Airbus A319. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016) - page 3

 

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Airbus A319. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016) - page 3

 

 

1
2
3
4
5
6
V(NG)
V(MG)(PER STRUT)
H (PER STRUT)
MAXIMUM
STATIC BRAKING
STEADY BRAKING
AT INSTANTANEOUS
WEIGHT
STATIC LOAD AT
STATIC LOAD AT
RAMP
AT 10 ft/s²
AT 10 ft/s²
BRAKING
VARIANT
FWD CG
AFT CG
WEIGHT
DECELERATION
DECELERATION
COEFFICIENT = 0.8
A319−100
64 400 kg
9 300 kg
21 %
15 310 kg
29 450 kg
36 %
10 010 kg
23 560 kg
WV008
(141 975 lb)
(20 500 lb)
MAC (a)
(33 750 lb)
(64 925 lb)
MAC (a)
(22 075 lb)
(51 925 lb)
(CG 36 %)
A319−100
66 400 kg
9 580 kg
21 %
15 770 kg
30 730 kg
38.8 %
10 320 kg
24 590 kg
WV009
(146 375 lb)
(21 125 lb)
MAC (a)
(34 775 lb)
(67 750 lb)
MAC (a)
(22 750 lb)
(54 200 lb)
(CG 38.8 %)
A319−100
66 400 kg
9 580 kg
21 %
15 770 kg
30 360 kg
36 %
10 320 kg
24 290 kg
WV009
(146 375 lb)
(21 125 lb)
MAC (a)
(34 775 lb)
(66 950 lb)
MAC (a)
(22 750 lb)
(53 550 lb)
(CG 36 %)
A319−100
66 400 kg
9 580 kg
21 %
15 770 kg
30 730 kg
38.8 %
10 320 kg
24 590 kg
WV011
(146 375 lb)
(21 125 lb)
MAC (a)
(34 775 lb)
(67 750 lb)
MAC (a)
(22 750 lb)
(54 200 lb)
(CG 38.8 %)
A319−100
66 400 kg
9 580 kg
21 %
15 770 kg
30 360 kg
36 %
10 320 kg
24 290 kg
WV011
(146 375 lb)
(21 125 lb)
MAC (a)
(34 775 lb)
(66 950 lb)
MAC (a)
(22 750 lb)
(53 550 lb)
(CG 36 %)
A319−100
62 400 kg
9 170 kg
20.4 %
15 000 kg
28 900 kg
39 %
9 700 kg
23 120 kg
WV012
(137 575 lb)
(20 200 lb)
MAC (a)
(33 075 lb)
(63 725 lb)
MAC (a)
(21 375 lb)
(50 975 lb)
(CG 39 %)
A319−100
62 400 kg
9 170 kg
20.4 %
15 000 kg
28 530 kg
36 %
9 700 kg
22 820 kg
WV012
(137 575 lb)
(20 200 lb)
MAC (a)
(33 075 lb)
(62 900 lb)
MAC (a)
(21 375 lb)
(50 325 lb)
(CG 36 %)
A319 CJ
75 900 kg
11 540 kg
14 %
17 880 kg
34 750 kg
36 %
11 800 kg
27 800 kg
WV002
(167 325 lb)
(25 450 lb)
MAC (b)
(39 425 lb)
(76 625 lb)
MAC (a)
(26 000 lb)
(61 300 lb)
A319 CJ
70 400 kg
11 550 kg
14 %
17 990 kg
32 240 kg
36 %
10 940 kg
25 800 kg
WV005
(155 200 lb)
(25 450 lb)
MAC (b)
(39 650 lb)
(71 075 lb)
MAC (a)
(24 125 lb)
(56 875 lb)
A319 CJ
76 900 kg
11 540 kg
14 %
17 790 kg
35 180 kg
36 %
11 950 kg
28 140 kg
WV010
(169 525 lb)
(25 450 lb)
MAC (b)
(39 225 lb)
(77 550 lb)
MAC (a)
(26 350 lb)
(62 050 lb)
A319 CJ
75 900 kg
11 540 kg
14 %
17 880 kg
34 750 kg
36 %
11 800 kg
27 800 kg
WV013
(167 325 lb)
(25 450 lb)
MAC (b)
(39 425 lb)
(76 625 lb)
MAC (a)
(26 000 lb)
(61 300 lb)
NOTE:
(a) LOADS CALCULATED USING AIRCRAFT AT MRW.
(b) LOADS CALCULATED USING AIRCRAFT AT 67 500 kg (148 800 lb).
