Airbus A321. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016) - page 2
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
20
40
60
80
PERMISSIBLE WIND SPEED (km/h)
30
50
70
80
45
40
AIRCRAFT CG (%RC)
35
30
25
20
15
10
5
B
0
70
80
75
C
60
70
A
65
50
60
D
55
40
50
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 67 500 kg A AND CENTER OF GRAVITY
AT 23 % RC B . THE REACTION AT THE WING JACKING POINTS IS 62 750 kg
(31 375 kg PER SIDE)
C
AND THE REACTION AT THE FORWARD FUSELAGE
JACKING POINT IS 4 750 kg D . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE THE WIND
SPEED MUST NOT BE IN EXCESS OF 70 km/h.
N_AC_021400_1_0430101_01_00
Loads at the Aircraft Jacking Points
Wing Jacking Point and Forward Fuselage Jacking Point
FIGURE-2-14-0-991-043-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FR73 / FR74
(SAFETY STAY)
FR60
FR56
RIB4
RIB4
RIB22
RIB22
RIB13
RIB13
FR34
FR29
FR9
NOTE: THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
N_AC_021400_1_0440101_01_00
Jacking for Maintenance
Location of Shoring Cradles
FIGURE-2-14-0-991-044-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
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.
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
1 270 x 455 R22
600 mm
(23.62 in)
FULLY
EXTENDED
49 x 18 R22
200 mm
205 mm
25 mm
38 mm
563 mm
(7.87 in)
(8.07 in)
(1 in)
(1.5 in)
(22.17 in)
FULLY
DIA. BALL
RETRACTED
186 mm
INFLATED TIRES
(7.32 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_0240101_01_00
Jacking of the Landing Gear
MLG Jacking Point Location - Twin Wheels
FIGURE-2-14-0-991-024-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
655 mm
(25.79 in)
MLG TIRE 1 270 x 455−R22
CANTILEVER
ARM
563 mm
(22.17 in)
25 mm
FWD
(1 in)
TWIN WHEEL TRACK
927 mm
(36.5 in)
DOUBLE FLAT MLG TIRES
205 mm (8.07 in)
(186 mm (7.32 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_0250101_01_00
Jacking of the Landing Gear
MLG Jacking with Cantilever Jack - Twin Wheels
FIGURE-2-14-0-991-025-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
LOAD AT MLG
JACKING POINT
(x 1 000 kg)
CG POSITION
45
CG 40%
CG 30%
CG 25%
CG 20%
40
CG 17%
35
30
25
20
15
AIRCRAFT WEIGHT
10
30
40
50
60
70
80
90
x 1 000 kg
70
80
90
100
110
120
130
140
150
160
170
180
190
200
x 1 000 lb
N_AC_021400_1_0260101_01_00
Jacking of the Landing Gear
Loads at MLG Jacking Points
FIGURE-2-14-0-991-026-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
LOAD AT MLG
JACKING POINT
(x 1 000 kg)
CG POSITION
50
45
CG 38.0%
CG 25.0%
40
CG 17.5%
35
30
25
20
15
AIRCRAFT WEIGHT
10
40
50
60
70
80
90
x 1 000 kg
90
100
110
120
130
140
150
160
170
180
190
200
x 1 000 lb
N_AC_021400_1_0270101_01_00
Jacking of the Landing Gear
Loads at MLG Jacking Points
FIGURE-2-14-0-991-027-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
40 mm
128 mm
25 mm
38 mm
326 mm
APPROX
(1.57 in)
(5.07 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_0280101_01_00
Jacking of the Landing Gear
NLG Jacking - Point Location
FIGURE-2-14-0-991-028-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
LOAD AT
JACKING POINT
(x 1 000 kg)
CG POSITION
10
CG 17.5%
9
8
CG 25.0%
7
6
5
CG 38.0%
4
3
2
1
AIRCRAFT WEIGHT
0
40
50
60
70
80
90
x 1 000 kg
90
100
110
120
130
140
150
160
170
180
190
200
x 1 000 lb
N_AC_021400_1_0290101_01_00
Jacking of the Landing Gear
Loads at NLG Jacking Points
FIGURE-2-14-0-991-029-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0
General Information
**ON A/C A321-100 A321-200 A321neo
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
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3-1-0
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1
Payload / Range - ISA Conditions
**ON A/C A321-100 A321-200 A321neo
Payload/Range - ISA Conditions
1.
This section provides the payload/range at ISA conditions.
Page 1
May 01/16
3-2-1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_030201_1_0190101_01_00
Payload/Range - ISA Conditions
FIGURE-3-2-1-991-019-A01
Page 2
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3-2-1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_030201_1_0200101_01_00
Payload/Range - ISA Conditions
Sharklet
FIGURE-3-2-1-991-020-A01
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3-2-1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321neo
N_AC_030201_1_0210101_01_00
Payload/Range - ISA Conditions
FIGURE-3-2-1-991-021-A01
Page 4
May 01/16
3-2-1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1
Take-off Weight Limitation - ISA Conditions
**ON A/C A321-100 A321-200
Take-Off Weight Limitation - ISA Conditions
1.
This section gives the take-off weight limitation at ISA conditions.
Page 1
May 01/16
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
0
2
210
4
200
90
6
190
180
8
80
170
160
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_0070101_01_00
Take-Off Weight Limitation - ISA Conditions
CFM56 Series Engine
FIGURE-3-3-1-991-007-A01
Page 2
May 01/16
3-3-1
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
0
2
210
4
200
90
190
6
180
80
8
170
160
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_0080101_01_00
Take-Off Weight Limitation - ISA Conditions
IAE V2500 Series Engine
FIGURE-3-3-1-991-008-A01
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3-3-1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2
Take-off Weight Limitation - ISA +15˚C (+59˚F) Conditions
**ON A/C A321-100 A321-200
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
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3-3-2
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
0
2
210
4
200
90
190
6
180
8
80
170
160
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_0070101_01_00
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
CFM56 Series Engine
FIGURE-3-3-2-991-007-A01
Page 2
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3-3-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
0
2
210
90
200
4
190
6
180
80
8
170
160
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_0080101_01_00
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
IAE V2500 Series Engine
FIGURE-3-3-2-991-008-A01
Page 3
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3-3-2
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1
Landing Field Length - ISA Conditions
**ON A/C A321-100 A321-200
Landing Field Length - ISA Conditions
1.
This section provides the landing field length.
Page 1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
(x 1 000 m)
(x 1 000 ft)
9
ISA CONDITIONS
AIRFIELD ELEVATION
2.5
SLATS 27 DEG.
(x 1 000 ft)
FLAPS 40 DEG.
8
7
10
8
6
4
2
2.0
SEA
LEVEL
6
5
1.5
4
1.0
3
80
100
120
140
160
180
200
GROSS WEIGHT (x 1 000 lb)
30
40
50
60
70
80
90
GROSS WEIGHT (x 1 000 kg)
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_0070101_01_01
Landing Field Length - ISA Conditions
CFM56 Series Engine
FIGURE-3-4-1-991-007-A01
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3-4-1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
(x 1 000 m)
(x 1 000 ft)
9
ISA CONDITIONS
AIRFIELD ELEVATION
2.5
SLATS 27 DEG.
(x 1000 ft)
FLAPS 40 DEG.
8
7
10
8
6
4
2
2.0
SEA
LEVEL
6
5
1.5
4
1.0
3
80
100
120
140
160
180
200
GROSS WEIGHT (x 1 000 lb)
30
40
50
60
70
80
90
GROSS WEIGHT (x 1 000 kg)
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_0080101_01_01
Landing Field Length - ISA Conditions
IAE V2500 Series Engine
FIGURE-3-4-1-991-008-A01
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3-4-1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0
Final Approach Speed
**ON A/C A321-100 A321-200
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 140 kt at a MLW of 75 500 kg (166 449 lb) and classifies the aircraft
into the Aircraft Approach Category C.
NOTE : This value is given for information only.
3.
The final approach speed is 142 kt at a MLW of 77 800 kg (171 520 lb) and classifies the aircraft
into the Aircraft Approach Category D.
NOTE : This value is given for information only.
Page 1
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3-5-0
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0
General Information
**ON A/C A321-100 A321-200 A321neo
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
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4-1-0
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0
Turning Radii
**ON A/C A321-100 A321-200 A321neo
Turning Radii
1.
This section provides the turning radii.
Page 1
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4-2-0
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
R3
R1
R5
50°
60°
70°
7.59 m
(24.9 ft)
R2
R6
16.9 m
(55.45 ft)
R4
NOTE:
FOR STEERING DIMENSION TABLE SEE SHEET 2.
APPLICABLE FOR A321−100 AND A321−200.
TURN TYPE:
1. ASYMMETRIC THRUST DIFFERENTIAL BRAKING
(PIVOTTING ON ONE MAIN GEAR).
2. SYMMETRIC THRUST NO BRAKING.
N_AC_040200_1_0070101_01_02
Turning Radii, No Slip Angle
(Sheet 1)
FIGURE-4-2-0-991-007-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
N_AC_040200_1_0080101_01_01
Turning Radii, No Slip Angle
(Sheet 2)
FIGURE-4-2-0-991-008-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0
Minimum Turning Radii
**ON A/C A321-100 A321-200 A321neo
Minimum Turning Radii
1.
This section provides the minimum turning radii.
