Airbus A318. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016) - page 2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
WING JACK PAD
A
LOWER SURFACE
B
POINT BB’ DETAIL
RIB9INTERSECTION WITH REAR
SPAR DATUM
Z−828.35
A
Z−895
EXAMPLE
SPHERICAL RADIUS
32 mm (1.26 in)
B
N_AC_021400_1_0560101_01_00
Jacking for Maintenance
Wing Jacking Points
FIGURE-2-14-0-991-056-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FR74
FR73
A
Z−729.441
Z−744.932
SPHERICAL RADIUS 19 mm (0.75 in)
(19 D535−71 595)
126.15 mm
(4.97 in)
A
FWD
N_AC_021400_1_0570101_01_01
Jacking for Maintenance
Safety Stay
FIGURE-2-14-0-991-057-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FR73 FR74
FR8
FUSELAGE
DATUM LINE
FORWARD JACK
WING JACK
SAFETY STAY
N
L
RIB9
RIB9
WING JACK
FORWARD WING JACK
M
JACK
TYPICAL JACK INSTALLATION SHOWN
DISTANCE BETWEEN
JACKING/SAFETY POINTS
AND THE GROUND
CONFIGURATION
DESCRIPTION
L
M
N
(FORWARD
(WING
(SAFETY
JACK)
JACK)
STAY)
− NLG SHOCK ABSORBER DEFLATED AND
NLG TIRES FLAT
1 565 mm
3 136 mm
3 685 mm
− MLG STANDARD TIRES, WITH STANDARD
(61.61 in)
(123.46 in)
(145.08 in)
SHOCK ABSORBERS
− AIRCRAFT ON WHEELS
TIRES FLAT
1 660 mm
2 736 mm
2 836 mm
SHOCK ABSORBERS DEFLATED
(65.35 in)
(107.72 in)
(111.65 in)
STANDARD TIRES
1 851 mm
3 138 mm
3 430 mm
STANDARD SHOCK ABSORBERS
(72.87 in)
(123.54 in)
(135.04 in)
STANDARD TIRES
−AIRCRAFT ON JACKS
MLG SHOCK ABSORBERS EXTENDED WITH
2 554 mm
3 655 mm
3 779 mm
(FORWARD JACK AND
WHEEL CLEARANCE OF 120 mm (4.72 in)
(100.55 in)
(143.90 in)
(148.78 in)
WING JACKS)
FOR MLG RETRACTION OR EXTENSION
− FUSELAGE DATUM LINE
PARALLEL TO THE GROUND
STANDARD TIRES
MLG SHOCK ABSORBERS EXTENDED WITH
3 204 mm
4 305 mm
4 429 mm
WHEEL CLEARANCE OF 770 mm (30.31 in)
(126.14 in)
(169.49 in)
(174.37 in)
FOR REPLACEMENT OF THE MLG
− AIRCRAFT ON FORWARD
STANDARD TIRES
JACK
NLG SHOCK ABSORBERS EXTENDED WITH
2 395 mm
2 939 mm
NA
−MLG WHEELS ON THE
WHEEL CLEARANCE OF 60 mm (2.36 in)
(94.29 in)
(115.71 in)
GROUND
FOR NLG RETRACTION OR EXTENSION
NOTE:
THE SAFETY STAY IS NOT USED FOR JACKING.
N_AC_021400_1_0040101_01_02
Jacking for Maintenance
Jacking Design
FIGURE-2-14-0-991-004-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
49 x 19 R20
600 mm
(23.62 in)
FULLY
EXTENDED
45 x 16 R20
200 mm
218 mm
25 mm
38 mm
552 mm
(7.87 in)
(8.58 in)
(1 in)
(1.5 in)
(21.73 in)
FULLY
DIA. BALL
RETRACTED
180 mm
INFLATED TIRES
(7.09 in)
ON THE RIM
FLAT TIRES
NOTE: TWIN WHEEL TRACK IS 927 mm (36.5 in).
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES.
THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)
CLEARANCE BETWEEN THE TIRE AND GROUND.