H
V
(NG)
V(MG)
V
MAXIMUM VERTICAL NOSE GEAR GROUND LOAD AT FWD CG
(NG)
V(MG)MAXIMUM VERTICAL MAIN GEAR GROUND LOAD AT AFT CG
H MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING
1
2
3
4
5
6
V(NG)
V(MG)(PER STRUT)
H (PER STRUT)
MAXIMUM
STATIC BRAKING
STEADY BRAKING
AT INSTANTANEOUS
WEIGHT
STATIC LOAD AT
STATIC LOAD AT
RAMP
AT 10 ft/s²
AT 10 ft/s²
BRAKING
VARIANT
FWD CG
AFT CG
WEIGHT
DECELERATION
DECELERATION
COEFFICIENT = 0.8
A319NEO
64 400 kg
9 300 kg
21 %
15 310 kg
29 830 kg
39 %
10 010 kg
23 860 kg
WV050
(141 975 lb)
(20 500 lb)
MAC (a)
(33 750 lb)
(65 775 lb)
MAC (a)
(22 075 lb)
(52 600 lb)
A319NEO
64 400 kg
9 300 kg
21 %
15 320 kg
29 190 kg
34 %
10 010 kg
23 350 kg
WV050
(141 975 lb)
(20 500 lb)
MAC (a)
(33 775 lb)
(64 350 lb)
MAC (a)
(22 075 lb)
(51 475 lb)
(CG 34 %)
A319NEO
64 400 kg
9 300 kg
21 %
15 310 kg
29 830 kg
39 %
10 010 kg
23 860 kg
WV051
(141 975 lb)
(20 500 lb)
MAC (a)
(33 750 lb)
(65 775 lb)
MAC (a)
(22 075 lb)
(52 600 lb)
A319NEO
70 400 kg
10 120 kg
21 %
16 660 kg
32 420 kg
37.5 %
10 940 kg
25 940 kg
WV052
(155 200 lb)
(22 325 lb)
MAC (a)
(36 725 lb)
(71 475 lb)
MAC (a)
(24 125 lb)
(57 175 lb)
A319NEO
70 400 kg
10 120 kg
21 %
16 660 kg
32 420 kg
37.5 %
10 940 kg
25 940 kg
WV053
(155 200 lb)
(22 325 lb)
MAC (a)
(36 725 lb)
(71 475 lb)
MAC (a)
(24 125 lb)
(57 175 lb)
A319NEO
75 900 kg
10 720 kg
21 %
17 870 kg
34 750 kg
36 %
11 800 kg
27 800 kg
WV054
(167 325 lb)
(23 625 lb)
MAC (b)
(39 400 lb)
(76 600 lb)
MAC (a)
(26 000 lb)
(61 275 lb)
A319NEO
75 900 kg
10 720 kg
21 %
17 870 kg
34 440 kg
34 %
11 800 kg
27 550 kg
WV054
(167 325 lb)
(23 625 lb)
MAC (b)
(39 400 lb)
(75 925 lb)
MAC (a)
(26 000 lb)
(60 750 lb)
(CG 34 %)
A319NEO
75 900 kg
10 720 kg
21 %
17 870 kg
34 750 kg
36 %
11 800 kg
27 800 kg
WV055
(167 325 lb)
(23 625 lb)
MAC (b)
(39 400 lb)
(76 600 lb)
MAC (a)
(26 000 lb)
(61 275 lb)
A319NEO
75 900 kg
10 720 kg
21 %
17 870 kg
34 440 kg
34 %
11 800 kg
27 550 kg
WV055
(167 325 lb)
(23 625 lb)
MAC (b)
(39 400 lb)
(75 925 lb)
MAC (a)
(26 000 lb)
(60 750 lb)
(CG 34 %)
NOTE:
(a) LOADS CALCULATED USING AIRCRAFT AT MRW.
(b) LOADS CALCULATED USING AIRCRAFT AT 74 500 kg (164 250 lb).
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0
Landing Gear Loading on Pavement
**ON A/C A319-100 A319neo
Landing Gear Loading on Pavement
1.
Landing Gear Loading on Pavement
This section provides data about the landing gear loading on pavement.
The MLG loading on pavement graphs are given for the weight variants that produce (at the MRW
and maximum aft CG) the lowest MLG load and the highest MLG load for each type of aircraft.
Example, see FIGURE 7-4-0-991-003-A, calculation of the total weight on the MLG for:
-
An aircraft with a MRW of 62 400 kg (137 575 lb),
-
The aircraft gross weight is 60 000 kg (132 275 lb),
-
A percentage of weight on the MLG of 91.5% (percentage of weight on the MLG at MRW and
maximum aft CG).
The total weight on the MLG group is 54 890 kg (121 000 lb).
NOTE : The CG in the figure title is the CG used for ACN/LCN calculation.
