Airbus A320. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016-2023)

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

1.80 m

(5.91 ft)

0.48 m

0.81 m

(1.57 ft)

(2.66 ft)

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)

SEE

0.03 m

CHAPTER

(0.10 ft)

2−3

N_AC_020700_1_0220101_01_00

Doors Clearances

Forward Passenger/Crew Doors

FIGURE-2-7-0-991-022-A01

Page 4

Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

FWD

0.85 m

(2.79 ft)

14.43 m

(FROM NOSE)

(47.34 ft)

0.50 m

(1.64 ft)

0.47 m

(1.54 ft)

SEE

SECTION

0.20 m

2−3

(0.66 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)

A A

B B

(FRAME 47)

NOTE:

ESCAPE SLIDE COMPARTMENT DOOR OPENS ON WING UPPER SURFACE.

N_AC_020700_1_0230101_01_00

Doors Clearances

Emergency Exits

FIGURE-2-7-0-991-023-A01

Page 5

Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

1.79 m

(5.87 ft)

0.81 m

(2.66 ft)

FWD

CRITICAL

CLEARANCE

LIMIT

0.58 m

A (1.90 ft)

2.44 m

(8.01 ft)

29.64 m

(FROM NOSE)

(97.24 ft)

0.03 m

SEE

1.85 m

(0.10 ft)

CHAPTER

(6.07 ft)

2−3

0.60 m

(1.97 ft)

A A

N_AC_020700_1_0240101_01_00

Doors Clearances

Aft Passenger/Crew Doors

FIGURE-2-7-0-991-024-A01

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Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

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

(12.96 ft)

1.82 m

(5.97 ft)

A A

2.71 m

(8.89 ft)

CFM56 = 2.18 m (7.15 ft)

IAE V2500 = 2.11 m (6.92 ft)

N_AC_020700_1_0250101_01_00

Door Clearances

Forward Cargo Compartment Door

FIGURE-2-7-0-991-025-A01

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Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320neo

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

(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 = 2.05 m (6.73 ft)

N_AC_020700_1_0260101_01_00

Door Clearances

Forward Cargo Compartment Door

FIGURE-2-7-0-991-026-A01

Page 8

Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

22.69 m

(FROM NOSE)

(74.44 ft)

1.43 m

1.23 m

(4.69 ft)

(4.04 ft)

FWD

SEE

CHAPTER

2−3

3.95 m

1.82 m

(12.96 ft)

(5.97 ft)

A A

FWD

2.03 m

(6.66 ft)

N_AC_020700_1_0270101_01_00

Doors Clearances

Aft Cargo Compartment Door

FIGURE-2-7-0-991-027-A01

Page 9

Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

16.36 m

1.83 m

(53.67 ft)

(6.00 ft)

AIRCRAFT

1.94 m

0.49 m

(6.36 ft)

(1.61 ft)

0.21 m

(0.69 ft)

1.76 m

84?

(5.77 ft)

1.23 m

(4.04 ft)

GROUND LINE

0.14 m

(0.46 ft)

NOTE:

VALUE OF CG: 25% RC.

N_AC_020700_1_0290101_01_00

Doors Clearances

Main Landing Gear Doors

FIGURE-2-7-0-991-029-A01

Page 11

Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

16.23 m

2.23 m

(53.25 ft)

(7.32 ft)

AIRCRAFT

1.94 m

0.49 m

(6.36 ft)

(1.61 ft)

1.76 m

82.5?

(5.77 ft)

1.27 m

(4.17 ft)

GROUND LINE

0.16 m

(0.52 ft)

NOTE:

VALUE OF CG: 25% RC.

N_AC_020700_1_0300101_01_00

Doors Clearances

Main Landing Gear Doors (Bogie)

FIGURE-2-7-0-991-030-A01

Page 12

Dec 01/20

2-7-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

2-8-0

Escape Slides

**ON A/C A320-200 A320neo

Escape Slides

General

This section provides location of slides/rafts facilities and related clearances.

Location

Slides/rafts facilities are provided at the following locations:

One single or dual lane slide at each door 1 & 4 (total four)

Dual lane overwing slides are installed above the wings in the left and right wing-to-fuselage

fairings for off-the-wing evacuation (total 2).

Page 1

Dec 01/20

2-8-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

2-9-0

Landing Gear

**ON A/C A320-200 A320neo

Landing Gear

General

The landing gear is of the conventional retractable tricycle type comprising:

Two main gears with twin-wheel or four-wheel bogie assembly,

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.