Page 1
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4-3-0
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
16.9 m
R4
(55 ft)
R6
R3
OUTSIDE FACE OF TIRE
Y
EFFECTIVE
TURN
STEERING
A
ANGLE 75°
MINIMUM
PAVEMENT
WIDTH FOR
180° TURN
R5
NOTE:
NOSE GEAR RADII TRACK
MEASURED FROM OUTSIDE FACE OF TIRE.
THEORETICAL CENTER OF TURN
FOR MINIMUM TURNING RADIUS.
SLOW CONTINUOUS TURNING,
APPROXIMATELY IDLE THRUST
ON ALL ENGINES.
NO DIFFERENTIAL BRAKING.
TYPE
STEERING
EFFECTIVE
R4 WING
R3
R5
R6
OF
ANGLE
STEERING
Y
A
NLG
WING TIP
NOSE
THS
SHARKLET
TURN
(DEG)
ANGLE
FENCE
m
5.1
27.7
17.8
22.6
23.4
22.6
24.5
1
75 (MAX)
73.1°
ft
17
91
58
74
77
74
80
m
5.6
28.3
17.9
23.1
23.9
22.7
24.7
2
75 (MAX)
71.6°
ft
18
93
59
76
78
74
81
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_0040101_01_02
Minimum Turning Radii
FIGURE-4-3-0-991-004-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0
Visibility from Cockpit in Static Position
**ON A/C A321-100 A321-200 A321neo
Visibility from Cockpit in Static Position
1.
This section gives the visibility from cockpit in static position.
Page 1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
NOT TO BE USED FOR
LANDING APPROACH VISIBILITY
DIMENSIONS ARE APPROXIMATE
30°
VISUAL ANGLES IN VERTICAL
20°
PLANE THROUGH PILOT
EYE POSITION.
2.41 m
4.56 m
(7 ft 10.92 in)
(14 ft 11.52 in)
5.07 m
10.14 m
(16 ft 7.56 in)
(33 ft 3.24 in)
MAX AFT VISION WITH HEAD TURNED
111°
AROUND SPINAL COLUMN.
WING TIP CAN BE SEEN WHEN HEAD IS MOVED
133°
TO THE SIDE.
FIRST OFFICER
FIELD OF VIEW
VISUAL ANGLES IN HORIZONTAL
PLANE THROUGH PILOT
EYE POSITION.
CAPTAIN FIELD OF VIEW
111°
133°
WITH HEAD MOVED
125 mm (5 in) OUTBOARD
VISUAL ANGLES IN PLANE
0.53 m
PERPENDICULAR TO
(1 ft 8.88 in)
LONGITUDINAL AXIS.
46°
46°
33°
33°
25°
25°
32°
32°
ZONE THAT CANNOT BE SEEN
NOTE:
PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
N_AC_040400_1_0010101_01_03
Visibility from Cockpit in Static Position
FIGURE-4-4-0-991-001-A01
Page 2
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
N_AC_040400_1_0050101_01_00
Binocular Visibility Through Windows from Captain Eye Position
FIGURE-4-4-0-991-005-A01
Page 3
May 01/16
4-4-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0
Runway and Taxiway Turn Paths
**ON A/C A321-100 A321-200 A321neo
Runway and Taxiway Turn Paths
1.
Runway and Taxiway Turn Paths.
Page 1
May 01/16
4-5-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1
135˚ Turn - Runway to Taxiway
**ON A/C A321-100 A321-200 A321neo
135˚ Turn - Runway to Taxiway
1.
This section gives the 135˚ turn - runway to taxiway.
Page 1
May 01/16
4-5-1
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
ADDITIONAL FILLET TO MEET
3 m (10 ft) EDGE CLEARANCE
APPROX 1.9 m
(6 ft)
FILLET R = 16.5 m
TAXIWAY
(55 ft)
CENTERLINE
TURN R = 30 m
(100 ft)
RUNWAY CENTERLINE
15 m
(50 ft)
NLG PATH
30 m
(100 ft)
MLG PATH
NOTE: FAA GROUP III FACILITIES.
N_AC_040501_1_0060101_01_02
135˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-1-991-006-A01
Page 2
May 01/16
4-5-1
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
APPROX 3 m
(10 ft)
FILLET R = 16.5 m
TAXIWAY
(55 ft)
CENTERLINE
TURN R = 30 m
(100 ft)
RUNWAY CENTERLINE
15 m
(50 ft)
NLG PATH
30 m
(100 ft)
MLG PATH
NOTE: FAA GROUP III FACILITIES.
N_AC_040501_1_0070101_01_02
135˚ Turn - Runway to Taxiway
Judgemental Oversteering Method
FIGURE-4-5-1-991-007-A01
Page 3
May 01/16
4-5-1
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2
90˚ Turn - Runway to Taxiway
**ON A/C A321-100 A321-200 A321neo
90˚ Turn - Runway to Taxiway
1.
This section gives the 90˚ turn - runway to taxiway.
Page 1
May 01/16
4-5-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 3.7 m
(12 ft)
TAXIWAY CENTERLINE
FILLET R = 16.5 m
(55 ft)
TURN R = 30 m
(100 ft)
NLG PATH
RUNWAY CENTERLINE
MLG PATH
30 m
(100 ft)
NOTE: FAA GROUP III FACILITIES.
N_AC_040502_1_0060101_01_02
90˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-2-991-006-A01
Page 2
May 01/16
4-5-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 9.2 m
(30 ft)
TAXIWAY CENTERLINE
FILLET R = 16.5 m
(55 ft)
TURN R = 30 m
(100 ft)
NLG PATH
RUNWAY CENTERLINE
MLG PATH
30 m
(100 ft)
NOTE: FAA GROUP III FACILITIES.
N_AC_040502_1_0070101_01_02
90˚ Turn - Runway to Taxiway
Judgemental Oversteering Method
FIGURE-4-5-2-991-007-A01
Page 3
May 01/16
4-5-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3
180˚ Turn on a Runway
**ON A/C A321-100 A321-200 A321neo
180˚ Turn on a Runway
1.
This section provides the 180˚ turn on a runway.
Page 1
May 01/16
4-5-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
RUNWAY CENTERLINE
14.9 m
3.45 m
(49 ft)
(11 ft)
R5 = 22.6 m
(74 ft)
R3 = 17.6 m
(58 ft)
R4
NLG PATH
WINGTIP PATH:
WINGTIP FENCES:
R4 = 22.7 m (74 ft)
SHARKLETS:
R4 = 23.4 m (77 ft)
NOSE PATH
MLG PATH
45 m
(150 ft)
NOTE:
TYPE 1 VALUES.
N_AC_040503_1_0020101_01_03
180˚ Turn on a Runway
Edge of Runway Method (Sheet 1 of 2)
FIGURE-4-5-3-991-002-A01
Page 2
May 01/16
4-5-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
RUNWAY CENTERLINE
4.4 m
(14 ft)
R5 = 22.6 m
(74 ft)
R4
R3 = 17.6 m
(58 ft)
6.3 m
(21 ft)
12 m
(39 ft)
NLG PATH
WINGTIP PATH:
WINGTIP FENCES:
R4 = 22.7 m (74 ft)
25°
SHARKLETS:
R4 = 23.4 m (77 ft)
NOSE PATH
MLG PATH
45 m
(150 ft)
NOTE:
TYPE 1 VALUES.
N_AC_040503_1_0020102_01_01
180˚ Turn on a Runway
Center of Runway Method (Sheet 2 of 2)
FIGURE-4-5-3-991-002-A01
Page 3
May 01/16
4-5-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4
135˚ Turn - Taxiway to Taxiway
**ON A/C A321-100 A321-200 A321neo
135˚ Turn - Taxiway to Taxiway
1.
This section gives the 135˚ turn - taxiway to taxiway.
Page 1
May 01/16
4-5-4
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
ADDITIONAL FILLET TO MEET
3 m (10 ft) EDGE CLEARANCE
APPROX 2.3 m
(8 ft)
FILLET R = 16.5 m
(55 ft)
TURN R = 30 m
(100 ft)
TAXIWAY CENTERLINE
15 m
TAXIWAY CENTERLINE
(50 ft)
15 m
NLG PATH
(50 ft)
MLG PATH
NOTE: FAA GROUP III FACILITIES
N_AC_040504_1_0070101_01_00
135˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-4-991-007-A01
Page 2
May 01/16
4-5-4
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
APPROX 3 m
(10 ft)
FILLET R = 16.5 m
(55 ft)
TURN R = 30 m
(100 ft)
TAXIWAY CENTERLINE
15 m
TAXIWAY CENTERLINE
(50 ft)
15 m
NLG PATH
(50 ft)
MLG PATH
NOTE: FAA GROUP III FACILITIES
N_AC_040504_1_0070102_01_00
135˚ Turn - Taxiway to Taxiway
Judgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-4-991-007-A01
Page 3
May 01/16
4-5-4
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5
90˚ Turn - Taxiway to Taxiway
**ON A/C A321-100 A321-200 A321neo
90˚ Turn - Taxiway to Taxiway
1.
This section gives the 90˚ turn - taxiway to taxiway.
Page 1
May 01/16
4-5-5
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 3.2 m
TAXIWAY CENTERLINE
(10 ft)
FILLET R = 16.5 m
(55 ft)
TURN R = 30 m
(100 ft)
NLG PATH
TAXIWAY CENTERLINE
MLG PATH
15 m
(50 ft)
NOTE: FAA GROUP III FACILITIES.