Page 1
May 01/16
7-4-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
80
80
170
75
75
160
70
70
150
65
65
CG FOR ACN
CALCULATION
140
36% MAC
MTOW − 62 000 kg
60
60
130
MLW
20.4% MAC
55
55
120
50
50
110
MZFW
100
45
45
LANDING
90
40
40
TAKE OFF
80
35
35
80
82
84
86
88
90
92
94
96
98
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
N_AC_070400_1_0030101_01_00
Landing Gear Loading on Pavement
WV012, MRW 62 400 kg, CG 36%
FIGURE-7-4-0-991-003-A01
Page 2
May 01/16
7-4-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
80
80
CG FOR ACN
CALCULATION
170
36% MAC
75
75
MTOW − 76 500 kg
160
70
26% MAC
70
150
65
65
140
60
MLW
60
130
55
55
120
50
50
110
MZFW
100
45
45
LANDING
90
40
40
TAKE OFF
80
35
35
80
82
84
86
88
90
92
94
96
98
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
N_AC_070400_1_0040101_01_00
Landing Gear Loading on Pavement
WV010, MRW 76 900 kg, CG 36%
FIGURE-7-4-0-991-004-A01
Page 3
May 01/16
7-4-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
80
80
170
75
75
160
70
70
150
65
CG FOR ACN
65
CALCULATION
34% MAC
140
MLW
MTOW − 64 000 kg
60
60
130
21% MAC
55
55
120
50
50
110
MZFW
100
45
45
LANDING
90
40
40
TAKE OFF
80
35
35
80
82
84
86
88
90
92
94
96
98
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
N_AC_070400_1_0050101_01_01
Landing Gear Loading on Pavement
WV050, MRW 64 400 kg, CG 34%
FIGURE-7-4-0-991-005-A01
Page 4
May 01/16
7-4-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
80
80
CG FOR ACN
170
CALCULATION
75
36% MAC
75
MTOW − 75 500 kg
160
70
70
26% MAC
150
65
65
140
MLW
60
60
130
55
55
120
50
50
110
MZFW
100
45
45
LANDING
90
40
40
TAKE OFF
80
35
35
80
82
84
86
88
90
92
94
96
98
100
PERCENTAGE OF WEIGHT ON MAIN GEAR
N_AC_070400_1_0060101_01_00
Landing Gear Loading on Pavement
WV054, MRW 75 900 kg, CG 36%
FIGURE-7-4-0-991-006-A01
Page 5
May 01/16
7-4-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A319-100 A319neo
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
1.
This section provides data about the flexible pavement requirements.
The flexible pavement requirement graphs are given at standard tire pressure for the weight variants
producing (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG load for
each type of aircraft.
They are calculated with the US Army Corps of Engineers Design Method.
To find a flexible pavement thickness, you must know the Subgrade Strength (CBR), the annual
departure level and the weight on one MLG.
The line that shows 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).
The procedure that follows is used to develop flexible pavement design curves:
-
With the scale for pavement thickness at the bottom and the scale for CBR at the top, a random
line is made to show 10 000 coverages,
-
A plot is then made of the incremental values of the weight on the MLG,
-
Annual departure lines are made based on the load lines of the weight on the MLG that is shown
on the graph.
Example, see FIGURE 7-5-0-991-003-A, calculation of the thickness of the flexible pavement for
MLG:
-
An aircraft with a MRW of 62 400 kg (137 575 lb),
-
A ”CBR” value of 10,
-
An annual departure level of 3 000,
-
The load on one MLG of 25 000 kg (55 125 lb).
The required flexible pavement thickness is 46.5 cm (18 in).
NOTE : The CG in the figure title is the CG used for ACN calculation.