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.

B. Four-Wheel Bogie

Each of the two main landing gear assemblies consists of a direct-action shock absorber on

which is installed a four-wheel bogie beam.

The shock absorber is 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.

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.

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.

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@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

A steering disconnection box is installed on the nose landing gear to allow steering deactivation for

towing purposes.

Landing Gear Servicing Points

A. General

Filling of the landing-gear shock absorbers is done through MIL-PRF-6164 standard valves.

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.

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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Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

HINGED FAIRING

(MECHANICALLY OPERATED)

HINGED

FAIRING

FIXED

DOOR ACTUATING CYLINDER

FAIRING

ADJUSTABLE

RAMP

PROXIMITY SENSORS

STEPS

UPLOCK

ROLLER

FIXED

ACTUATING CYLINDER

MAIN DOOR

RAMPS

(HYDRAULICALLY OPERATED)

DOWNLOCK

ACTUATOR

LOCK STAY

MAIN FITTING

SIDE STAY

SHOCK ABSORBER

TORQUE

LINK

NOTE: MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION.

N_AC_020900_1_0100101_01_00

Landing Gear

Main Landing Gear - Twin-Wheel (Sheet 1 of 2)

FIGURE-2-9-0-991-010-A01

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2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

DOOR

LOCKSTAY

LOCKING

GROUND LOCK SLEEVE

ACTUATING

CYLINDER

LOCKING

FLAG

BOTTOM FILLING AND

CHARGING CONNECTION

TOP FILLING AND CHARGING

CONNECTION

EXAMPLE

N_AC_020900_1_0100102_01_01

Landing Gear

Main Landing Gear - Twin-Wheel (Sheet 2 of 2)

FIGURE-2-9-0-991-010-A01

Page 4

Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

2 265 mm

(89.17 in)

2 868.70 mm

(112.94 in)

3 795 mm

COMPRESSED

(149.41 in)

EXTENDED

469.90 mm

(18.50 in)

3 453 mm

80?30

(135.94 in)

20 252.50 mm

RETRACTION

(797.34 in)

ANGLE

927.10 mm

(36.50 in)

N_AC_020900_1_0110101_01_00

Landing Gear

Main Landing Gear Dimensions - Twin-Wheel

FIGURE-2-9-0-991-011-A01

Page 5

Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

HINGED

FAIRING

FIXED

DOOR ACTUATING

FAIRING

CYLINDER

STEPS

AJUSTABLE

RAMP

MAIN DOOR

ACTUATING CYLINDER

UPLOCK

DOOR

ROLLER

RAMPS

DOWNLOCK

ACTUATOR

LEG UNIT

STRUT ASSEMBLY

LOCK STAY

SHOCK ABSORBER

TORQUE

PITCH TRIMMER

LINK

BRAKE BAR

NOTE: MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION.

N_AC_020900_1_0120101_01_00

Landing Gear

Main Landing Gear - Four-Wheel Bogie (Sheet 1 of 2)

FIGURE-2-9-0-991-012-A01

Page 6

Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

DOOR

LOCKSTAY

LOCKING

GROUND LOCK SLEEVE

ACTUATING

CYLINDER

LOCKING

FLAG

TOP FILLING AND CHARGING

CONNECTION

N_AC_020900_1_0120102_01_01

Landing Gear

Main Landing Gear - Four-Wheel Bogie (Sheet 2 of 2)

FIGURE-2-9-0-991-012-A01

Page 7

Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

2 506 mm

(98.66 in)

2 978.70 mm

(117.27 in)

COMPRESSED

Y = 3 795 mm

(149.41 in)

X = 20 266 mm

80?30

(797.87 in)

RETRACTION

ANGLE

1 005 mm

(39.57 in)

780 mm

(30.71 in)

N_AC_020900_1_0130101_01_00

Landing Gear

Main Landing Gear Dimensions - Four-Wheel Bogie

FIGURE-2-9-0-991-013-A01

Page 8

Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

DOOR UPLOCK

BELL

FR9

ASSEMBLY

GEAR UPLOCK

CRANK

DRAG STRUT

ASSEMBLY

DOOR

ASSEMBLY

FR20

ACTUATING

CYLINDER

CONTROL ROD

ROTATING ROD

FITTING

ASSEMBLY

FWD DOORS

AFT DOORS

LEG DOOR

ACTUATING

CYLINDER

DOWNLOCK

PROXIMITY

DETECTORS

NOSE WHEEL

STEERING

SERVO CONTROL

STEERING

ACTUATING

CYLINDER

SHOCK

TORQUE

ABSORBER

LINK

TOWING

FITTING

N_AC_020900_1_0140101_01_00

Landing Gear

Nose Landing Gear (Sheet 1 of 2)