N_AC_040505_1_0040101_01_00
90˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-5-991-004-A01
Page 2
May 01/16
4-5-5
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 9.1 m
TAXIWAY CENTERLINE
(30 ft)
FILLET R = 16.5 m
(55 ft)
TURN R = 30 m
(100 ft)
NLG PATH
TAXIWAY CENTERLINE
MLG PATH
15 m
(50 ft)
NOTE: FAA GROUP III FACILITIES.
N_AC_040505_1_0040102_01_00
90˚ Turn - Taxiway to Taxiway
Judgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-5-991-004-A01
Page 3
May 01/16
4-5-5
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0
Runway Holding Bay (Apron)
**ON A/C A321-100 A321-200 A321neo
Runway Holding Bay (Apron)
1.
This section gives the runway holding bay (Apron).
Page 1
May 01/16
4-6-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
6.1 m
(20 ft)
90 m
61 m
(300 ft)
(200 ft)
12.2 m
(40 ft)
HOLDING POINT
6.1 m
(20 ft)
190 m
(625 ft)
TAXIWAY
CENTERLINE
RUNWAY CENTERLINE
23 m
45 m
(75 ft)
(150 ft)
NOTE: APPLICABLE FOR A321−100 AND A321−200.
N_AC_040600_1_0040101_01_02
Runway Holding Bay (Apron)
FIGURE-4-6-0-991-004-A01
Page 2
May 01/16
4-6-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0
Minimum Line-Up Distance Corrections
**ON A/C A321-100 A321-200 A321neo
Minimum Line-Up Distance Corrections
1.
The ground maneuvers were performed using asymmetric thrust and differential braking only to
initiate the turn.
TODA: Take-Off Distance Available
ASDA: Acceleration-Stop Distance Available
2.
90˚ Turn on Runway Entry
This section gives the minimum line-up distance correction for a 90˚ turn on runway entry.
This maneuver consists in a 90˚ turn at minimum turn radius. It starts with the edge of the MLG at
a distance of 3 m (10 ft) from the taxiway edge, and finishes with the aircraft aligned on the
centerline of the runway, see FIGURE 4-7-0-991-020-A.
During the turn, all the clearances must meet the minimum value of 3 m (10 ft) for this category of
aircraft as recommended in ICAO Annex 14.
3.
180˚ Turn on Runway Turn Pad
This section gives the minimum line-up distance correction for a 180˚ turn on the runway turn pad.
This maneuver consists in a 180˚ turn at minimum turn radius on a runway turn pad with standard
ICAO geometry.
It starts with the edge of the MLG at a distance of 3 m (10 ft) from the pavement edge, and it
finishes with the aircraft aligned on the centerline of the runway, see FIGURE 4-7-0-991-021-A.
During the turn, all the clearances must meet the minimum value of 3 m (10 ft) for this category of
aircraft as recommended in ICAO Annex 14.
4.
180˚ Turn on Runway Width
This section gives the minimum line-up distance correction for a 180˚ turn on the runway width.
For this maneuver, the pavement width is considered to be the runway width, which is a frozen
parameter (30 m (100 ft), 45 m (150 ft) and 60 m (200 ft)).
As per the standard operating procedures for the ”180˚ turn on runway” (described in the Flight
Crew Operating Manual), the aircraft is initially angled with respect to the runway centerline when
starting the 180˚ turn, see FIGURE 4-7-0-991-022-A.
The value of this angle depends on the aircraft type and is mentioned in the FCOM.
During the turn, all the clearances must meet the minimum value of 3 m (10 ft) for this category of
aircraft as recommended in ICAO Annex 14.
Page 1
May 01/16
4-7-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
3 m
(10 ft)
TODA
ASDA
TAXIWAY
CENTERLINE
> 3 m
(10 ft)
RUNWAY
CENTERLINE
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
90° TURN ON RUNWAY ENTRY
30 m (100 ft)
45 m (150 ft)/60 m (200 ft)
WIDE RUNWAY
WIDE RUNWAY
MAX
AIRCRAFT
STEERING
MINIMUM LINE−UP
MINIMUM LINE−UP
TYPE
ANGLE
DISTANCE CORRECTION
DISTANCE CORRECTION
ON TODA
ON ASDA
ON TODA
ON ASDA
A321
75°
13.9 m
46 ft
30.8 m
101 ft
12.6 m
41 ft
29.5 m
97 ft
N_AC_040700_1_0200101_01_00
Minimum Line-Up Distance Corrections
90˚ Turn on Runway Entry
FIGURE-4-7-0-991-020-A01
Page 2
May 01/16
4-7-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
MINIMUM PAVEMENT WIDTH
3 m
(10 ft)
> 3 m
(10 ft)
3 m
TODA
(10 ft)
ASDA
RUNWAY CENTERLINE
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
180° TURN ON RUNWAY TURN PAD
30 m (100 ft)
45 m (150 ft)/60 m (200 ft)
WIDE RUNWAY
WIDE RUNWAY
MAX
AIRCRAFT
MINIMUM LINE−UP
MINIMUM LINE−UP
STEERING
REQUIRED
REQUIRED
DISTANCE
DISTANCE
TYPE
ANGLE
MINIMUM
MINIMUM
CORRECTION
PAVEMENT
CORRECTION
PAVEMENT
WIDTH
WIDTH
ON TODA
ON ASDA
ON TODA
ON ASDA
A321
75°
21.4 m
70 ft
38.3 m
126 ft
35.3 m
116 ft
21 m
69 ft
37.9 m
124 ft
40.3 m
132 ft
N_AC_040700_1_0210101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Turn Pad
FIGURE-4-7-0-991-021-A01
Page 3
May 01/16
4-7-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
3 m
(10 ft)
3 m
(10 ft)
TODA
ASDA
> 3 m
(10 ft)
RUNWAY CENTERLINE
20°
ASDA: ACCELERATION−STOP DISTANCE AVAILABLE
TODA: TAKE−OFF DISTANCE AVAILABLE
180° TURN ON RUNWAY WIDTH
30 m (100 ft)
45 m (150 ft)/60 m (200 ft)
WIDE RUNWAY
WIDE RUNWAY
MAX
AIRCRAFT
STEERING
MINIMUM LINE−UP
MINIMUM LINE−UP
TYPE
ANGLE
DISTANCE CORRECTION
DISTANCE CORRECTION
ON TODA
ON ASDA
ON TODA
ON ASDA
A321
75°
NOT POSSIBLE
21.0 m
69 ft
37.9 m
124 ft
NOTE:
"NOT POSSIBLE" MEANS THAT IT IS NOT POSSIBLE FOR THE AIRCRAFT TO TURN ON SUCH A RUNWAY
WIDTH WITH THE GIVEN ASSUMPTIONS DEFINED IN THIS SECTION (4−7−0) WHILE MAINTAINING THE
MINIMUM 3 m (10 ft) MARGIN RECOMMENDED BY ICAO
N_AC_040700_1_0220101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Width
FIGURE-4-7-0-991-022-A01
Page 4
May 01/16
4-7-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-8-0
Aircraft Mooring
**ON A/C A321-100 A321-200 A321neo
Aircraft Mooring
1.
This section provides information on aircraft mooring.
Page 1
May 01/16
4-8-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
TOWING
FITTING
TOWING
FITTING
A
B
GROUND
ANCHOR
FWD
A
B
N_AC_040800_1_0010101_01_00
Aircraft Mooring
FIGURE-4-8-0-991-001-A01
Page 2
May 01/16
4-8-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-1-1
Aircraft Servicing Arrangements
**ON A/C A321-100 A321-200 A321neo
Aircraft Servicing Arrangements
1.
This section provides typical ramp layouts, showing the various GSE items in position during typical
turn-round scenarios.
These ramp layouts show typical arrangements only. Each operator will have its own specific
requirements/regulations for positioning and operation on the ramp.
This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC
AIR CONDITIONING UNIT
AS
AIR START UNIT
BULK
BULK TRAIN
CAT
CATERING TRUCK
CB
CONVEYOR BELT
CLEAN
CLEANING TRUCK
FUEL
FUEL HYDRANT DISPENSER or TANKER
GPU
GROUND POWER UNIT
LDCL
LOWER DECK CARGO LOADER
LV
LAVATORY VEHICLE
PBB
PASSENGER BOARDING BRIDGE
PS
PASSENGER STAIRS
TOW
TOW TRACTOR
ULD
ULD TRAIN
WV
POTABLE WATER VEHICLE
Page 1
May 01/16
5-1-1
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2
Typical Ramp Layout - Open Apron
**ON A/C A321-100 A321-200 A321neo
Typical Ramp Layout - Open Apron
1.
This section gives the typical servicing arrangement for pax version (Open Apron).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m from the
aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks in
position on landing gears).
Page 1
May 01/16
5-1-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FEET
0
5
10 15 20
AS
0
2
4
6
8
TOW
METERS
BULK
CAT
CB
AC
FUEL
BULK
CB
STAND SAFETY LINE
LV
NOTE: TYPICAL RAMP LAYOUT
APPLICABLE TO AIRCRAFT
WITH OR WITHOUT SHARKLETS.
N_AC_050102_1_0050101_01_03
Typical Ramp Layout
Open Apron - Bulk Loading
FIGURE-5-1-2-991-005-A01
Page 2
May 01/16
5-1-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FEET
0
5
10 15 20
AS
0
2
4
6
8
TOW
METERS
ULD
CAT
LD CL
AC
FUEL
ULD
LD CL
CB
BULK
STAND SAFETY LINE
LV
NOTE: TYPICAL RAMP LAYOUT
APPLICABLE TO AIRCRAFT
WITH OR WITHOUT SHARKLETS.