N_AC_021400_1_0120101_01_00
Jacking of the Landing Gear
MLG Jacking Point Location - Twin Wheels
FIGURE-2-14-0-991-012-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
643 mm
(25.32 in)
MLG TIRE 49 x 19 R20
CANTILEVER
ARM
552 mm
(21.73 in)
25 mm
FWD
(1 in)
TWIN WHEEL TRACK
927 mm
(36.5 in)
DOUBLE FLAT MLG TIRES
218 mm (8.58 in)
(180 mm (7.09 in)
ON RIM)
409 mm
FORK
(16.1 in)
25 mm
1 620 mm
25 mm
MIN
APPROX
MIN
(1 in)
(63.78 in)
(1 in)
CONTOUR OF TIRES ON GROUND
N_AC_021400_1_0130101_01_00
Jacking of the Landing Gear
MLG Jacking with Cantilever Jack - Twin Wheels
FIGURE-2-14-0-991-013-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
32
30
CG POSITION
15.0% MAC
18.7% MAC
28
25.0% MAC
31.0% MAC
37.0% MAC
26
24
22
20
18
16
14
35
40
45
50
55
60
65
70
(x1 000 kg)
80
90
100
110
120
130
140
150
(x1 000 lbs)
AIRCRAFT GROSS WEIGHT
N_AC_021400_1_0140101_01_00
Jacking of the Landing Gear
Loads at MLG Jacking Points - Twin Wheels
FIGURE-2-14-0-991-014-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
40 mm
128 mm
25 mm
38 mm
326 mm
APPROX
(1.57 in)
(5.04 in)
(1 in)
(1.5 in)
(12.83 in)
DIA. BALL
SAE AS 33559
FWD
500 mm (19.69 in)
264 mm MIN (10.39 in)
289 mm MAX (11.38 in)
198 mm
(7.8 in)
FLAT TIRES
INFLATED TIRES
A
NOTE:
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES.
THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)
CLEARANCE BETWEEN THE TIRE AND GROUND.
N_AC_021400_1_0150101_01_00
Jacking of the Landing Gear
NLG Jacking - Point Location
FIGURE-2-14-0-991-015-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
14
12
CG POSITION
15.0% MAC
18.7% MAC
25.0% MAC
31.0% MAC
37.0% MAC
10
8
6
4
2
35
40
45
50
55
60
65
70
(x1 000 kg)
80
90
100
110
120
130
140
150
(x1 000 lbs)
AIRCRAFT GROSS WEIGHT
N_AC_021400_1_0160101_01_00
Jacking of the Landing Gear
Loads at NLG Jacking Points
FIGURE-2-14-0-991-016-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0
General Information
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1
Payload / Range - ISA Conditions
**ON A/C A318-100
Payload/Range - ISA Conditions
1.
This section provides the payload/range at ISA conditions.
Page 1
May 01/16
3-2-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_030201_1_0120101_01_00
Payload/Range - ISA Conditions
FIGURE-3-2-1-991-012-A01
Page 2
May 01/16
3-2-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1
Take-off Weight Limitation - ISA Conditions
**ON A/C A318-100
Take-Off Weight Limitation - ISA Conditions
1.
This section gives the take-off weight limitation at ISA conditions.
Page 1
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3-3-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
200
90
190
180
80
0
2
170
4
6
160
8
70
150
140
60
130
120
50
110
100
90
40
80
70
1000 ft
30
4
6
8
10
12
14
16
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030301_1_0010101_01_00
Take-Off Weight Limitation - ISA Conditions
CFM56 Series Engine
FIGURE-3-3-1-991-001-A01
Page 2
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3-3-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
200
90
190
180
80
170
160
70
0
2
4
6
150
8
140
60
130
120
50
110
100
90
40
80
70
1000 ft
30
4
6
8
10
12
14
16
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030301_1_0020101_01_00
Take-Off Weight Limitation - ISA Conditions
PW 6000 Series Engine
FIGURE-3-3-1-991-002-A01
Page 3
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3-3-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2
Take-off Weight Limitation - ISA +15˚C (+59˚F) Conditions
**ON A/C A318-100
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
1.
This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions.
Page 1
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3-3-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
200
90
190
180
80
0
2
170
4
6
160
8
70
150
140
60
130
120
50
110
100
90
40
80
70
1000 ft
30
4
6
8
10
12
14
16
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030302_1_0010101_01_00
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
CFM56 Series Engine
FIGURE-3-3-2-991-001-A01
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3-3-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1000 kg
1000 lb
200
90
190
180
80
170
160
70
2
4
6
150
8
140
60
130
120
50
110
100
90
40
80
70
1000 ft
30
4
6
8
10
12
14
16
RUNWAY LENGTH
1000 m
1
2
3
4
5
N_AC_030302_1_0020101_01_00
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
PW 6000 Series Engine
FIGURE-3-3-2-991-002-A01
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3-3-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1
Landing Field Length - ISA Conditions
**ON A/C A318-100
Landing Field Length - ISA Conditions
1.
