Airbus A320. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016-2023) - page 14
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
10
BREAKAWAY RESISTANCE 4%
# OF ENGINES ON FOR PB: 1
ENGINE THRUST 825 daN FOR
ALL TEMPERATURES AND SLS
AND ECS NOMINAL
75
80
1.5% SLOPE
75
70
65
1 ENGINE ON
60
5
55
5.0
50
8.71
0
0
10
20
30
40
50
60
70
80
0
1
2
0
0.5
1.0
1.5
2.0
TOTAL TRACTION WHEEL LOAD (x 1 000 kg)
No. OF ENGINES
SLOPE ( % )
AT IDLE
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A320 AT 75 000 kg, AT 1.5% SLOPE,
1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
−
ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (75 000 kg),
−
FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),
−
FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 2,
−
FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED No. OF ENGINES (1),
−
FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,
−
THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5 000 kg),
− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE.
THE OBTAINED X−COORDINATE IS THE TOTAL TRACTION WHEEL LOAD (8 710 kg).
NOTE:
USE A TRACTOR WITH A LIMITED DRAWBAR PULL TO PREVENT LOADS ABOVE THE TOW−BAR SHEAR−PIN
CAPACITY.
N_AC_050800_1_0010502_01_00
Ground Towing Requirements
CFM LEAP-1A Engine (Sheet 2 of 2)
FIGURE-5-8-0-991-001-E01
Page 4
Dec 01/20
5-8-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0
De-Icing and External Cleaning
**ON A/C A320-200 A320neo
De-Icing and External Cleaning
1.
De-Icing and External Cleaning on Ground
The mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heights
up to approximately 13 m (43 ft).
2.
De-Icing
Wingtip Devices
Wing Top Surface
(Both Inside and
HTP Top Surface
VTP
AIRCRAFT TYPE
(Both Sides)
Outside Surfaces)
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
m2
ft2
A320
100
1 076
2
22
27
291
43
463
A320 Sharklet/neo
100
1 076
10
108
27
291
43
463
Nacelle and Pylon
Fuselage Top Surface
(Top Third - 120˚ Arc)
Total De-Iced Area
AIRCRAFT TYPE
(Top Third - 120˚ Arc)
(All Engines)
m2
ft2
m2
ft2
m2
ft2
A320
138
1 485
24
258
333
3 584
A320 Sharklet/neo
138
1 485
24
258
341
3 670
NOTE : Dimensions are approximate.
3.
External Cleaning
Wing Lower Surface
Wingtip Devices
Wing Top Surface
(Including Flap Track
(Both Inside and
AIRCRAFT TYPE
(Both Sides)
Fairing)
Outside Surfaces)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A320
100
1 076
103
1 109
2
22
A320 Sharklet/neo
100
1 076
103
1 109
10
108
HTP Top Surface
HTP Lower Surface
VTP
AIRCRAFT TYPE
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A320
27
291
27
291
43
463
Page 1
Dec 01/20
5-9-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HTP Top Surface
HTP Lower Surface
VTP
AIRCRAFT TYPE
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A320 Sharklet/neo
27
291
27
291
43
463
Fuselage and
Nacelle and Pylon
Total Cleaned Area
AIRCRAFT TYPE
Belly Fairing
(All Engines)
m2
ft2
m2
ft2
m2
ft2
A320
421
4 532
73
786
796
8 568
A320 Sharklet/neo
421
4 532
73
786
804
8 654
NOTE : Dimensions are approximate.
Page 2
Dec 01/20
5-9-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0
Engine Exhaust Velocities and Temperatures
**ON A/C A320-200 A320neo
Engine Exhaust Velocities and Temperatures
**ON A/C A320-200
1.
General
This section provides the estimated engine exhaust efflux velocities and temperatures contours for
Ground Idle, Breakaway and Maximum Take-Off (MTO) conditions.
**ON A/C A320neo
2.
General
This section provides the estimated engine exhaust velocity and temperature contours for MTO,
Breakaway 12% MTO, Breakaway 24% MTO and Ground Idle conditions for the CFM LEAP-1A and
PW 1100G engines.