N_AC_050102_1_0100101_01_00
Typical Ramp Layout
Open Apron - ULD Loading
FIGURE-5-1-2-991-010-A01
Page 3
May 01/16
5-1-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3
Typical Ramp Layout - Gate
**ON A/C A321-100 A321-200 A321neo
Typical Ramp Layout - Gate
1.
This section gives the typical servicing arrangement for pax version (Passenger Bridge).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m from the
aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks in
position on landing gears).
Page 1
May 01/16
5-1-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FEET
0
5
10 15 20
AS
0
2
4
6
8
TOW
METERS
ULD
CAT
LD CL
AC
FUEL
ULD
LD CL
CB
BULK
STAND SAFETY LINE
LV
NOTE: TYPICAL RAMP LAYOUT
APPLICABLE TO AIRCRAFT
WITH OR WITHOUT SHARKLETS.
N_AC_050103_1_0030101_01_03
Typical Ramp Layout
Gate
FIGURE-5-1-3-991-003-A01
Page 2
May 01/16
5-1-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0
Terminal Operations - Full Servicing Turn Round Time Chart
**ON A/C A321-100 A321-200 A321neo
Terminal Operations - Full Servicing Turn Round Time
1.
This section provides a typical turn round time chart showing the typical time for ramp activities
during aircraft turn round.
Actual times may vary due to each operator’s specific practices, resources, equipment and operating
conditions.
2.
Assumptions used for full servicing turn round time chart
A.
PASSENGER HANDLING
185 pax: 16 F/C + 169 Y/C.
All passengers deplane and board the aircraft.
1 Passenger Boarding Bridge (PBB) used at door L1.
Equipment positioning + opening door = +2 min.
Closing door + equipment removal = +1.5 min.
No Passenger with Reduced Mobility (PRM) on board.
Deplaning:
-
185 pax at door L1
-
Deplaning rate = 20 pax/min per door
-
Priority deplaning for premium passengers.
Boarding:
-
185 pax at door L1
-
Boarding rate = 12 pax/min per door
-
Last Pax Seating allowance (LPS) + headcounting = +2
min.
B.
CARGO
2 cargo loaders + 1 belt loader.
Opening door + equipment positioning = +2 min.
Equipment removal + closing door = +1.5 min.
100% cargo exchange (baggage only):
-
FWD cargo compartment: 5 containers
-
AFT cargo compartment: 5 containers
-
Bulk compartment: 500 kg (1 102 lb).
Container unloading/loading times:
-
Unloading = 1.5 min/container
-
Loading = 1.5 min/container.
Bulk unloading/loading times:
Page 1
May 01/16
5-2-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
-
Unloading = 150 kg/min (331 lb/min)
-
Loading = 120 kg/min (265 lb/min).
C.
REFUELING
20 000 l (5 283 US gal) at 50 psig (3.45 bars-rel), one hose (right wing).
Dispenser positioning/removal + connection/disconnection times = +2.5
min.
D.
CLEANING
Cleaning is performed in available time.
E.
CATERING
1 catering truck for servicing galleys sequentially at doors R1 and R2.
Equipment positioning + opening door = +2 min.
Closing door + equipment removal = +1.5 min.
Time to drive from one door to the other = +2 min.
Full Size Trolley Equivalent (FSTE) to unload and load: 14 FSTE
-
4 FSTE at door R1
-
10 FSTE at door R2.
Time for trolley exchange = 1.2 min per FSTE.
F.
GROUND HANDLING/GENERAL SERVICING
Start of operations:
-
Bridges/stairs: t0 = 0
-
Other equipment: t = t0 + 1 min.
Ground Power Unit (GPU): up to 90 kVA.
Air conditioning: one hose.
Potable water servicing: 100% uplift, 200 l (53 US gal).
Toilet servicing: draining + rinsing.
Page 2
May 01/16
5-2-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
TRT: 52 min
0
10
20
30
40
50
60
DEPLANING/BOARDING AT L1
HEADCOUNTING
CATERING AT R1
CATERING AT R2
CLEANING
AVAILABLE TIME
CARGO FWD CC
CARGO AFT CC
BULK
REFUELING
POTABLE WATER SERVICING
TOILET SERVICING
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
N_AC_050200_1_0070101_01_02
Full Servicing Turn Round Time Chart
FIGURE-5-2-0-991-007-A01
Page 3
May 01/16
5-2-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0
Terminal Operation - Outstation Turn Round Time Chart
**ON A/C A321-100 A321-200 A321neo
Terminal Operations - Outstation Turn Round Time
1.
This section provides a typical turn round time chart showing the typical time for ramp activities
during aircraft turn round.
Actual times may vary due to each operator’s specific practices, resources, equipment and operating
conditions.
2.
Assumptions used for outstation turn round time chart
A.
PASSENGER HANDLING
220 pax (all Y/C).
All passengers deplane and board the aircraft.
2 stairways used at doors L1 & L2.
Equipment positioning + opening door = +2 min.
Closing door + equipment removal = +1.5 min.
No Passenger with Reduced Mobility (PRM) on board.
Deplaning:
-
110 pax at door L1
-
110 pax at door L2
-
Deplaning rate = 18 pax/min per door.
Boarding:
-
110 pax at door L1
-
110 pax at door L2
-
Boarding rate = 12 pax/min per door
-
Last Pax Seating allowance (LPS) + headcounting = +2
min.
B.
CARGO
2 cargo loaders.
Opening door + equipment positioning = +2 min.
Equipment removal + closing door = +1.5 min.
100% cargo exchange:
-
FWD cargo compartment: 5 containers
-
AFT cargo compartment: 5 containers.
Container unloading/loading times:
-
Unloading = 1.5 min/container
-
Loading = 1.5 min/container.
C.
REFUELING
No refueling.
Page 1
May 01/16
5-3-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
D. CLEANING
Cleaning is performed in available time.
E. CATERING
One catering truck for servicing the galleys as required.
F. GROUND HANDLING/GENERAL SERVICING
Start of operations:
-
Bridges/stairs: t0 = 0
-
Other equipment: t = t0 + 1 min.
Ground Power Unit (GPU): up to 90 kVA.
Air conditioning: one hose.
No potable water servicing.
No toilet servicing.
Page 2
May 01/16
5-3-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
TRT: 23 min
0
5
10
15
20
25
DEPLANING/BOARDING AT L1
DEPLANING/BOARDING AT L2
HEADCOUNTING
CATERING
AVAILABLE TIME
CLEANING
AVAILABLE TIME
CARGO FWD CC
CARGO AFT CC
REFUELING
POTABLE WATER SERVICING
TOILET SERVICING
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
N_AC_050300_1_0040101_01_02
Outstation Turn Round Time Chart
FIGURE-5-3-0-991-004-A01
Page 3
May 01/16
5-3-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1
Ground Service Connections
**ON A/C A321-100 A321-200 A321neo
Ground Service Connections Layout
1.
This section provides the ground service connections layout.
Page 1
May 01/16
5-4-1
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
2
13
12
9
11
1
7
3
8
10
4
5
6
18
9
8
11
15
12
14
16
18
14
1715
13
20
10
19
21
1 − GROUND ELECTRICAL POWER
12 − OVERWING REFUEL (IF INSTALLED)
CONNECTOR
13 − NACA VENT INTAKE
2 − OXYGEN SYSTEM
14 − YELLOW HYDRAULIC−SYSTEM SERVICE PANEL
3 − NLG GROUNDING (EARTHING) POINT
15 − BLUE HYDRAULIC−SYSTEM SERVICE PANEL
4 − POTABLE WATER DRAIN PANEL
16 − ACCUMULATOR CHARGING (GREEN SYSTEM)
AND RESERVOIR DRAIN (GREEN SYSTEM)
5 − LOW PRESSURE AIR PRE−CONDITIONING
6 − HIGH PRESSURE AIR PRE−CONDITIONING
17 − GREEN HYDRAULIC−SYSTEM SERVICE PANEL
7 − REFUEL/DEFUEL INTEGRATED PANEL
18 − MLG GROUNDING (EARTHING) POINT
8 − IDG/STARTER OIL SERVICING
19 − WASTE WATER SERVICE PANEL
9 − ENGINE OIL SERVICING
20 − POTABLE WATER SERVICE PANEL
10 − OVERPRESSURE PROTECTOR
21 − APU OIL SERVICING
11 − REFUEL/DEFUEL COUPLINGS
(OPTIONAL−LH WING)
N_AC_050401_1_0070101_01_02
Ground Service Connections Layout
FIGURE-5-4-1-991-007-A01
Page 2
May 01/16
5-4-1
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2
Grounding Points
**ON A/C A321-100 A321-200 A321neo
Grounding (Earthing) Points
1.
Grounding (Earthing) Points
DISTANCE
FROM AIRCRAFT CENTERLINE MEAN HEIGHT
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
On Nose Landing Gear
5.07 m
0.94 m
On Centerline
leg:
(16.63 ft)
(3.08 ft)
On left Main Landing
21.97 m
3.79 m
1.07 m
-
Gear leg:
(72.08 ft)
(12.43 ft)
(3.51 ft)
On right Main Landing
21.97 m
3.79 m
1.07 m
-
Gear leg:
(72.08 ft)
(12.43 ft)
(3.51 ft)
A. The grounding (earthing) stud on each landing gear leg is designed for use with a clip-on
connector (such as Appleton TGR).