This section provides the landing field length.
Page 1
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3-4-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
(x 1 000 ft) (x 1 000 m)
12
3.5
10
3.0
8
2.5
AIRFIELD ELEVATION
(x 1 000 ft)
6
2.0
8
6
4
4
1.5
2
0
2
1.0
35
40
45
50
55
60
65
GROSS WEIGHT (x 1 000 kg)
80
90
100
110
120
130
140
GROSS WEIGHT (x 1 000 lb)
NOTE:
THESE CURVES ARE GIVEN FOR INFORMATION ONLY.
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
N_AC_030401_1_0010101_01_01
Landing Field Length - ISA Conditions
CFM56-5B Series Engine
FIGURE-3-4-1-991-001-A01
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3-4-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
(x 1 000 ft)
(x 1 000 m)
12
3.5
10
3.0
8
2.5
AIRFIELD ELEVATION
6
(1 000 ft)
2.0
8
6
4
1.5
4
2
0
2
1.0
35
40
45
50
55
60
65
GROSS WEIGHT (x 1 000 kg)
80
90
100
110
120
130
140
GROSS WEIGHT (x 1 000 lb)
NOTE:
THESE CURVES ARE GIVEN FOR INFORMATION ONLY.
THE APPROVED VALUES ARE STATED IN THE "OPERATING
MANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
N_AC_030401_1_0020101_01_01
Landing Field Length - ISA Conditions
PW 6000 Series Engine
FIGURE-3-4-1-991-002-A01
Page 3
May 01/16
3-4-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0
Final Approach Speed
**ON A/C A318-100
Final Approach Speed
1.
This section provides the final approach speed. It is defined as the indicated airspeed at threshold in
the landing configuration, at the certificated maximum flap setting and Maximum Landing Weight
(MLW), in standard atmospheric conditions. The approach speed is used to classify the aircraft into
an Aircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.
2.
The final approach speed is 121 kt at a MLW of 57 500 kg (126 766 lb) and classifies the aircraft
into the Aircraft Approach Category C.
NOTE : This value is given for information only.
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3-5-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0
General Information
**ON A/C A318-100
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.
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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 A318-100
Turning Radii
1.
This section provides the turning radii.
Page 1
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4-2-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
R3
50°
R1
R5
60°
7.59 m
(24.9 ft)
70°
R2
R6
10.25 m
(33.63 ft)
R4
NOTE:
FOR STEERING DIMENSION TABLE SEE SHEET 2.
TURN TYPE:
1. ASYMMETRIC THRUST DIFFERENTIAL BRAKING
(PIVOTTING ON ONE MAIN GEAR).
2. SYMMETRIC THRUST NO BRAKING.
N_AC_040200_1_0010101_01_02
Turning Radii, No Slip Angle
(Sheet 1)
FIGURE-4-2-0-991-001-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_040200_1_0020101_01_02
Turning Radii, No Slip Angle
(Sheet 2)
FIGURE-4-2-0-991-002-A01
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0
Minimum Turning Radii
**ON A/C A318-100
Minimum Turning Radii
1.
This section provides the minimum turning radii.
Page 1
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4-3-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
R4
10.3 m
(34 ft)
R6
OUTSIDE FACE OF TIRE
Y
EFFECTIVE
TURN
A
STEERING
ANGLE 75°
MINIMUM
PAVEMENT
WIDTH FOR
180° TURN
R3
R5
NOTE:
NOSE GEAR RADII TRACK R3,
MEASURED FROM OUTSIDE FACE OF TIRE.
MODEL 100 TURN DIMENSION SHOWN.
THEORETICAL CENTER OF TURN
FOR MINIMUM TURNING RADIUS.
SLOW CONTINUOUS TURNING.
APPROXIMATELY IDLE THRUST
ON BOTH ENGINES.
NO DIFFERENTIAL BRAKING.
DRY SURFACE.
TYPE
STEERING
EFFECTIVE
R4
R3
R5
R6
OF
ANGLE
STEERING
Y
A
WING TIP
NLG
NOSE
THS
TURN
(DEG)
ANGLE
FENCE
m
3.4
19.0
10.9
20.9
15.7
18.1
1
75 (MAX)
71.8°
ft
11
62
36
68
51
59
m
3.7
19.4
11.0
21.2
15.8
18.2
2
75 (MAX)
70.3°
ft
12
64
36
69
52
60
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_0010101_01_03
Minimum Turning Radii
FIGURE-4-3-0-991-001-A01
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0
Visibility from Cockpit in Static Position
**ON A/C A318-100
Visibility from Cockpit in Static Position
1.