FIGURE-2-9-0-991-014-A01

Page 9

Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

LOCKSTAY

NLG DOOR

SAFETY PIN

DOWNLOCK

SAFETY PIN

DOOR HINGE

NLG DOOR

FLAG

RH SHOWN

LH SYMMETRICAL

TOWING LEVER

FILLING AND CHARGING

CONNECTION

NORMAL POSITION

(NOSE WHEEL STEERING

OPERATIONAL)

TOWING POSITION

(NOSE WHEEL STEERING DEACTIVATED)

SAFETY PIN

(TOWING POSITION)

N_AC_020900_1_0140102_01_01

Landing Gear

Nose Landing Gear (Sheet 2 of 2)

FIGURE-2-9-0-991-014-A01

Page 10

Dec 01/20

2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

Landing Gear Maintenance Pits

Description

The minimum maintenance pit envelopes for the landing-gear shock absorber removal are shown in

FIGURE 2-9-0-991-024-A and FIGURE 2-9-0-991-025-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

2-9-0-991-024-A and FIGURE 2-9-0-991-025-A.

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2-9-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

2-10-0

Exterior Lighting

**ON A/C A320-200 A320neo

Exterior Lighting

General

This section provides the location of the aircraft exterior lighting.

EXTERIOR LIGHTING

ITEM

DESCRIPTION

RIGHT NAVIGATION LIGHT (GREEN)

TAIL NAVIGATION LIGHT (WHITE)

LEFT NAVIGATION LIGHT (RED)

RETRACTABLE LANDING LIGHT

RUNWAY TURN OFF LIGHT

TAXI LIGHT

TAKE-OFF LIGHT

LOGO LIGHT

UPPER ANTI-COLLISION LIGHT/BEACON (RED)

LOWER ANTI-COLLISION LIGHT/BEACON (RED)

WING STROBE LIGHT (HIGH INTENSITY, WHITE)

TAIL STROBE LIGHT (HIGH INTENSITY, WHITE)

WING/ENGINE SCAN LIGHT

WHEEL WELL LIGHT (DOME)

CARGO COMPARTMENT FLOOD LIGHT

Page 1

Dec 01/20

2-10-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

WEATHER RADAR

EMERGENCY STATIC PROBE

AOA SENSOR(3) STBY

ATC(4)

VHF(1)

GPS(2)

AOA SENSOR(1)

VHF(3)

GPS(1)

ELT

TCAS TOP

LOC

GLIDE

RADIO ALTIMETER(2)

DME(1)

TAT PROBE

MARKER

RADIO ALTIMETER(1)

PITOT PROBE(3)

TCAS BOTTOM

VHF(2)

PITOT PROBE(1)

ATC(1)

DME(2)

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_0030101_01_00

Antennas and Probes

Location

FIGURE-2-11-0-991-003-A01

Page 2

Dec 01/20

2-11-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

2-12-0

Power Plant

**ON A/C A320-200 A320neo

Auxiliary Power Unit

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.

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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2-12-0

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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

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

NOTE:

LH ACCESS DOOR 315AL NOT SHOWN FOR CLARITY.

N_AC_021200_1_0050101_01_01

Auxiliary Power Unit

Access Doors

FIGURE-2-12-0-991-005-A01

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Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

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

N_AC_021200_1_0060101_01_01

Auxiliary Power Unit

General Layout

FIGURE-2-12-0-991-006-A01

Page 3

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200 A320neo

Engine and Nacelle

**ON A/C A320-200

Engine and Nacelle - CFM Engine

Engine

The engine is a dual-rotor, variable stator, high bypass ratio turbofan powerplant 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.

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.

Engine and Nacelle - IAE Engine

A. Engine

The engine is a two spool, axial flow, high bypass ratio turbofan powerplant for subsonic service.

The main modules of the engine are:

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2-12-0

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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.