Page 1
May 01/16
7-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
3
6
10
15
20
30
40
60
80
WEIGHT ON ONE MAIN LANDING GEAR
28 530 kg (62 900 lb)
25 000 kg (55 125 lb)
20 000 kg (44 100 lb)
15 000 kg (33 075 lb)
10 000 kg (22 050 lb)
MAXIMUM POSSIBLE
MAIN GEAR LOAD
AT MAXIMUM RAMP
WEIGHT AND AFT CG
10 000 COVERAGES USED
FOR ACN CALCULATIONS
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*
1 200
3 000
6 000
15 000
25 000
*20 YEAR PAVEMENT LIFE
3
6
10
15
20
30
40
60
80
(in)
10
15
20
30
40
60
80
100
120
150 180
(cm)
FLEXIBLE PAVEMENT THICKNESS
46x17R20 (46x16−20) TIRES
TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
N_AC_070500_1_0030101_01_00
Flexible Pavement Requirements
WV012, MRW 62 400 kg, CG 36 %
FIGURE-7-5-0-991-003-A01
Page 2
May 01/16
7-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
3
6
10
15
20
30
40
60
80
WEIGHT ON ONE MAIN LANDING GEAR
35 180 kg (77 550 lb)
25 000 kg (55 125 lb)
20 000 kg (44 100 lb)
15 000 kg (33 075 lb)
10 000 kg (22 050 lb)
MAXIMUM POSSIBLE
MAIN GEAR LOAD
AT MAXIMUM RAMP
WEIGHT AND AFT CG
10 000 COVERAGES USED
FOR ACN CALCULATIONS
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*
1 200
3 000
6 000
15 000
25 000
*20 YEAR PAVEMENT LIFE
3
6
10
15
20
30
40
60
80
(in)
10
15
20
30
40
60
80
100
120
150 180
(cm)
FLEXIBLE PAVEMENT THICKNESS
46x17R20 TIRES
TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
N_AC_070500_1_0040101_01_00
Flexible Pavement Requirements
WV010, MRW 76 900 kg, CG 36 %
FIGURE-7-5-0-991-004-A01
Page 3
May 01/16
7-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
SUBGRADE STRENGTH − CBR
3
6
10
15
20
30
40
60
80
WEIGHT ON ONE MAIN LANDING GEAR
29 190 kg (64 350 lb)
25 000 kg (55 125 lb)
20 000 kg (44 100 lb)
15 000 kg (33 075 lb)
10 000 kg (22 050 lb)
MAXIMUM POSSIBLE
MAIN GEAR LOAD
AT MAXIMUM RAMP
WEIGHT AND AFT CG
10 000 COVERAGES USED
FOR ACN CALCULATIONS
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*
1 200
3 000
6 000
15 000
25 000
*20 YEAR PAVEMENT LIFE
3
6
10
15
20
30
40
60
80
(in)
10
15
20
30
40
60
80
100
120
150 180
(cm)
FLEXIBLE PAVEMENT THICKNESS
46x17R20 TIRES
TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
N_AC_070500_1_0050101_01_01
Flexible Pavement Requirements
WV050, MRW 64 400 kg, CG 34 %
FIGURE-7-5-0-991-005-A01
Page 4
May 01/16
7-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
SUBGRADE STRENGTH − CBR
3
6
10
15
20
30
40
60
80
WEIGHT ON ONE MAIN LANDING GEAR
34 750 kg (76 600 lb)
25 000 kg (55 125 lb)
20 000 kg (44 100 lb)
15 000 kg (33 075 lb)
10 000 kg (22 050 lb)
MAXIMUM POSSIBLE
MAIN GEAR LOAD
AT MAXIMUM RAMP
WEIGHT AND AFT CG
10 000 COVERAGES USED
FOR ACN CALCULATIONS
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*
1 200
3 000
6 000
15 000
25 000
*20 YEAR PAVEMENT LIFE
3
6
10
15
20
30
40
60
80
(in)
10
15
20
30
40
60
80
100
120
150 180
(cm)
FLEXIBLE PAVEMENT THICKNESS
46x17R20 TIRES
TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
N_AC_070500_1_0060101_01_00
Flexible Pavement Requirements
WV054, MRW 75 900 kg, CG 36 %
FIGURE-7-5-0-991-006-A01
Page 5
May 01/16
7-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0
Flexible Pavement Requirements - LCN Conversion
**ON A/C A319-100 A319neo
Flexible Pavement Requirements - LCN Conversion
1.
The Load Classification Number (LCN) curves are no longer provided in section 07-06-00 since the
LCN system for reporting pavement strength is obsolete, having been replaced by the ICAO
recommended ACN/PCN system in 1983.
For questions regarding the LCN system, contact Airbus.
Page 1
May 01/16
7-6-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0
Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A319-100 A319neo
Rigid Pavement Requirements - Portland Cement Association Design Method
1.
This section provides data about the rigid pavement requirements for the PCA (Portland Cement
Association) design method.
The rigid pavement requirement graphs are given at standard tire pressure for the weight variants
producing (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG load for
each A/C type.
They are calculated with the PCA design method.
To find a rigid pavement thickness, you must know the Subgrade Modulus (k), the permitted working
stress and the weight on one MLG.
The procedure that follows is used to develop rigid pavement design curves:
-
With the scale for pavement thickness on the left and the scale for permitted working stress on
the right, a random load line is made. This represents the MLG maximum weight to be shown,
-
A plot is then made of all values of the subgrade modulus (k values),
-
More load lines for the incremental values of the weight on the MLG are made based on the
curve for k = 150 MN/m3, which is already shown on the graph.
Example, see FIGURE 7-7-0-991-005-A, calculation of the thickness of the rigid pavement for the
MLG:
-
An aircraft with a MRW of 62 400 kg (137 575 lb),
-
A k value of 150 MN/m3 (550 lbf/in3),
-
A permitted working stress of 31.64 kg/cm2 (450 lb/in2),
-
The load on one MLG is 20 000 kg (44 100 lb).
The required rigid pavement thickness is 186 mm (7 in).