This section gives the visibility from cockpit in static position.
Page 1
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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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4-4-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_040400_1_0050101_01_00
Binocular Visibility Through Windows from Captain Eye Position
FIGURE-4-4-0-991-005-A01
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4-4-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0
Runway and Taxiway Turn Paths
**ON A/C A318-100
Runway and Taxiway Turn Paths
1.
Runway and Taxiway Turn Paths.
Page 1
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4-5-0
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1
135˚ Turn - Runway to Taxiway
**ON A/C A318-100
135˚ Turn - Runway to Taxiway
1.
This section gives the 135˚ turn - runway to taxiway.
Page 1
May 01/16
4-5-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
APPROX 5.7 m
(19 ft)
TAXIWAY
FILLET R = 16.5 m
CENTERLINE
(55 ft)
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_0010101_01_02
135˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-1-991-001-A01
Page 2
May 01/16
4-5-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
APPROX 3.2 m
(10 ft)
TAXIWAY
FILLET R = 16.5 m
CENTERLINE
(55 ft)
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_0110101_01_00
135˚ Turn - Runway to Taxiway
Judgemental Oversteering Method
FIGURE-4-5-1-991-011-A01
Page 3
May 01/16
4-5-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2
90˚ Turn - Runway to Taxiway
**ON A/C A318-100
90˚ Turn - Runway to Taxiway
1.
This section gives the 90˚ turn - runway to taxiway.
Page 1
May 01/16
4-5-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 6.9 m
(22 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_0010101_01_02
90˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-2-991-001-A01
Page 2
May 01/16
4-5-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 9.3 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_0080101_01_00
90˚ Turn - Runway to Taxiway
Judgemental Oversteering Method
FIGURE-4-5-2-991-008-A01
Page 3
May 01/16
4-5-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3
180˚ Turn on a Runway
**ON A/C A318-100
180˚ Turn on a Runway
1.
This section provides the 180˚ turn on a runway.
Page 1
May 01/16
4-5-3
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RUNWAY CENTERLINE
7.4 m
(24 ft)
3 m
(10 ft)
R3 = 10.9 m
(36 ft)
R5 = 15.8 m
(52 ft)
R4 = 20.9 m
(69 ft)
NLG PATH
WINGTIP PATH
NOSE PATH
MLG PATH
30 m
(100 ft)
NOTE:
TYPE 1 VALUES.
N_AC_040503_1_0050101_01_01
180˚ Turn on a Runway
Edge of Runway Method (Sheet 1 of 2)
FIGURE-4-5-3-991-005-A01
Page 2
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RUNWAY CENTERLINE
R4 = 20.9 m
(69 ft)
R5 = 15.8 m
(52 ft)
R3 = 10.9 m
(36 ft)
6.23 m
(20 ft)
4.76 m
(16 ft)
25°
NLG PATH
WINGTIP PATH
NOSE PATH
MLG PATH
30 m
(100 ft)
NOTE:
TYPE 1 VALUES.
N_AC_040503_1_0050102_01_01
180˚ Turn on a Runway
Center of Runway Method (Sheet 2 of 2)
FIGURE-4-5-3-991-005-A01
Page 3
May 01/16
4-5-3
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4
135˚ Turn - Taxiway to Taxiway
**ON A/C A318-100
135˚ Turn - Taxiway to Taxiway
1.
This section gives the 135˚ turn - taxiway to taxiway.
Page 1
May 01/16
4-5-4
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
APPROX 6.3 m
(21 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_0010101_01_02
135˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-4-991-001-A01
Page 2
May 01/16
4-5-4
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
APPROX 3.1 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_0010102_01_00
135˚ Turn - Taxiway to Taxiway
Judgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-4-991-001-A01
Page 3
May 01/16
4-5-4
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5
90˚ Turn - Taxiway to Taxiway
**ON A/C A318-100
90˚ Turn - Taxiway to Taxiway
1.
This section gives the 90˚ turn - taxiway to taxiway.
