009
Assumptions
Performance assumptions (“typical airline” rules)
Weight standards: OWEs are to “typical airline” assumptions including an allowance for cabin changes and option selection. Cabin layouts are as shown in the cabin section.
Flight profile: En-route profile includes engine start and taxi-out, take-off, climb, cruise, descent, approach, landing and taxi-in. Sector distance comprises the climb, cruise and descent phases.
Payloads: Passenger + baggage weights are 90.7kg / 200lb. Volumetric payloads assume an average baggage volume of 3.0ft3 per passenger, a bulk and ULD loadability of 85% and cargo with an average density of 10ft3.
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Page 52 May 2009
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
This document and all information contained herein is the sole property of AIRBUS S.A.S.. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied.
The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof.
AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.
AIRBUS S.A.S.31707 BLAGNAC CEDEX, FRANCE
REFERENCE CSMS_PR0907198_V1May 2009
PRINTED IN FRANCE© AIRBUS S.A.S. 2009
ALL RIGHTS RESERVED