NOTE : The CG in the figure title is the CG used for ACN calculation.
Page 1
May 01/16
7-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
46x17R20 (46x16−20) TIRES
TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
14
1 000
70
MAXIMUM POSSIBLE MAIN
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
34
WEIGHT ON ONE
MAIN LANDING GEAR
13
900
28 530 kg (62 900 lb)
25 000 kg (55 125 lb)
32
60
20 000 kg (44 100 lb)
15 000 kg (33 075 lb)
10 000 kg (22 050 lb)
12
800
30
50
28
11
700
26
10
600
k = 20 MN/m³
k = 40 MN/m³
40
k = 80 MN/m³
24
k = 150 MN/m³
9
500
22
30
8
400
20
18
7
300
20
16
6
200
NOTE:
REFERENCE:
THE VALUES OBTAINED BY USING
"DESIGN OF CONCRETE AIRPORT
THE MAXIMUM LOAD REFERENCE
PAVEMENTS" AND "COMPUTER
LINE AND ANY VALUES FOR k ARE
PROGRAM FOR AIRPORT
EXACT.
PAVEMENT DESIGN − PROGRAM
FOR LOADS LESS THAN MAXIMUM,
PDILB" PORTLAND CEMENT
THE CURVES ARE EXACT FOR k =
ASSOCIATION.
80 MN/m³ BUT DEVIATE SLIGHTLY
FOR ANY OTHER VALUES OF k.
N_AC_070700_1_0050101_01_00
Rigid Pavement Requirements
WV012, MRW 62 400 kg, CG 36 %
FIGURE-7-7-0-991-005-A01
Page 2
May 01/16
7-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
46x17R20 TIRES
TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
38
15
900
60
36
k = 20 MN/m³
14
k = 40 MN/m³
800
k = 80 MN/m³
k = 150 MN/m³
34
MAXIMUM POSSIBLE MAIN
GEAR LOAD AT MAXIMUM
50
13
RAMP WEIGHT AND AFT CG
700
32
12
600
30
40
28
11
500
26
30
10
400
24
9
300
20
22
WEIGHT ON ONE
MAIN LANDING GEAR
8
200
35 180 kg (77 550 lb)
20
25 000 kg (55 125 lb)
20 000 kg (44 100 lb)
15 000 kg (33 075 lb)
10
10 000 kg (22 050 lb)
18
7
100
NOTE:
REFERENCE:
THE VALUES OBTAINED BY USING
"DESIGN OF CONCRETE AIRPORT
THE MAXIMUM LOAD REFERENCE
PAVEMENTS" AND "COMPUTER
LINE AND ANY VALUES FOR k ARE
PROGRAM FOR AIRPORT
EXACT.
PAVEMENT DESIGN − PROGRAM
FOR LOADS LESS THAN MAXIMUM,
PDILB" PORTLAND CEMENT
THE CURVES ARE EXACT FOR k =
ASSOCIATION.
80 MN/m³ BUT DEVIATE SLIGHTLY
FOR ANY OTHER VALUES OF k.
N_AC_070700_1_0060101_01_00
Rigid Pavement Requirements
WV010, MRW 76 900 kg, CG 36 %
FIGURE-7-7-0-991-006-A01
Page 3
May 01/16
7-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
46x17R20 (46x16−20) TIRES
TIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
38
15
900
k = 20 MN/m³
60
k = 40 MN/m³
k = 80 MN/m³
36
k = 150 MN/m³
14
800
34
MAXIMUM POSSIBLE
50
13
MAIN GEAR LOAD
700
AT MAXIMUM RAMP
32
WEIGHT AND AFT CG
12
600
30
40
28
11
500
30
26
10
400
24
9
300
20
22
WEIGHT ON ONE MAIN
LANDING GEAR
29 190 kg (64 350 lb)
8
200
20
25 000 kg (55 125 lb)
20 000 kg (44 100 lb)
15 000 kg (33 075 lb)
10
10 000 kg (22 050 lb)
18
7
100
NOTE:
REFERENCE:
THE VALUES OBTAINED BY USING
"DESIGN OF CONCRETE AIRPORT
THE MAXIMUM LOAD REFERENCE
PAVEMENTS" AND "COMPUTER
LINE AND ANY VALUES FOR k ARE
PROGRAM FOR AIRPORT
EXACT.
PAVEMENT DESIGN − PROGRAM
FOR LOADS LESS THAN MAXIMUM,
PDILB" PORTLAND CEMENT
THE CURVES ARE EXACT FOR k =
ASSOCIATION.
80 MN/m³ BUT DEVIATE SLIGHTLY
FOR ANY OTHER VALUES OF k.