Page 1
May 01/16
4-5-5
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 6.4 m
TAXIWAY CENTERLINE
(21 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_0010101_01_02
90˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-5-991-001-A01
Page 2
May 01/16
4-5-5
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 9.3 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_0010102_01_00
90˚ Turn - Taxiway to Taxiway
Judgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-5-991-001-A01
Page 3
May 01/16
4-5-5
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0
Runway Holding Bay (Apron)
**ON A/C A318-100
Runway Holding Bay (Apron)
1.
This section gives the runway holding bay (Apron).
Page 1
May 01/16
4-6-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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)
N_AC_040600_1_0010101_01_02
Runway Holding Bay (Apron)
FIGURE-4-6-0-991-001-A01
Page 2
May 01/16
4-6-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0
Minimum Line-Up Distance Corrections
**ON A/C A318-100
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 4-7-0-991-014-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 4-7-0-991-015-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 4-7-0-991-016-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
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4-7-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
3 m
(10 ft)
TODA
ASDA
> 3 m
TAXIWAY
(10 ft)
CENTERLINE
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
MAX
AIRCRAFT
STEERING
MINIMUM LINE−UP
TYPE
ANGLE
DISTANCE CORRECTION
ON TODA
ON ASDA
A318
75°
10.8 m
35 ft
21.1 m
69 ft
N_AC_040700_1_0140101_01_00
Minimum Line-Up Distance Corrections
90˚ Turn on Runway Entry
FIGURE-4-7-0-991-014-A01
Page 2
May 01/16
4-7-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
MINIMUM PAVEMENT WIDTH
3 m
(10 ft)
> 3 m
3 m
(10 ft)
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
MAX
AIRCRAFT
MINIMUM LINE−UP
STEERING
REQUIRED
TYPE
DISTANCE
MINIMUM
ANGLE
CORRECTION
PAVEMENT
WIDTH
ON TODA
ON ASDA
A318
75°
14.1 m
46 ft
24.4 m
80 ft
29.2 m
96 ft
N_AC_040700_1_0150101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Turn Pad
FIGURE-4-7-0-991-015-A01
Page 3
May 01/16
4-7-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
3 m
(10 ft)
TODA
3 m
(10 ft)
ASDA
> 3 m
(10 ft)
RUNWAY CENTERLINE
25°
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
MAX
AIRCRAFT
STEERING
MINIMUM LINE−UP
TYPE
ANGLE
DISTANCE CORRECTION
ON TODA
ON ASDA
A318
75°
14.1 m
46 ft
24.4 m
80 ft
N_AC_040700_1_0160101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Width
FIGURE-4-7-0-991-016-A01
Page 4
May 01/16
4-7-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-8-0
Aircraft Mooring
**ON A/C A318-100
Aircraft Mooring
1.
This section provides information on aircraft mooring.
Page 1
May 01/16
4-8-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-1-1
Aircraft Servicing Arrangements
**ON A/C A318-100
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
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5-1-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2
Typical Ramp Layout - Open Apron
**ON A/C A318-100
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 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
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5-1-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FEET
0
5
10 15 20
0
2
4
6
8
METERS
AS
TOW
BULK
CAT
CB
FUEL
BULK
CB
WV
LV
STAND SAFETY LINE
N_AC_050102_1_0010101_01_04
Typical Ramp Layout
Open Apron - Bulk Loading
FIGURE-5-1-2-991-001-A01
Page 2
May 01/16
5-1-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3
Typical Ramp Layout - Gate
**ON A/C A318-100
Typical Ramp Layout - Gate
1.
This section give 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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FEET
0
5
10 15 20
0
2
4
6
8
METERS
TOW
AS
BULK
CAT
CB
FUEL
BULK
CB
WV
LV
STAND SAFETY LINE
N_AC_050103_1_0040101_01_03
Typical Ramp Layout
Gate
FIGURE-5-1-3-991-004-A01
Page 2
May 01/16
5-1-3
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0
Terminal Operations - Full Servicing Turn Round Time Chart
**ON A/C A318-100
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
107 pax: 8 F/C + 99 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:
-
107 pax at door L1
-
Deplaning rate = 20 pax/min per door
-
Priority deplaning for premium passengers.
Boarding:
-
107 pax at door L1
-
Boarding rate = 12 pax/min per door
-
Last Pax Seating allowance (LPS) + headcounting = +2
min.
B.
CARGO
2 belt loaders.
Opening door + equipment positioning = +2 min.
Equipment removal + closing door = +1.5 min.
100% cargo exchange (baggage only):
An average 15 kg (33 lb) per pax is assumed.