The MTO data are presented at the maximum thrust rating. The Breakaway data are presented at a
rating that corresponds to the minimum thrust level necessary to start the movement of the A/C
from a static position at its maximum ramp weight. Breakaway thrust corresponds to 12% MTO if
applied on both engines and 24% MTO when applied on a single engine (Idle thrust on the other
engine).
The Idle data, provided by the engine manufacturer, are calculated for operational conditions ISA
+15K (+15˚C), Sea Level, Static and no headwind. In the charts, the longitudinal distances are
measured from the inboard engine core-nozzle exit section. The lateral distances are measured from
the aircraft fuselage centerline.
The effects of on-wing installation are not taken into account. The effects of ground proximity are
not taken into account for PW 1100G engines, but they are taken into account for the CFM
LEAP-1A engines.
The velocity contours are presented at 50 ft/s (15 m/s), 100 ft/s (30 m/s) and 150 ft/s (46 m/s).
The temperature contours are shown at 313K (+40˚C), 323K (+50˚C) and 333K (+60˚C). The
velocity and temperature contours do not take into account possible variations affecting performance,
such as ambient temperature, field elevation or failure cases leading to an abnormal bleed
configuration. To evaluate the impact of these specific variables on the exhaust contours, a specific
study of the airport where the aircraft is intended to operate should be carried out.
Page 1
Dec 01/20
6-1-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A320-200 A320neo
Engine Exhaust Velocities Contours - Ground Idle Power
1.
This section provides engine exhaust velocities contours at ground idle power.
Page 1
Dec 01/20
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060101_1_0050101_01_01
Engine Exhaust Velocities
Ground Idle Power -- CFM56 Series Engine
FIGURE-6-1-1-991-005-A01
Page 2
Dec 01/20
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060101_1_0060101_01_00
Engine Exhaust Velocities
Ground Idle Power -- IAE V2500 Series Engine
FIGURE-6-1-1-991-006-A01
Page 3
Dec 01/20
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060101_1_0110101_01_00
Engine Exhaust Velocities
Ground Idle Power -- CFM LEAP-1A Engine
FIGURE-6-1-1-991-011-A01
Page 4
Dec 01/20
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060101_1_0120101_01_00
Engine Exhaust Velocities
Ground Idle Power -- PW 1100G Engine
FIGURE-6-1-1-991-012-A01
Page 5
Dec 01/20
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A320-200 A320neo
Engine Exhaust Temperatures Contours - Ground Idle Power
1.
This section provides engine exhaust temperatures contours at ground idle power.
Page 1
Dec 01/20
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060102_1_0050101_01_01
Engine Exhaust Temperatures
Ground Idle Power -- CFM56 Series Engine
FIGURE-6-1-2-991-005-A01
Page 2
Dec 01/20
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060102_1_0060101_01_01
Engine Exhaust Temperatures
Ground Idle Power -- IAE V2500 Series Engine
FIGURE-6-1-2-991-006-A01
Page 3
Dec 01/20
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060102_1_0110101_01_00
Engine Exhaust Temperatures
Ground Idle Power -- CFM LEAP-1A Engine
FIGURE-6-1-2-991-011-A01
Page 4
Dec 01/20
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060102_1_0120101_01_00
Engine Exhaust Temperatures
Ground Idle Power -- PW 1100G Engine
FIGURE-6-1-2-991-012-A01
Page 5
Dec 01/20
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A320-200 A320neo
Engine Exhaust Velocities Contours - Breakaway Power
1.
This section provides engine exhaust velocities contours at breakaway power.