B. The grounding (earthing) studs are used to connect the aircraft to an approved ground (earth)
connection on the ramp or in the hangar for:
-
Refuel/defuel operations,
-
Maintenance operations,
-
Bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tire is sufficient.
If the aircraft is on jacks for retraction and extension checks or for the
removal/installation of the landing gear, the grounding (earthing) alternative points (if
installed) are:
-
In the hole on the avionics-compartment lateral right door-frame (on FR14),
-
On the engine nacelles,
-
Adjacent to the high-pressure connector,
-
On the wing upper surfaces.
Page 1
May 01/16
5-4-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
A
NOSE LANDING GEAR
MAIN LANDING GEAR
LANDING
GEAR
GROUNDING (EARTHING) POINT
GROUNDING (EARTHING) CABLE
A
TYPICAL
N_AC_050402_1_0070101_01_01
Ground Service Connections
Grounding (Earthing) Points - Landing Gear
FIGURE-5-4-2-991-007-A01
Page 2
May 01/16
5-4-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
A
RIB20
RIB19
B
A
FOR SPECIFICATIONS REFER
TO FLIGHT MANUAL
NOTE: R SIDE SYMMETRICAL
F
W
B
D
N_AC_050402_1_0080101_01_00
Ground Service Connections
Grounding (Earthing) Points - Wing (If Installed)
FIGURE-5-4-2-991-008-A01
Page 3
May 01/16
5-4-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FR14
FR12
FR12
A
FR14
Z822
B
C
A
A/C STRUCTURE
GROUNDING
(EARTHING) POINT
GROUNDING
(EARTHING) CABLE
B
FWD
C
N_AC_050402_1_0180101_01_00
Ground Service Connections
Grounding (Earthing) Point - Avionics Compartment Door-Frame
FIGURE-5-4-2-991-018-A01
Page 4
May 01/16
5-4-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
PHONE JACK
GROUNDING (EARTHING) POINT
A
N_AC_050402_1_0190101_01_00
Ground Service Connections
Grounding (Earthing) Point - Engine Air Intake (If Installed)
FIGURE-5-4-2-991-019-A01
Page 5
May 01/16
5-4-2
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3
Hydraulic System
**ON A/C A321-100 A321-200 A321neo
Hydraulic Servicing
1.
Access
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Green System:
23.44 m
1.27 m
1.76 m
Access Door 197CB
(76.90 ft)
(4.17 ft)
(5.77 ft)
Yellow System:
23.44 m
1.27 m
1.76 m
Access Door 198CB
(76.90 ft)
(4.17 ft)
(5.77 ft)
Blue System:
24.49 m
1.27 m
1.76 m
Access Door 197EB
(80.35 ft)
(4.17 ft)
(5.77 ft)
2.
Reservoir Pressurization
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
19.92 m
0.25 m
1.74 m
Access Door 195BB
(65.35 ft)
(0.82 ft)
(5.71 ft)
3.
Accumulator Charging
Four MIL-PRF-6164 connections:
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Yellow System
19.92 m
0.25 m
1.74 m
Accumulator:
(65.35 ft)
(0.82 ft)
(5.71 ft)
Access Door 196BB
Page 1
May 01/16
5-4-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Green System
21.04 m
0.25 m
3.20 m
Accumulator:
(69.03 ft)
(0.82 ft)
(10.50 ft)
Left MLG Door
Blue System
19.92 m
0.25 m
1.74 m
Accumulator:
(65.35 ft)
(0.82 ft)
(5.71 ft)
Access Door 195BB
Yellow System Braking
19.92 m
0.25 m
1.74 m
Accumulator:
(65.35 ft)
(0.82 ft)
(5.71 ft)
Access Door 196BB
4.
Reservoir Filling
Centralized filling capability on the Green System ground service panel:
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
23.44 m
1.27 m
1.76 m
Access Door 197CB
(76.90 ft)
(4.17 ft)
(5.77 ft)
Filling: Ground pressurized supply or hand pump.
5.
Reservoir Drain
Three 3/8 in. self-sealing connections:
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Yellow System:
19.92 m
0.25 m
1.74 m
Access Door 196BB
(65.35 ft)
(0.82 ft)
(5.71 ft)
Green System:
21.04 m
0.25 m
3.20 m
Left MLG Door
(69.03 ft)
(0.82 ft)
(10.5 ft)
Page 2
May 01/16
5-4-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Blue System:
24.49 m
1.27 m
1.76 m
Access Door 197EB
(80.35 ft)
(4.17 ft)
(5.77 ft)
NOTE : The drain valve is on the Blue System ground service panel for the reservoir of the Blue
hydraulic system.
The drain valve is on the reservoir for the Green and Yellow Hydraulic Systems.
6.
Ground Test
On each ground service panel:
-
One self-sealing connector (suction).
-
One self-sealing connector (delivery).
Page 3
May 01/16
5-4-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
FR47
FR50
197CB
RESERVOIR FILL SYSTEM
RESERVOIR FILL SYSTEM
QUANTITY
HAND PUMP FILL CONNECTION
SELECTOR VALVE
INDICATOR
RESERVOIR
DEPRESSURIZATION
CONNECTION
GROUND
GROUND SUPPLY
A
GROUND
DELIVERY
RESERVOIR FILL
SUCTION
CONNECTION
CONNECTION
CONNECTION
FWD
N_AC_050403_1_0040101_01_01
Ground Service Connections
Green System Ground Service Panel
FIGURE-5-4-3-991-004-A01
Page 4
May 01/16
5-4-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
FR47
197EB
FR50
RESERVOIR
GROUND
GROUND
DEPRESSURIZATION
DELIVERY
SUCTION
VALVE
CONNECTION
CONNECTION
RESERVOIR
DRAIN VALVE
A
FWD
N_AC_050403_1_0050101_01_01
Ground Service Connections
Blue System Ground Service Panel
FIGURE-5-4-3-991-005-A01
Page 5
May 01/16
5-4-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FR47
A
FR50
198CB
GROUND
GROUND
DELIVERY
HAND PUMP
SUCTION
CONNECTION
LEVER
CONNECTION
RESERVOIR
A
DEPRESSURIZATION
VALVE
FWD
N_AC_050403_1_0060101_01_01
Ground Service Connections
Yellow System Ground Service Panel
FIGURE-5-4-3-991-006-A01
Page 6
May 01/16
5-4-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
B
Z195
C
A
195BB
A
RAT RETRACTED
RAT UPLOCK SAFETY−PIN
195CB
RAM AIR TURBINE (RAT)
0.64 m (2.10 ft)
01
0.69 m (2.26 ft)
02
GROUND
B
RAT EXTENDED
C
NOTE:
01
FOR A318, A319 AND A320
02
FOR A321
N_AC_050403_1_0070101_01_00
Ground Service Connections
RAT
FIGURE-5-4-3-991-007-A01
Page 7
May 01/16
5-4-3
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4
Electrical System
**ON A/C A321-100 A321-200 A321neo
Electrical System
1.
Electrical System
This chapter provides data related to the location of the ground service connections.
DISTANCE
ACCESS
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
AFT OF NOSE
LH SIDE
RH SIDE
FROM GROUND
A/C External
2.55 m
2.00 m
Power:
On centerline
(8.37 ft)
(6.56 ft)
Access Door 121AL
NOTE : Distances are approximate.
2.
Technical Specifications
A. External Power Receptacle:
-
One receptacle according to MS 90362-3 (without shield MS 17845-1) -- 90 kVA.
NOTE : Make sure that for connectors featuring micro switches, the connector is chamfered to
properly engage in the receptacle.
B. Power Supply:
-
Three-phase, 115/200V, 400 Hz.
C. Electrical Connectors for Servicing:
-
AC outlets: HUBBELL 5258
-
DC outlets: HUBBELL 7472.
Page 1
May 01/16
5-4-4
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
121AL
108VU
A
N_AC_050404_1_0010101_01_01
Ground Service Connections
External Power Receptacles
FIGURE-5-4-4-991-001-A01
Page 2
May 01/16
5-4-4
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5
Oxygen System
**ON A/C A321-100 A321-200 A321neo
Oxygen System
1.
Oxygen System
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN
ACCESS
HEIGHT
AFT OF NOSE
LH SIDE
RH SIDE
FROM
GROUND
Oxygen Replenishment:
3.45 m
1.15 m
2.60 m
-
Access Door 812
(11.32 ft)
(3.77 ft)
(8.53 ft)
2.
Technical Specifications
-
One 3/8 in. MIL-DTL 7891 standard service connection.
NOTE : External charging in the avionics compartment.
Page 1
May 01/16
5-4-5
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
OXYGEN STORAGE
FR16
CYLINDER
FR9
B
Z125
812
A
FR12
FR9
A
C
B
OXYGEN FILLING
PORT
OXYGEN FILLING
INDICATOR
TEST PORT
C
N_AC_050405_1_0010101_01_00
Ground Service Connections
Oxygen System
FIGURE-5-4-5-991-001-A01
Page 2
May 01/16
5-4-5
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6
Fuel System
**ON A/C A321-100 A321-200 A321neo
Fuel System
1.