N_AC_070700_1_0070101_01_01
Rigid Pavement Requirements
WV050, MRW 64 400 kg, CG 34 %
FIGURE-7-7-0-991-007-A01
Page 4
May 01/16
7-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
46x17R20 TIRES
MAXIMUM POSSIBLE MAIN
TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
14
1 000
70
WEIGHT ON ONE
MAIN LANDING GEAR
34 750 kg (76 600 lb)
34
25 000 kg (55 125 lb)
20 000 kg (44 100 lb)
13
15 000 kg (33 075 lb)
900
10 000 kg (22 050 lb)
32
60
12
800
30
50
28
11
700
26
10
600
k = 20 MN/m³
k = 40 MN/m³
40
k = 80 MN/m³
24
k = 150 MN/m³
9
500
22
30
8
400
20
18
7
300
20
16
6
200
NOTE:
REFERENCE:
THE VALUES OBTAINED BY USING
"DESIGN OF CONCRETE AIRPORT
THE MAXIMUM LOAD REFERENCE
PAVEMENTS" AND "COMPUTER
LINE AND ANY VALUES FOR k ARE
PROGRAM FOR AIRPORT
EXACT.
PAVEMENT DESIGN − PROGRAM
FOR LOADS LESS THAN MAXIMUM,
PDILB" PORTLAND CEMENT
THE CURVES ARE EXACT FOR k =
ASSOCIATION.
80 MN/m³ BUT DEVIATE SLIGHTLY
FOR ANY OTHER VALUES OF k.
N_AC_070700_1_0080101_01_00
Rigid Pavement Requirements
WV054, MRW 75 900 kg, CG 36 %
FIGURE-7-7-0-991-008-A01
Page 5
May 01/16
7-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-0
Rigid Pavement Requirements - LCN Conversion
**ON A/C A319-100 A319neo
Rigid Pavement Requirements - LCN Conversion
1.
The Load Classification Number (LCN) curves are no longer provided in section 07-08-00 since the
LCN system for reporting pavement strength is obsolete, having been replaced by the ICAO
recommended ACN/PCN system in 1983.
For questions regarding the LCN system, contact Airbus.
Page 1
May 01/16
7-8-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0
ACN/PCN Reporting System - Flexible and Rigid Pavements
**ON A/C A319-100 A319neo
Aircraft Classification Number - Flexible and Rigid Pavements
1.
This section provides data about the Aircraft Classification Number (ACN) for an aircraft gross
weight in relation to a subgrade strength value for flexible and rigid pavement.
The flexible and rigid pavement requirement graphs are given at standard tire pressure for the weight
variants producing (at the MRW and maximum aft CG) the lowest MLG load and the highest MLG
load for each type of aircraft.
To find the ACN of an aircraft on flexible and rigid pavement, you must know the aircraft gross
weight and the subgrade strength.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on that
pavement, subject to any limitation on the tire pressure.
(Ref: ICAO Aerodrome Design Manual, Part 3, Chapter 1, Second Edition 1983).
Example, see FIGURE 7-9-0-991-007-A (sheet 1), calculation of the ACN for flexible pavement for:
-
An aircraft with a MRW of 62 400 kg (137 575 lb),
-
An aircraft gross weight of 55 000 kg (121 250 lb),
-
A low subgrade strength (code C).
The ACN for flexible pavement is 29.
Example, see FIGURE 7-9-0-991-007-A (sheet 2), calculation of the ACN for rigid pavement for:
-
An aircraft with a MRW of 62 400 kg (137 575 lb),
-
An aircraft gross weight of 55 000 kg (121 250 lb),
-
A medium subgrade strength (code B).
The ACN for rigid pavement is 30.
2.
Aircraft Classification Number - ACN table
The tables in FIGURE 7-9-0-991-006-A and FIGURE 7-9-0-991-009-A provide ACN data in tabular
format similar to the one used by ICAO in the ”Aerodrome Design Manual Part 3, Pavements -
Edition 1983” for all the operational weight variants of the aircraft.
As an approximation, use a linear interpolation in order to get the ACN at the required operating
weight using the following equation:
-
ACN = ACN min + (ACN max - ACN min) x (Operating weight - 41 000 kg)/(MRW - 41 000
kg)
As an approximation, also use a linear interpolation in order to get the aircraft weight at the
pavement PCN using the following equation:
-
Operating weight = 41 000 kg + (MRW - 41 000 kg) x (PCN - ACN min)/(ACN max - ACN
min)
With ACN max: ACN calculated at the MRW in the table and with ACN min: ACN calculated at 41
000 kg.
Page 1
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOTE : The CG in the figure title is the CG used for ACN calculation.