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

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

2 943 mm

(115.87 in)

2 600 mm

(102.36 in)

1 125 mm

TURBINE

(44.28 in)

COMPRESSOR

FRAME

FAN AND BOOSTER

FWD HOISTING

COMBUSTOR

POINT

FWD

HANDLING

POINT

1 820 mm

TURBINE

(71.65 in)

AFT HANDLING

AND HANDLING

AGB

TGB

POINT

ACCESSORY

DIA 986 mm

DRIVE

(38.82 in)

2 145 mm

(84.45 in)

FWD

1 130 mm

(44.49 in)

989 mm

(38.94 in)

1 978 mm

(77.87 in)

N_AC_021200_1_0270101_01_00

Power Plant Handling

Major Dimensions - CFM56 Series Engine

FIGURE-2-12-0-991-027-A01

Page 6

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2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

DISTANCE FROM

0.33 m

THE NOSE

(1.1 ft)

11 m

0.93 m

1.3 m

1.2 m

(36.1 ft)

(3.1 ft)

(4.3 ft)

(3.9 ft)

PRIMARY

NOZZLE

2.3 m

1.6 m

(7.5 ft)

(5.2 ft)

CENTERBODY

2.1 m

(6.9 ft)

ENGINE AIR

0.57 m

INLET COWL

FAN COWL

(1.9 ft)

FAN

REVERSER

A A

1.9 m

2.07 m

1.8 m

(6.2 ft)

(6.8 ft)

(5.9 ft)

1.2 m

(3.9 ft)

BLOCKER DOOR

EXTENDED

B B

C C

D D

N_AC_021200_1_0280101_01_00

Power Plant Handling

Major Dimensions - CFM56 Series Engine

FIGURE-2-12-0-991-028-A01

Page 7

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

4.25 m

(14 ft)

3.73 m

(12.3 ft)

1.85 m

(6.1 ft)

1.51 m

(4.98 ft)

40?

55?

0.81 m

1.2 m

SEE

(2.67 ft)

(3.96 ft)

CHAPTER

2−3

NOTE: APPROXIMATE DIMENSIONS.

N_AC_021200_1_0290101_01_01

Power Plant Handling

Fan Cowls - CFM56 Series Engine

FIGURE-2-12-0-991-029-A01

Page 8

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

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

SEE

(3.3 ft)

45?

(2.3 ft)

CHAPTER

2−3

GROUND

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.

NOTE: APPROXIMATE DIMENSIONS.

N_AC_021200_1_0300101_01_01

Power Plant Handling

Thrust Reverser Cowls - CFM56 Series Engine

FIGURE-2-12-0-991-030-A01

Page 9

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

3 101 mm

(122.1 in)

TURBINE

FRAME

TURBINE

COMBUSTOR

FAN AND BOOSTER

COMPRESSOR

TURBINE

1 715 mm

(67.5 in)

1 067 mm

(42.0 in)

ACCESSORY

DRIVE

FWD

N_AC_021200_1_0310101_01_00

Power Plant Handling

Major Dimensions - IAE V2500 Series Engine

FIGURE-2-12-0-991-031-A01

Page 10

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

DISTANCE FROM

THE NOSE

11.12 m

5.25 m

(36.5 ft)

(17.23 ft)

0.5?

1.50 m

(4.95 ft)

5.26 m

(17.27 ft)

PPS

COMPONENT

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

TECH 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

N_AC_021200_1_0320101_01_00

Power Plant Handling

Major Dimensions - IAE V2500 Series Engine

FIGURE-2-12-0-991-032-A01

Page 11

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

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)

SEE

CHAPTER

2−3

GROUND

NOTE: APPROXIMATE DIMENSIONS.

N_AC_021200_1_0330101_01_01

Power Plant Handling

Fan Cowls - IAE V2500 Series Engine

FIGURE-2-12-0-991-033-A01

Page 12

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320-200

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)

SEE

CHAPTER

2−3

NOTE: APPROXIMATE DIMENSIONS.

N_AC_021200_1_0340101_01_01

Power Plant Handling

Thrust Reverser Halves - IAE V2500 Series Engine

FIGURE-2-12-0-991-034-A01

Page 13

Dec 01/20

2-12-0

@A320

AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

**ON A/C A320neo

FAN COWL THRUST

NOSE COWL

REVERSER

PRIMARY

NOZZLE

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)

SEE

CHAPTER

2−3

N_AC_021200_1_0460101_01_01

Power Plant Handling

Major Dimensions - PW 1100G Engine

FIGURE-2-12-0-991-046-A01

Page 14

Dec 01/20

2-12-0

Airbus A320. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016-2023) - page 10