Refuel/Defuel Control Panel
DISTANCE
POSITION FROM AIRCRAFT
ACCESS
MEAN HEIGHT
AFT OF NOSE
CENTERLINE
FROM GROUND
LH SIDE
RH SIDE
Refuel/Defuel
Integrated Panel:
20.65 m
1.8 m
1.8 m
-
Access Door
(67.75 ft)
(5.91 ft)
(5.91 ft)
192MB
2.
Refuel/Defuel Connectors
DISTANCE
POSITION FROM AIRCRAFT
ACCESS
MEAN HEIGHT
AFT OF NOSE
CENTERLINE
FROM GROUND
LH SIDE
RH SIDE
Refuel/Defuel
Coupling, Left:
21.84 m
9.83 m
3.65 m
Access Panel
-
(71.65 ft)
(32.25 ft)
(11.98 ft)
522HB
(Optional)
Refuel/Defuel
Coupling, Right:
21.84 m
9.83 m
3.65 m
-
Access Panel
(71.65 ft)
(32.25 ft)
(11.98 ft)
622HB
Overwing Gravity-
23.35 m
12.4 m
12.4 m
3.7 m
Refuel Cap
(76.61 ft)
(40.68 ft)
(40.68 ft)
(12.14 ft)
A. Refuel/Defuel Couplings:
-
Right wing: one standard ISO
45,
2.5 in.
-
Left wing: one optional standard ISO 45, 2.5
in.
B. Refuel Pressure:
-
Maximum Pressure: 3.45 bar (50 psi).
C. Average Flow Rate:
-
1250 l/min (330 US gal/min).
Page 1
May 01/16
5-4-6
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3.
Overpressure Protectors and NACA Vent Intake
DISTANCE
POSITION FROM AIRCRAFT
ACCESS
MEAN HEIGHT
AFT OF NOSE
CENTERLINE
FROM GROUND
LH SIDE
RH SIDE
Surge Tank
Overpressure-
24.61 m
14.9 m
14.9 m
4.32 m
Protector:
(80.74 ft)
(48.88 ft)
(48.88 ft)
(14.17 ft)
Access Panel
550CB (650CB)
Wing Tank
Overpressure-
24.2 m
12.15 m
12.15 m
4.1 m
Protector:
(79.40 ft)
(39.86 ft)
(39.86 ft)
(13.45 ft)
Access Panel
540PB (640PB)
NACA Vent Intake:
24.05 m
13.7 m
13.7 m
4.02 m
Access Panel
(78.90 ft)
(44.95 ft)
(44.95 ft)
(13.19 ft)
550AB (650AB)
NOTE : Distances are approximate.
Page 2
May 01/16
5-4-6
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
REFUEL/DEFUEL
CONTROL PANEL
FUEL QTY
kg x 1000
LEFT
CTR
RIGHT
HI
LVL
LEFT
CTR
RIGHT
REFUEL
VALVES
OPEN
OPEN
OPEN
NORM
NORM
NORM
SHUT
SHUT
SHUT
MODE SELECT
TEST BATT POWER
REFUEL
HI LVL
ON
OFF
DEFUEL / XFR
OPEN
LTS
NORM
PRESELECTED
REFUEL
ACTUAL
kg x 1000
DEC
INC
CKPT END
A
NOTE: STANDARD CONFIGURATION OF REFUEL/DEFUEL PANEL.
N_AC_050406_1_0010101_01_00
Ground Service Connections
Refuel/Defuel Control Panel
FIGURE-5-4-6-991-001-A01
Page 3
May 01/16
5-4-6
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
RIB14
RIB15
A
LEADING
EDGE
WING FRONT
SPAR
40QM
41QM
A
N_AC_050406_1_0020101_01_00
Ground Service Connections
Refuel/Defuel Couplings
FIGURE-5-4-6-991-002-A01
Page 4
May 01/16
5-4-6
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
RIB19
A
RIB20
ADAPTER
(REF ONLY)
GROUND CONNECTION
(REF ONLY)
44QM
(45QM)
F
A
W
D
N_AC_050406_1_0030101_01_00
Ground Service Connections
Overwing Gravity-Refuel Cap (If Installed)
FIGURE-5-4-6-991-003-A01
Page 5
May 01/16
5-4-6
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
Z500 (Z600)
540PB (640PB)
C
550AB (650AB)
A
550CB (650CB)
B
RIB19
RIB20
RIB22
RIB25
RIB23
RIB24
NACA VENT
PROTECTOR
NACA VENT INTAKE
A
01
OVERPRESSURE
PROTECTOR
B
C
01
NOTE:
01
LH SHOWN, RH SYMMETRICAL
N_AC_050406_1_0040201_01_00
Ground Service Connections
Overpressure Protectors and NACA Vent Intake
FIGURE-5-4-6-991-004-B01
Page 6
May 01/16
5-4-6
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7
Pneumatic System
**ON A/C A321-100 A321-200 A321neo
Pneumatic System
1.
High Pressure Air Connector
DISTANCE
ACCESS
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
AFT OF NOSE
LH SIDE
RH SIDE
FROM GROUND
HP Connector:
17.25 m
0.84 m
1.76 m
-
Access Door 191DB
(56.59 ft)
(2.76 ft)
(5.77 ft)
A. Connector:
-
One standard 3 in. ISO 2026
connection.
2.
Low Pressure Air Connector
DISTANCE
ACCESS
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
AFT OF NOSE
LH SIDE
RH SIDE
FROM GROUND
LP Connector:
16.72 m
1.11 m
1.73 m
-
Access Door 191CB
(54.86 ft)
(3.64 ft)
(5.68 ft)
A. Connector:
-
One standard 8 in. SAE AS4262 connection.
Page 1
May 01/16
5-4-7
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FR34
FR36
B
A
191CB
191DB
HP CONNECTOR
A
LP CONNECTOR
B
N_AC_050407_1_0010101_01_00
Ground Service Connections
LP and HP Ground Connectors
FIGURE-5-4-7-991-001-A01
Page 2
May 01/16
5-4-7
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8
Oil System
**ON A/C A321-100 A321-200 A321neo
Oil System
**ON A/C A321-100 A321-200
1.
Engine Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-8-991-003-A):
One gravity filling cap and one pressure filling connection per engine.
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
Engine Oil Gravity Filling
Cap:
17.38 m
6.63 m
4.82 m
1.46 m
Access door: 437BL
(57.02 ft)
(21.75 ft)
(15.81 ft)
(4.79 ft)
(LH),
447BL (RH)
Engine Oil Pressure
17.26 m
6.49 m
4.74 m
1.42 m
Filling Port:
(56.63 ft)
(21.29 ft)
(15.55 ft)
(4.66 ft)
NOTE : Distances are approximate.
A. Tank capacity:
-
Full level: 19.6 l (5 US gal),
-
Usable: 9.46 l (3 US gal).
B. Maximum delivery pressure required: 1.72 bar (25 psi).
Maximum delivery flow required: 180 l/h (48 US gal/h).
2.
IDG Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-8-991-004-A):
One pressure filling connection per engine: OMP 2506-18 plus one connection overflow: OMP
2505-18.
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
IDG Oil Pressure Filling
Connection:
16.46 m
6.90 m
5.52 m
0.68 m
Access door: 438AR
(54.00 ft)
(22.64 ft)
(18.11 ft)
(2.23 ft)
(LH),
448AR (RH)
Page 1
May 01/16
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@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOTE : Distances are approximate.
A. Tank capacity: 5 l (1 US gal).
B. Delivery pressure required: 0.34 bar (5 psi) to 2.76 bar (40 psi) at the IDG inlet.
3.
Starter Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-8-991-005-A):
One gravity filling cap per engine.
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
Starter Oil Filling
16.81 m
5.30 m
6.20 m
0.76 m
Connection:
(55.15 ft)
(17.39 ft)
(20.34 ft)
(2.49 ft)
NOTE : Distances are approximate.
A. Tank capacity: 0.8 l (0.21 US gal).
4.
Engine Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-8-991-006-B):
One gravity filling cap per engine.
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
Engine Oil Gravity Filling
Cap:
16.50 m
6.56 m
4.92 m
1.22 m
Access door: 437BL
(54.13 ft)
(21.52 ft)
(16.14 ft)
(4.00 ft)
(LH),
447BL (RH)
NOTE : Distances are approximate.
A. Tank capacity:
-
Full level: 28 l (7 US gal),
-
Usable: 23.50 l (6 US gal).
5.
IDG Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-8-991-007-B):
One pressure filling connection per engine: 2506-2 plus one overflow connection: 2505-2.
Page 2
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
IDG Oil Pressure Filling
17.06 m
5.42 m
6.04 m
0.80 m
Connection:
(55.97 ft)
(17.78 ft)
(19.82 ft)
(2.62 ft)
NOTE : Distances are approximate.
A. Tank capacity: 4.10 l (1 US gal).
6.
Starter Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-8-991-008-B):
One gravity filling cap per engine.
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
Starter Oil Filling
19.66 m
5.30 m
6.14 m
0.75 m
Connection:
(64.50 ft)
(17.39 ft)
(20.14 ft)
(2.46 ft)
NOTE : Distances are approximate.
A. Tank capacity: 0.35 l (0.09 US gal).
**ON A/C A321-100 A321-200 A321neo
7.
APU Oil System (See FIGURE 5-4-8-991-009-A):
APU oil gravity filling cap.