Page 2
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
ACN FOR
ACN FOR
LOAD ON
RIGID PAVEMENT
TIRE
FLEXIBLE PAVEMENT
WEIGHT
ALL UP
ONE MAIN
SUBGRADES − MN/m³
SUBGRADES − CBR
PRESSURE
VARIANT
MASS (kg)
GEAR LEG
(MPa)
(%)
High
Medium
Low
Ultra−low
High
Medium
Low
Ultra−low
150
80
40
20
15
10
6
3
A319−100
64 400
45.7
34
37
39
41
32
32
36
41
1.19
WV000 (CG 36%)
41 000
45.7
20
22
23
24
19
19
21
24
A319−100
64 400
46.3
35
37
39
41
32
33
36
42
1.19
WV000 (CG 39%)
41 000
46.3
20
22
23
25
19
19
21
24
A319−100
70 400
46.1
39
42
44
46
35
36
41
46
1.29
WV001 (CG 37.5%)
41 000
46.0
21
22
24
25
19
19
21
24
A319−100
70 400
45.8
39
41
44
46
35
36
40
46
1.29
WV001 (CG 36%)
41 000
45.7
21
22
23
25
19
19
21
24
A319−100
75 900
45.8
44
46
49
51
39
40
45
50
1.38
WV002
41 000
45.7
21
22
24
25
19
19
21
24
A319−100
68 400
46.1
38
40
42
44
34
35
39
45
1.25
WV003 (CG 38.1%)
41 000
46.1
21
22
23
25
19
19
21
24
A319−100
68 400
45.7
37
40
42
44
34
35
39
45
1.25
WV003 (CG 36%)
41 000
45.7
20
22
23
24
19
19
21
24
A319−100
68 400
46.1
38
40
42
44
34
35
39
45
1.25
WV004 (CG 38.1%)
41 000
46.1
21
22
23
25
19
19
21
24
A319−100
68 400
45.7
37
40
42
44
34
35
39
45
1.25
WV004 (CG 36%)
41 000
45.7
20
22
23
24
19
19
21
24
A319−100
70 400
46.1
39
42
44
46
35
36
41
46
1.29
WV005 (CG 37.5%)
41 000
46.0
21
22
24
25
19
19
21
24
A319−100
70 400
45.8
39
41
44
46
35
36
40
46
1.29
WV005 (CG 36%)
41 000
45.7
21
22
23
25
19
19
21
24
A319−100
73 900
45.9
42
44
47
49
37
39
43
49
1.34
WV006 (CG 36.52%)
41 000
45.8
21
22
24
25
19
19
21
24
A319−100
73 900
45.8
42
44
47
49
37
39
43
49
1.34
WV006 (CG 36%)
41 000
45.7
21
22
24
25
19
19
21
24
N_AC_070900_1_0060101_01_00
Aircraft Classification Number
ACN Table (Sheet 1 of 2)
FIGURE-7-9-0-991-006-A01
Page 3
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
ACN FOR
ACN FOR
LOAD ON
RIGID PAVEMENT
FLEXIBLE PAVEMENT
TIRE
SUBGRADES − MN/m³
SUBGRADES − CBR
WEIGHT
ALL UP
ONE MAIN
PRESSURE
VARIANT
MASS (kg)
GEAR LEG
ULTRA
ULTRA
(MPa)
(%)
HIGH
MEDIUM
LOW
HIGH
MEDIUM
LOW
−LOW
−LOW
150
80
40
15
10
6
20
3
A319−100
75 900
45.8
44
46
49
51
39
40
45
50
1.38
WV007
41 000
45.7
21
22
24
25
19
19
21
24
A319−100
64 400
46.3
35
37
39
41
32
33
36
42
1.19
WV008 (CG 39%)
41 000
46.3
20
22
23
25
19
19
21
24
A319−100
64 400
45.7
34
37
39
41
32
32
36
41
1.19
WV008 (CG 36%)
41 000
45.7
20
22
23
24
19
19
21
24
A319−100
66 400
46.3
37
39
41
43
33
34
38
44
1.25
WV009 (CG 38.8%)
41 000
46.2
21
22
24
25
19
19
21
24
A319−100
66 400
45.7
36
38
41
42
33
34
37
43
1.25
WV009 (CG 36%)
41 000
45.7
20
22
23
24
19
19
21
24
A319−100
66 400
46.3
37
39
41
43
33
34
38
44
1.25
WV011 (CG 38.8%)
41 000
46.2
21
22
24
25
19
19
21
24
A319−100
66 400
45.7
36
38
41
42
33
34
37
43
1.25
WV011 (CG 36%)
41 000
45.7
20
22
23
24
19
19
21
24
A319−100
62 400
46.3
33
36
38
40
31
32
35
41
1.19
WV012 (CG 39%)
41 000
46.3
20
22
23
25
19
19
21
24
A319−100
62 400
45.7
33
35
37
39
30
31
34
40
1.19
WV012 (CG 36%)
41 000
45.7
20
22
23
24
19
19
21
24
A319 CJ
75 900
45.8
44
46
49
51
39
40
45
50
1.38
WV002
41 000
45.8
21
22
24
25
19
19
21
24
A319 CJ
70 400
45.8
40
42
44
46
36
37
40
46
1.38
WV005
41 000
45.7
21
22
24
25
19
19
21
24
A319 CJ
76 900
45.7
44
47
49
51
39
41
45
51
1.38
WV010