-
FWD cargo compartment: 800 kg (1 764 lb)
-
AFT cargo compartment: 800 kg (1 764 lb).
Bulk unloading/loading times:
-
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).
Page 1
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@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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: 8 FSTE
-
4 FSTE at door R1
-
4 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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
TRT: 35 min
0
5
10
15
20
25
30
35
40
DEPLANING/BOARDING AT L1
HEADCOUNTING
CATERING AT R1
CATERING AT R2
CLEANING
AVAILABLE TIME
CARGO FWD CC
CARGO AFT CC
REFUELING
POTABLE WATER SERVICING
TOILET SERVICING
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
N_AC_050200_1_0040101_01_03
Full Servicing Turn Round Time Chart
FIGURE-5-2-0-991-004-A01
Page 3
May 01/16
5-2-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0
Terminal Operation - Outstation Turn Round Time Chart
**ON A/C A318-100
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
132 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:
-
66 pax at door L1
-
66 pax at door L2
-
Deplaning rate = 18 pax/min per door.
Boarding:
-
66 pax at door L1
-
66 pax at door L2
-
Boarding rate = 12 pax/min per door
-
Last Pax Seating allowance (LPS) + headcounting = +2
min.
B.
CARGO
2 belt loaders.
Opening door + equipment positioning = +2 min.
Equipment removal + closing door = +1.5 min.
100% cargo exchange (baggage only):
An average 15 kg (33 lb) per pax is assumed.
-
FWD cargo compartment: 990 kg (2 183 lb)
-
AFT cargo compartment: 990 kg (2 183 lb).
Bulk unloading/loading times:
-
Unloading = 120 kg/min (265 lb/min)
-
Loading = 100 kg/min (220 lb/min).
Page 1
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
C. REFUELING
No refueling.
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
TRT: 21 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_0010101_01_02
Outstation Turn Round Time Chart
FIGURE-5-3-0-991-001-A01
Page 3
May 01/16
5-3-0
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1
Ground Service Connections
**ON A/C A318-100
Ground Service Connections Layout
1.
This section provides the ground service connections layout.
Page 1
May 01/16
5-4-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
9
12
11
10
7
8
6
1
2
9
3
4
17
8
5
7
10
14
15
13
11
13
1614
17
19
18
9
9
20
12
1 − GROUND ELECTRICAL POWER
11 − OVERWING REFUEL (IF INSTALLED)
CONNECTOR
12 − NACA VENT INTAKE
2 − NLG GROUNDING (EARTHING) POINT
13 − YELLOW HYDRAULIC−SYSTEM SERVICE PANEL
14 − BLUE HYDRAULIC−SYSTEM SERVICE PANEL
3 − POTABLE WATER DRAIN PANEL
4 − LOW PRESSURE AIR PRE−CONDITIONING
15 − ACCUMULATOR CHARGING (GREEN SYSTEM)
5 − HIGH PRESSURE AIR PRE−CONDITIONING
AND RESERVOIR DRAIN (GREEN SYSTEM)
6 − REFUEL/DEFUEL INTEGRATED PANEL
16 − GREEN HYDRAULIC−SYSTEM SERVICE PANEL
7 − IDG/STARTER OIL SERVICING
17 − MLG GROUNDING (EARTHING) POINT
8 − ENGINE OIL SERVICING*
18 − WASTE WATER SERVICE PANEL
9 − OVERPRESSURE PROTECTOR
19 − POTABLE WATER SERVICE PANEL
10 − REFUEL/DEFUEL COUPLINGS
20 − APU OIL SERVICING
(OPTIONAL−LH WING)
NOTE:
* FOR THE PW 6000 ENGINE, THE ENGINE OIL SERVICING POINTS (8) ARE LOCATED SYMMETRICALLY ON
THE RH SIDE OF EACH ENGINE.
THE ENGINE OIL SERVICING POINTS (8) ARE SHOWN FOR THE CFM 56 ENGINE.