Page 1
Dec 01/20
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060103_1_0030101_01_01
Engine Exhaust Velocities
Breakaway Power -- CFM56 Series Engine
FIGURE-6-1-3-991-003-A01
Page 2
Dec 01/20
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060103_1_0040101_01_00
Engine Exhaust Velocities
Breakaway Power -- IAE V2500 Series Engine
FIGURE-6-1-3-991-004-A01
Page 3
Dec 01/20
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0130101_01_00
Engine Exhaust Velocities
Breakaway Power 12% MTO -- CFM LEAP-1A Engine
FIGURE-6-1-3-991-013-A01
Page 4
Dec 01/20
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0140101_01_00
Engine Exhaust Velocities
Breakaway Power 12% MTO -- PW 1100G Engine
FIGURE-6-1-3-991-014-A01
Page 5
Dec 01/20
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0150101_01_00
Engine Exhaust Velocities
Breakaway Power 24% MTO -- CFM LEAP-1A Engine
FIGURE-6-1-3-991-015-A01
Page 6
Dec 01/20
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0160101_01_00
Engine Exhaust Velocities
Breakaway Power 24% MTO -- PW 1100G Engine
FIGURE-6-1-3-991-016-A01
Page 7
Dec 01/20
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A320-200 A320neo
Engine Exhaust Temperatures Contours - Breakaway Power
1.
This section provides engine exhaust temperatures contours at breakaway power.
Page 1
Dec 01/20
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060104_1_0030101_01_01
Engine Exhaust Temperatures
Breakaway Power -- CFM56 Series Engine
FIGURE-6-1-4-991-003-A01
Page 2
Dec 01/20
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060104_1_0040101_01_01
Engine Exhaust Temperatures
Breakaway Power -- IAE V2500 Series Engine
FIGURE-6-1-4-991-004-A01
Page 3
Dec 01/20
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0090101_01_00
Engine Exhaust Temperatures
Breakaway Power 12% MTO - CFM LEAP-1A Engine
FIGURE-6-1-4-991-009-A01
Page 4
Dec 01/20
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0100101_01_00
Engine Exhaust Temperatures
Breakaway Power 12% MTO - PW 1100G Engine
FIGURE-6-1-4-991-010-A01
Page 5
Dec 01/20
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0110101_01_00
Engine Exhaust Temperatures
Breakaway Power 24% MTO - CFM LEAP-1A Engine
FIGURE-6-1-4-991-011-A01
Page 6
Dec 01/20
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0120101_01_00
Engine Exhaust Temperatures
Breakaway Power 24% MTO - PW 1100G Engine
FIGURE-6-1-4-991-012-A01
Page 7
Dec 01/20
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5
Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A320-200 A320neo
Engine Exhaust Velocities Contours - Takeoff Power
1.
This section provides engine exhaust velocities contours at takeoff power.
Page 1
Dec 01/20
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060105_1_0050101_01_01
Engine Exhaust Velocities
Takeoff Power -- CFM56 Series Engine
FIGURE-6-1-5-991-005-A01
Page 2
Dec 01/20
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060105_1_0060101_01_01
Engine Exhaust Velocities
Takeoff Power -- IAE V2500 Series Engine
FIGURE-6-1-5-991-006-A01
Page 3
Dec 01/20
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060105_1_0110101_01_00
Engine Exhaust Velocities
Takeoff Power -- CFM LEAP-1A Engine
FIGURE-6-1-5-991-011-A01
Page 4
Dec 01/20
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060105_1_0120101_01_00
Engine Exhaust Velocities
Takeoff Power -- PW 1100G Engine
FIGURE-6-1-5-991-012-A01
Page 5
Dec 01/20
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A320-200 A320neo
Engine Exhaust Temperatures Contours - Takeoff Power
1.
This section provides engine exhaust temperatures contours at takeoff power.
Page 1
Dec 01/20
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060106_1_0050101_01_01
Engine Exhaust Temperatures
Takeoff Power -- CFM56 Series Engine
FIGURE-6-1-6-991-005-A01
Page 2
Dec 01/20
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060106_1_0060101_01_00
Engine Exhaust Temperatures
Takeoff Power -- IAE V2500 Series Engine
FIGURE-6-1-6-991-006-A01
Page 3
Dec 01/20
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060106_1_0110101_01_00
Engine Exhaust Temperatures
Takeoff Power - CFM LEAP-1A Engine
FIGURE-6-1-6-991-011-A01
Page 4
Dec 01/20
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060106_1_0120101_01_00
Engine Exhaust Temperatures
Takeoff Power - PW 1100G Engine
FIGURE-6-1-6-991-012-A01
Page 5
Dec 01/20
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0
Danger Areas of Engines
**ON A/C A320-200 A320neo
Danger Areas of Engines
1.