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
42.42 m
0.30 m
4.83 m
-
GTCP 36-300
(139.17 ft)
(0.98 ft)
(15.85 ft)
42.42 m
0.30 m
4.78 m
-
APS 3200
(139.17 ft)
(0.98 ft)
(15.68 ft)
42.32 m
0.35 m
4.32 m
-
131-9
(138.85 ft)
(1.15 ft)
(14.17 ft)
NOTE : Distances are approximate.
Page 3
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
A. Tank capacity (usable):
-
APU type GTCP 36-300: 6.20 l (2 US gal),
-
APU type APS 3200: 5.40 l (1 US gal),
-
APU type 131-9: 6.25 l (2 US gal).
Page 4
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5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
A
B
437BL (ENGINE 1)
447BL (ENGINE 2)
FWD
A
OIL IN
VENT
OIL LEVEL
TRANSMITTER
(OPTIONAL)
ANTI−SIPHON
DEVICE
OIL CAP
AIR PRESSURE
SWITCH NIPPLE
SIGHT WINDOW
PRESSURE NIPPLE
OIL OUT
SELF−SEALING MAGNETIC
DRAIN PLUG
OIL/FUEL HEAT
SERVO FUEL
EXCHANGER
HEATER
B
N_AC_050408_1_0030101_01_00
Ground Service Connections
Engine Oil Tank -- CFM56 Series Engine
FIGURE-5-4-8-991-003-A01
Page 5
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
B
A
1 − PRESSURE FILL VALVE
2 − CASE DRAIN PLUG
3 − DUST CAP
4 − DUST CAP
5 − OVERFLOW DRAIN VALVE
1
5
OVER
A
2
FULL
4
3
B
ADD
ADD
OIL
OIL
A
C
NOTE: A
IF THE OIL LEVEL IS ABOVE
THE YELLOW BAND, OIL SERVICING
IS REQUIRED.
CFM−56
B
IF THE OIL LEVEL IS WITHIN
THE GREEN AND YELLOW BANDS,
SIGHT GLASS
OIL SERVICING IS NOT REQUIRED.
C
IF THE OIL LEVEL IS BELOW
THE GREEN BAND, OIL SERVICING
IS REQUIRED.
B
N_AC_050408_1_0040101_01_00
Ground Service Connections
IDG Oil Tank -- CFM56 Series Engine
FIGURE-5-4-8-991-004-A01
Page 6
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
A
STARTER
DRAIN PORT
AND MAGNETIC
PLUG
OVERFLOW
PLUG
OIL FILLER
PLUG
A
N_AC_050408_1_0050101_01_00
Ground Service Connections
Starter Oil Tank -- CFM56 Series Engine
FIGURE-5-4-8-991-005-A01
Page 7
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
A
437BL (ENGINE 1)
FCOC
447BL (ENGINE 2)
GRAVITY
FILLER CAP
PRISMALITE
B
LEVEL INDICATOR
OIL TANK
FWD
A
’FULL’ LEVEL NOTCH
27.3 LT
29.0 US QTS
6.0 IMP GAL
(WITHIN 60 MIN FROM SHUTDOWN)
NOTCH ’1’
26 LT
27 US QTS
NOTCH ’2’
5.7 IMP GAL
23 LT
24 US QTS
5.1 IMP GAL
NOTCH ’3’
20 LT
22 US QTS
4.5 IMP GAL
B
N_AC_050408_1_0060201_01_00
Ground Service Connections
Engine Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-8-991-006-B01
Page 8
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
IDG
B
PRESSURE
A
FILL VALVE
OVER FLOW
OIL LEVEL
DRAIN VALVE
INDICATOR
DUST CAP
DUST CAP
OVER FLOW
OVER FULL
PRESSURE
OVER FULL
DRAIN HOSE
FILL HOSE
ADD
ADD
ADD
ADD
OIL
OIL
OIL
OIL
CORRECTLY FILLED IDG
V2500
V2500
A
B
B
AFTER SERVICING OR
AFTER ENGINE
ENGINE SHUTDOWN
SHUTDOWN
(COLD OIL/IDG)
(HOT OIL/IDG)
OIL LEVEL CAN BE
OIL LEVEL MUST BE AT OR NEAR
IN THE GREEN BAND OR THE
THE LINE BETWEEN THE YELLOW BAND
YELLOW BAND
AND THE GREEN BAND
INCORRECTLY FILLED IDG
OVER FULL
OVER FULL
OVER FULL
ADD
ADD
ADD
ADD
ADD
ADD
OIL
OIL
OIL
OIL
OIL
OIL
V2500
V2500
V2500
B
B
AFTER SERVICING OR
AT ALL TIMES
ENGINE SHUTDOWN
(HOT OR COLD OIL/IDG)
(COLD OIL/IDG)
THE OIL LEVEL MUST NOT BE IN
THE OIL LEVEL MUST NOT BE
THE YELLOW BAND BUT IT CAN
IN THE RED BAND
BE IMMEDIATELY ABOVE THE
LOWER LIMIT OF THE YELLOW
BAND BECAUSE OF THE AIRCRAFT
PERFORM IDG OIL SERVICING
RAMP ANGLE
TO GET THE CORRECT IDG OIL LEVEL.
DO NOT USE THE OVERFLOW DRAIN HOSE
DO THE IDG SERVICING
TO GET THE CORRECT IDG OIL LEVEL.
TO GET THE CORRECT IDG
OIL LEVEL.
N_AC_050408_1_0070201_01_00
Ground Service Connections
IDG Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-8-991-007-B01
Page 9
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
THE STARTER IS FULL WHEN THE OIL LEVEL
*
SHOWS NOT LESS THAN 3/4 FULL
ON THE SIGHT GLASS
A
B
EXTERNAL GEARBOX
OIL FILLING POINT
ADAPTER
B
SIGHT GLASS
OIL OVERFLOW
POINT
PNEUMATIC STARTER
A
N_AC_050408_1_0080201_01_00
Ground Service Connections
Starter Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-8-991-008-B01
Page 10
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
FR84
A
Z315
(Z316)
FR80
GRAVITY
OIL FILLER
OIL LEVEL
SIGHT GLASS
PRESSURE
FILL PORT
OVERFLOW
DRAIN VALVE
A
N_AC_050408_1_0090101_01_00
Ground Service Connections
APU Oil Tank
FIGURE-5-4-8-991-009-A01
Page 11
May 01/16
5-4-8
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9
Potable Water System
**ON A/C A321-100 A321-200 A321neo
Potable Water System
1.
Potable Water Ground Service Panels
DISTANCE
POSITION FROM AIRCRAFT
ACCESS
MEAN HEIGHT
AFT OF NOSE
CENTERLINE
FROM GROUND
LH SIDE
RH SIDE
Potable-Water
38.2 m
0.3 m
2.6 m
-
Service Panel:
(125.33 ft)
(0.98 ft)
(8.53 ft)
Access Door 171AL
Potable-Water
11.8 m
0.15 m
1.75 m
-
Drain Panel:
(38.71 ft)
(0.49 ft)
(5.74 ft)
Access Door 133AL
NOTE : Distances are approximate.
2.
Technical Specifications
A. Connectors:
(1) On the potable-water service panel (Access Door 171AL)
-
Fill/Drain Nipple 3/4 in. (ISO 17775).
-
One ground air-pressure connector.
(2) On the potable-water drain panel (Access Door 133AL)
-
Drain Nipple 3/4 in. (ISO 17775).
B. Usable capacity:
-
Standard configuration - one tank: 200 l (53 US gal).
C. Filling pressure:
-
3.45 bar (50 psi).
D. Typical flow rate:
-
50 l/min (13 US gal/min).
Page 1
May 01/16
5-4-9
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
FR29
133AL
DRAIN CONTROL
HANDLE
B
171AL
FR28
DRAIN PORT
FILL/DRAIN
CONTROL HANDLE
A
OVERFLOW PORT
POTABLE−WATER DRAIN PANEL
FR66
FR65
FILL/DRAIN PORT
GROUND AIR−PRESSURE
CONNECTION
B
POTABLE−WATER SERVICE PANEL
N_AC_050409_1_0290101_01_00
Ground Service Connections
Potable Water Ground Service Panels
FIGURE-5-4-9-991-029-A01
Page 2
May 01/16
5-4-9
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
B
Z170
FR68
FR65
A
POTABLE WATER
TANK
FILL/DRAIN
LINE
OVERFLOW
POTABLE WATER
LINE
DISTRIBUTION LINE
B
N_AC_050409_1_0300101_01_00
Ground Service Connections
Potable Water Tank Location
FIGURE-5-4-9-991-030-A01
Page 3
May 01/16
5-4-9
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10
Waste Water System
**ON A/C A321-100 A321-200 A321neo
Vacuum Toilet System
1.
Vacuum Toilet System
DISTANCE
POSITION FROM AIRCRAFT
ACCESS
MEAN HEIGHT
AFT OF NOSE
CENTERLINE
FROM GROUND
LH SIDE
RH SIDE
Waste-Water
Ground Service
38.2 m
0.8 m
2.8 m
-
Panel:
(125.33 ft)
(2.62 ft)
(9.19 ft)
Access door 172AR
NOTE : Distances are approximate.
2.
Technical Specifications
A. Connectors:
-
Draining: 4 in. (ISO 17775).
-
Flushing and filling: 1 in. (ISO 17775).
B. Usable waste tank capacity:
-
Standard configuration - one tank: 177 l (47 US gal).
C. Waste tank - Rinsing:
-
Operating pressure: 3.45 bar (50 psi).
D. Waste tank - Precharge:
-
10 l (3 US gal).