N_AC_050401_1_0010101_01_02
Ground Service Connections Layout
FIGURE-5-4-1-991-001-A01
Page 2
May 01/16
5-4-1
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2
Grounding Points
**ON A/C A318-100
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
15.32 m
3.79 m
1.07 m
-
Gear leg:
(50.26 ft)
(12.43 ft)
(3.51 ft)
On right Main Landing
15.32 m
3.79 m
1.07 m
-
Gear leg:
(50.26 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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
A
NOSE LANDING GEAR
MAIN LANDING GEAR
LANDING
GEAR
GROUNDING (EARTHING) POINT
GROUNDING (EARTHING) CABLE
A
TYPICAL
N_AC_050402_1_0010101_01_01
Ground Service Connections
Grounding (Earthing) Points - Landing Gear
FIGURE-5-4-2-991-001-A01
Page 2
May 01/16
5-4-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
A
RIB20
RIB19
B
A
FOR SPECIFICATIONS REFER
TO FLIGHT MANUAL
NOTE: R SIDE SYMMETRICAL
F
W
B
D
N_AC_050402_1_0020101_01_00
Ground Service Connections
Grounding (Earthing) Points - Wing (If Installed)
FIGURE-5-4-2-991-002-A01
Page 3
May 01/16
5-4-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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_0090101_01_00
Ground Service Connections
Grounding (Earthing) Point - Avionics Compartment Door-Frame
FIGURE-5-4-2-991-009-A01
Page 4
May 01/16
5-4-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
PHONE JACK
GROUNDING (EARTHING) POINT
A
N_AC_050402_1_0100101_01_00
Ground Service Connections
Grounding (Earthing) Point - Engine Air Intake (If Installed)
FIGURE-5-4-2-991-010-A01
Page 5
May 01/16
5-4-2
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3
Hydraulic System
**ON A/C A318-100
Hydraulic Servicing
1.
Access
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Green System:
16.43 m
1.27 m
1.76 m
Access Door 197CB
(53.90 ft)
(4.17 ft)
(5.77 ft)
Yellow System:
16.43 m
1.27 m
1.76 m
Access Door 198CB
(53.90 ft)
(4.17 ft)
(5.77 ft)
Blue System:
16.96 m
1.27 m
1.76 m
Access Door 197EB
(55.64 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
13.20 m
0.25 m
1.74 m
Access Door 195BB
(43.31 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
13.20 m
0.25 m
1.74 m
Accumulator:
(43.31 ft)
(0.82 ft)
(5.71 ft)
Access Door 196BB
Page 1
May 01/16
5-4-3
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Green System
14.30 m
0.25 m
3.20 m
Accumulator:
(46.92 ft)
(0.82 ft)
(10.50 ft)
Left MLG Door
Blue System
13.20 m
0.25 m
1.74 m
Accumulator:
(43.31 ft)
(0.82 ft)
(5.71 ft)
Access Door 195BB
Yellow System Braking
13.20 m
0.25 m
1.74 m
Accumulator:
(43.31 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
16.43 m
1.27 m
1.76 m
Access Door 197CB
(53.90 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:
13.20 m
0.25 m
1.74 m
Access Door 196BB
(43.31 ft)
(0.82 ft)
(5.71 ft)
Green System:
14.30 m
0.25 m
3.20 m
Left MLG Door
(46.92 ft)
(0.82 ft)
(10.50 ft)
Page 2
May 01/16
5-4-3
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Blue System:
16.96 m
1.27 m
1.76 m
Access Door 197EB
(55.64 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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4
Electrical System
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5
Oxygen System
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6
Fuel System
**ON A/C A318-100
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:
14.01 m
1.8 m
1.8 m
-
Access Door
(45.96 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:
15.2 m
9.83 m
3.65 m
Access Panel
-
(49.87 ft)
(32.25 ft)
(11.98 ft)
522HB
(Optional)
Refuel/Defuel
Coupling, Right:
15.2 m
9.83 m
3.65 m
-
Access Panel
(49.87 ft)
(32.25 ft)
(11.98 ft)
622HB
Overwing Gravity-
16.71 m
12.4 m
12.4 m
3.7 m
Refuel Cap
(54.82 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
@A318
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-
17.96 m
14.9 m
14.9 m
4.32 m
Protector:
(58.92 ft)
(48.88 ft)
(48.88 ft)
(14.17 ft)
Access Panel
550CB (650CB)
Inner Cell
Overpressure-
16.5 m
9.19 m
9.19 m
4.1 m
Protector:
(54.14 ft)
(30.15 ft)
(30.15 ft)
(13.45 ft)
Access Panel
540HB (640HB)
NACA Vent Intake:
17.4 m
13.7 m
13.7 m
4.02 m
Access Panel
(57.09 ft)
(44.95 ft)
(44.95 ft)
(13.19 ft)
550AB (650AB)
NOTE : Distances are approximate.