Danger Areas of the Engines
A. The danger areas of the engines shown below are given in the normalized format:
-
Entry corridors are only available at ground idle.
-
Do not go into the areas between the engines.
-
The exhaust danger areas are given for 0 kt headwind (if not specified otherwise).
Page 1
Dec 01/20
6-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1
Ground Idle Power
**ON A/C A320-200 A320neo
Ground Idle Power
1.
This section provides danger areas of the engines at ground idle power conditions.
Page 1
Dec 01/20
6-3-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
R = 2.23 m
1 m
(3.3 ft)
(7.3 ft)
30?
TO 55 m (180 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) INCLUDES CROSS WIND EFFECT
NOTE:
INLET SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST WAKE DANGER AREA
N_AC_060301_1_0050101_01_04
Danger Areas of the Engines
CFM56 Series Engine
FIGURE-6-3-1-991-005-A01
Page 2
Dec 01/20
6-3-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
R = 2.74m
0.91 m
(3 ft)
(9 ft)
30?
TO 55 m (180 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) INCLUDES CROSS WIND EFFECT
NOTE:
INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060301_1_0060101_01_04
Danger Areas of the Engines
IAE V2500 Series Engine
FIGURE-6-3-1-991-006-A01
Page 3
Dec 01/20
6-3-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
R = 2.9 m
1 m
(9.5 ft)
(3.3 ft)
30?
TO 38.7 m (127 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
INCLUDES CROSS WIND EFFECT
NOTE:
INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060301_1_0130101_01_02
Danger Areas of the Engines
CFM LEAP-1A Engine
FIGURE-6-3-1-991-013-A01
Page 4
Dec 01/20
6-3-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
R = 2.74 m
1 m
(3.3 ft)
(9 ft)
30?
TO 40.3 m (132 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) INCLUDES CROSS WIND EFFECT
NOTE:
INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060301_1_0140101_01_02
Danger Areas of the Engines
PW 1100G Engine
FIGURE-6-3-1-991-014-A01
Page 5
Dec 01/20
6-3-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2
Breakaway Power
**ON A/C A320-200 A320neo
Breakaway Power
1.
This section provides danger areas of the engines at breakaway power.
Page 1
Dec 01/20
6-3-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
R = 5.2 m
1.6 m
(17.1 ft)
(5.2 ft)
30?
TO 74.7 m (245 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
INCLUDES CROSS WIND EFFECT
NOTE:
INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER
EXHAUST WAKE DANGER AREA
N_AC_060302_1_0050101_01_03
Danger Areas of the Engines
CFM56 Series Engine
FIGURE-6-3-2-991-005-A01
Page 2
Dec 01/20
6-3-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
R = 5 m
(16.4 ft)
1.2 m
(3.9 ft)
30?
TO 91.4 m (300 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) INCLUDES CROSS WIND EFFECT
NOTE:
INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER
EXHAUST DANGER AREA
N_AC_060302_1_0060101_01_03
Danger Areas of the Engines
IAE V2500 Series Engine
FIGURE-6-3-2-991-006-A01
Page 3
Dec 01/20
6-3-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
R = 3.8 m
(12.5 ft)
1.1 m
(3.6 ft)
30?
TO 63.5 m (208 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) INCLUDES CROSS WIND EFFECT
NOTE:
INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER
EXHAUST DANGER AREA
N_AC_060302_1_0110101_01_02
Danger Areas of the Engines
CFM LEAP-1A Engine
FIGURE-6-3-2-991-011-A01
Page 4
Dec 01/20
6-3-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
R = 3.7 m
(12.1 ft)
1.9 m
(6.2 ft)
30?
TO 71.6 m (235 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA) INCLUDES CROSS WIND EFFECT
NOTE:
INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER
EXHAUST DANGER AREA
N_AC_060302_1_0120101_01_02
Danger Areas of the Engines
PW 1100G Engine
FIGURE-6-3-2-991-012-A01
Page 5
Dec 01/20
6-3-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-3
Max Take Off Power
**ON A/C A320-200 A320neo
Take Off Power
1.
This section provides danger areas of the engines at maximum take-off power conditions.
Page 1
Dec 01/20
6-3-3