Page 1
May 01/16
5-4-10
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
Z172
FR66
FR65
FILL AND RINSE
TOILET DRAIN
CONNECTION
CONNECTION
A
N_AC_050410_1_0010101_01_00
Ground Service Connections
Waste Water Ground Service Panel
FIGURE-5-4-10-991-001-A01
Page 2
May 01/16
5-4-10
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
A
Z170
FR68
WASTE TANK
FR65
FLUSH LINE
DRAIN LINE
A
N_AC_050410_1_0040101_01_00
Ground Service Connections
Waste Tank Location
FIGURE-5-4-10-991-004-A01
Page 3
May 01/16
5-4-10
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0
Engine Starting Pneumatic Requirements
**ON A/C A321-100 A321-200 A321neo
Engine Starting Pneumatic Requirements
1.
The purpose of this section is to provide the minimum air data requirements at the aircraft
connection, needed to start the engine within no more than 60 seconds, at sea level (0 feet), for a set
of Outside Air Temperatures (OAT).
ABBREVIATION
DEFINITION
A/C
Aircraft
ASU
Air Start Unit
HPGC
High Pressure Ground Connection
OAT
Outside Air Temperature
A. Air data (discharge temperature, absolute discharge pressure) are given at the HPGC.
B. For a given OAT the following charts are used to determine an acceptable combination for air
discharge temperature, absolute discharge pressure and mass flow rate.
C. This section addresses requirements for the ASU only, and is not representative of the start
performance of the aircraft using the APU or engine cross bleed procedure.
D. To protect the A/C, the charts feature, if necessary:
-
The maximum discharge pressure at the HPGC
-
The maximum discharge temperature at the HPGC.
Page 1
May 01/16
5-5-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
CFM56 SERIES/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
70
150
65
140
60
130
55
120
50
110
45
100
35
40
45
50
ABSOLUTE PRESSURE (psia)
50
45
40
35
−45
−35
−25
−15
−5
5
15
25
35
45
55
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
120
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
EXAMPLE:
FOR AN OAT OF 15° C (59° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 220° C (428° F)
AT HPGC:
− THE REQUIRED PRESSURE AT HPGC IS 41 psia
− THE REQUIRED AIRFLOW AT A/C CONNECTION IS 49.5 kg/min.
NOTE:
IN CASE THE ACTUAL DISCHARGE TEMPERATURE OF THE ASU DIFFERS SUBSTANTIALLY FROM THE
ONES GIVEN IN THE CHARTS, A SIMPLE INTERPOLATION (LINEAR) IS SUFFICIENT TO DETERMINE THE
REQUIRED AIR DATA.
N_AC_050500_1_0160101_01_00
Example for Use of the Charts
FIGURE-5-5-0-991-016-A01
Page 2
May 01/16
5-5-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
A321-200
IAE V2500 SERIES/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
85
180
80
170
75
160
70
150
65
140
60
130
55
120
50
110
45
100
35
40
45
50
55
60
65
ABSOLUTE PRESSURE (psia)
65
60
55
50
45
40
35
−50
−40
−30
−20
−10
0
10
20
30
40
50
60
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
120
140
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
N_AC_050500_1_0170101_01_00
Engine Starting Pneumatic Requirements
IAE V2500 Series Engine
FIGURE-5-5-0-991-017-A01
Page 3
May 01/16
5-5-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
CFM56 SERIES AND CFM LEAP−1A NEO/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
70
150
65
140
60
130
55
120
50
110
45
100
35
40
45
50
ABSOLUTE PRESSURE (psia)
50
45
40
35
−45
−35
−25
−15
−5
5
15
25
35
45
55
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
120
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
N_AC_050500_1_0180101_01_00
Engine Starting Pneumatic Requirements
CFM56 Series and CFM LEAP-1A NEO Engine
FIGURE-5-5-0-991-018-A01
Page 4
May 01/16
5-5-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321neo
PW 1100G NEO/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
80
170
75
160
70
150
65
140
60
130
55
40
45
50
55
ABSOLUTE PRESSURE (psia)
55
50
45
40
−45
−35
−25
−15
−5
5
15
25
35
45
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
N_AC_050500_1_0190101_01_00
Engine Starting Pneumatic Requirements
PW 1100G NEO Engine
FIGURE-5-5-0-991-019-A01
Page 5
May 01/16
5-5-0
@A321
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0
Ground Pneumatic Power Requirements
**ON A/C A321-100 A321-200 A321neo
Ground Pneumatic Power Requirements
1.
General
This section describes the required performance for the ground equipment to maintain the cabin
temperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for heating cases after boarding
(Section 5.7 - steady state), and provides the time needed to cool down or heat up the aircraft cabin
to the required temperature (Section 5.6 - dynamic cases with aircraft empty).
ABBREVIATION
DEFINITION
A/C
Aircraft
AHM
Aircraft Handling Manual
AMM
Aircraft Maintenance Manual
GC
Ground Connection
GSE
Ground Service Equipment
IFE
In-Flight Entertainment
OAT
Outside Air Temperature
PCA
Pre-Conditioned Air
A. The air flow rates and temperature requirements for the GSE, provided in Sections 5.6 and 5.7,
are given at A/C ground connection.
NOTE : The cooling capacity of the equipment (kW) is only indicative and is not sufficient by
itself to ensure the performance (outlet temperature and flow rate combinations are
the requirements needed for ground power). An example of cooling capacity
calculation is given in Section 5.7.
NOTE : The maximum air flow is driven by pressure limitation at the ground connection.
B. For temperatures at ground connection below 2 ˚C (35.6 ˚F) (Subfreezing), the ground
equipment shall be compliant with the Airbus document ”Subfreezing PCA Carts - Compliance
Document for Suppliers” (contact Airbus to obtain this document) defining all the requirements
with which Subfreezing Pre-Conditioning Air equipment must comply to allow its use on Airbus
aircraft. These requirements are in addition to the functional specifications included in the IATA
AHM997.
2.
Ground Pneumatic Power Requirements
This section provides the ground pneumatic power requirements for:
-
Heating (pull up) the cabin, initially at OAT, up to 21 ˚C (69.8 ˚F) (see FIGURE
5-6-0-991-001-A)
-
Cooling (pull down) the cabin, initially at OAT, down to 27 ˚C (80.6 ˚F) (see FIGURE
5-6-0-991-002-A).
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
PULL UP PERFORMANCE
1.4
MAXIMUM AIRFLOW
3.0
1.3
1.2
2.5
1.1
1.0
0.9
2.0
0.8
0.7
1.5
0.6
0.5
1.0
0.4
15
30
45
60
75
90
TIME TO HEAT CABIN TO +21° C (+69.8° F) ON GROUND (min)
OAT ISA −38° C ( −36.4° F); GC INLET +70° C (+158° F); EMPTY CABIN; IFE OFF; NO SOLAR
LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
N_AC_050600_1_0010101_01_00
Ground Pneumatic Power Requirements
Heating
FIGURE-5-6-0-991-001-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
PULL DOWN PERFORMANCE
1.4
MAXIMUM AIRFLOW
3.0
1.3
1.2
2.5
1.1
1.0
0.9
2.0
0.8
0.7
1.5
0.6
30
45
60
75
90
105
120
TIME TO COOL CABIN TO +27° C (+80.6° F) ON GROUND (min)
OAT ISA +23° C (+73.4° F); GC INLET +2° C (+35.6° F); EMPTY CABIN; IFE OFF; NO SOLAR
LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
OAT ISA +23° C (+73.4° F); GC INLET −10° C (+14° F); EMPTY CABIN; IFE OFF; NO SOLAR
LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
N_AC_050600_1_0020101_01_00
Ground Pneumatic Power Requirements
Cooling
FIGURE-5-6-0-991-002-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0
Preconditioned Airflow Requirements
**ON A/C A321-100 A321-200 A321neo
Preconditioned Airflow Requirements
1.
This section provides the preconditioned airflow rate and temperature needed to maintain the cabin
temperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for the heating cases.
These settings are not intended to be used for operation (they are not a substitute for the settings
given in the AMM). They are based on theoretical simulations and give the picture of a real steady
state.
The purpose of the air conditioning (cooling) operation (described in the AMM) is to maintain the
cabin temperature below 27 ˚C (80.6 ˚F) during boarding (therefore it is not a steady state).
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200 A321neo
COOLING/HEATING PERFORMANCE
1.4
3.0
MAXIMUM AIRFLOW (RECIRCULATION FANS OFF)
1.2
2.5
MAXIMUM AIRFLOW
(RECIRCULATION
FANS ON)
1.0
H
SETTINGS NOT
INTENDED TO BE USED
2.0
C2
FOR OPERATION
C1
0.8
1.5
0.6
1.0
0.4
−10
−5
0
2
5
10
15
20
25
30
35
INLET TEMPERATURE AT GC (° C)
20
30
40
50
60
70
80
90
INLET TEMPERATURE AT GC (° F)
OAT ISA +23° C (73.4° F); EMPTY CABIN; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION
FANS ON; GALLEYS ON
OAT ISA; 164 PAX; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON; GALLEYS ON
OAT ISA −38° C ( −36.4° F); EMPTY CABIN; IFE OFF; LIGHTS ON; NO SOLAR LOAD; RECIRCULATION
FANS ON; GALLEYS OFF
N_AC_050700_1_0030101_01_04
Preconditioned Airflow Requirements
FIGURE-5-7-0-991-003-A01
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