Page 2
May 01/16
5-4-6
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
Z500 (Z600)
C
540HB (640HB)
A
550AB (650AB)
550CB (650CB)
B
RIB14
RIB22
RIB25
RIB13
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_0040101_01_01
Ground Service Connections
Overpressure Protectors and NACA Vent Intake
FIGURE-5-4-6-991-004-A01
Page 6
May 01/16
5-4-6
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7
Pneumatic System
**ON A/C A318-100
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:
10.43 m
0.84 m
1.76 m
-
Access Door 191DB
(34.22 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:
9.9 m
1.11 m
1.73 m
-
Access Door 191CB
(32.48 ft)
(3.64 ft)
(5.68 ft)
A. Connector:
-
One standard 8 in. SAE AS4262 connection.
Page 1
May 01/16
5-4-7
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8
Oil System
**ON A/C A318-100
Oil System
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:
12.30 m
6.63 m
4.82 m
1.46 m
Access door: 437BL
(40.35 ft)
(21.75 ft)
(15.81 ft)
(4.79 ft)
(LH),
447BL (RH)
Engine Oil Pressure
12.20 m
6.49 m
4.74 m
1.42 m
Filling Port:
(40.03 ft)
(21.29 ft)
(15.55 ft)
(4.66 ft)
NOTE : Distances are approximate.
A. Tank capacity:
-
Full level: 19.60 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.
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
ENGINE 1 (LH) ENGINE 2 (RH)
GROUND
IDG Oil Pressure Filling
Connection:
11.40 m
6.90 m
5.52 m
0.68 m
Access door: 438AR
(37.40 ft)
(22.64 ft)
(18.11 ft)
(2.23 ft)
(LH),
448AR (RH)
NOTE : Distances are approximate.
A. IDG oil tank capacity: 5 l (1 US gal).
Page 1
May 01/16
5-4-8
@A318
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B. Maximum servicing pressure: 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
10.40 m
5.30 m
6.20 m
0.76 m
Connection:
(34.12 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 PW 6000 Series Engine (See FIGURE 5-4-8-991-006-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
Engine Oil Gravity Filling
Cap:
10.16 m
4.80 m
6.63 m
1.80 m
Access door: 438BR
(33.33 ft)
(15.75 ft)
(21.75 ft)
(5.91 ft)
(LH),
448BR (RH)
NOTE : Distances are approximate.
A. Tank capacity:
-
Full level: 18.36 l (5 US gal),
-
Usable: 23.50 l (6 US gal),
-
Engine oil tank capacity: 18.36 l (5 US gal).
5.
IDG Oil Replenishment for PW 6000 Series Engine (See FIGURE 5-4-8-991-007-A):
One pressure filling connection per engine.
Page 2
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@A318
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
Connection:
10.00 m
5.33 m
6.17 m
1.02 m
Access door: 438DR
(32.81 ft)
(17.49 ft)
(20.24 ft)
(3.35 ft)
(LH),
448DR (RH)
NOTE : Distances are approximate.
A. Distances are approximate.
-
Tank capacity: 6.28 l (2 US gal),
-
Maximum servicing pressure: 2.41 bar (35 psi).
6.
Starter Oil Replenishment for PW 6000 Series Engine (See FIGURE 5-4-8-991-008-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
10.16 m
5.84 m
5.59 m
1.02 m
Connection:
(33.33 ft)
(19.16 ft)
(18.34 ft)
(3.35 ft)
NOTE : Distances are approximate.
A. Tank capacity: 0.35 l (0.09 US gal).
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
29.37 m
0.30 m
4.83 m
GTCP 36-300
-
(96.36 ft)
(0.98 ft)
(15.85 ft)
29.37 m
0.30 m
4.78 m
-
APS 3200
(96.36 ft)
(0.98 ft)
(15.68 ft)
29.27 m
0.35 m
4.32 m
131-9
-
(96.03 ft)
(1.15 ft)
(14.17 ft)
Page 3
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOTE : Distances are approximate.
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
May 01/16
5-4-8
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
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
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
438BR (ENGINE 1)
448BR (ENGINE 2)
OIL
A
FULL
FULL
1
1
QTS
LTR
LOW
LOW
LEVEL
B
SIGHT GLASS
B
OIL TANK
CAP
N−02463(0601)
PW V
A
N_AC_050408_1_0060101_01_00
Ground Service Connections
Engine Oil Tank -- PW6000 Series Engine
FIGURE-5-4-8-991-006-A01
Page 8
May 01/16
5-4-8