41 000
45.8
21
22
24
25
19
19
21
24
A319 CJ
75 900
45.8
44
46
49
51
39
40
45
50
1.38
WV013
41 000
45.8
21
22
24
25
19
19
21
24
N_AC_070900_1_0060102_01_01
Aircraft Classification Number
ACN Table (Sheet 2 of 2)
FIGURE-7-9-0-991-006-A01
Page 4
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0070101_01_00
Aircraft Classification Number
Flexible Pavement - WV012, MRW 62 400 kg, CG 36 % (Sheet 1 of 2)
FIGURE-7-9-0-991-007-A01
Page 5
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0070102_01_00
Aircraft Classification Number
Rigid Pavement - WV012, MRW 62 400 kg, CG 36 % (Sheet 2 of 2)
FIGURE-7-9-0-991-007-A01
Page 6
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0080101_01_00
Aircraft Classification Number
Flexible Pavement - WV010, MRW 76 900 kg, CG 36 % (Sheet 1 of 2)
FIGURE-7-9-0-991-008-A01
Page 7
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0080102_01_00
Aircraft Classification Number
Rigid Pavement - WV010, MRW 76 900 kg, CG 36 % (Sheet 2 of 2)
FIGURE-7-9-0-991-008-A01
Page 8
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
ACN FOR
ACN FOR
LOAD ON
RIGID PAVEMENT
FLEXIBLE PAVEMENT
TIRE
SUBGRADES − MN/m³
SUBGRADES − CBR
WEIGHT
ALL UP
ONE MAIN
PRESSURE
VARIANT
MASS (kg)
GEAR LEG
ULTRA
ULTRA
(MPa)
(%)
HIGH
MEDIUM
LOW
HIGH
MEDIUM
LOW
−LOW
−LOW
150
80
40
15
10
6
20
3
A319NEO
64 400
46.3
35
37
39
41
32
33
36
42
1.19
WV050
41 000
46.3
20
22
23
25
19
19
21
24
A319NEO
64 400
45.3
34
36
38
40
31
32
35
41
1.19
WV050 (CG 34%)
41 000
45.3
20
21
23
24
19
19
20
24
A319NEO
64 400
46.3
35
37
39
41
32
33
36
42
1.19
WV051
41 000
46.3
20
22
23
25
19
19
21
24
A319NEO
70 400
46.1
39
42
44
46
35
36
41
46
1.29
WV052
41 000
46.0
21
22
24
25
19
19
21
24
A319NEO
70 400
46.1
39
42
44
46
35
36
41
46
1.29
WV053
41 000
46.0
21
22
24
25
19
19
21
24
A319NEO
75 900
45.8
44
46
49
51
39
40
45
50
1.38
WV054
41 000
45.7
21
22
24
25
19
19
21
24
A319NEO
75 900
45.4
43
46
48
50
38
40
44
50
1.38
WV054 (CG 34%)
41 000
45.3
21
22
24
25
19
19
21
24
A319NEO
75 900
45.8
44
46
49
51
39
40
45
50
1.38
WV055
41 000
45.7
21
22
24
25
19
19
21
24
A319NEO
75 900
45.4
43
46
48
50
38
40
44
50
1.38
WV055 (CG 34%)
41 000
45.3
21
22
24
25
19
19
21
24
N_AC_070900_1_0090101_01_01
Aircraft Classification Number
ACN Table
FIGURE-7-9-0-991-009-A01
Page 9
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0100101_01_01
Aircraft Classification Number
Flexible Pavement - WV050, MRW 64 400 kg, CG 34 % (Sheet 1 of 2)
FIGURE-7-9-0-991-010-A01
Page 10
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0100102_01_01
Aircraft Classification Number
Rigid Pavement - WV050, MRW 64 400 kg, CG 34 % (Sheet 2 of 2)
FIGURE-7-9-0-991-010-A01
Page 11
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0110101_01_00
Aircraft Classification Number
Flexible Pavement - WV054, MRW 75 900 kg, CG 36 % (Sheet 1 of 2)
FIGURE-7-9-0-991-011-A01
Page 12
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070900_1_0110102_01_00
Aircraft Classification Number
Rigid Pavement - WV054, MRW 75 900 kg, CG 36 % (Sheet 2 of 2)
FIGURE-7-9-0-991-011-A01
Page 13
May 01/16
7-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0
SCALED DRAWINGS
**ON A/C A319-100 A319neo
Scaled Drawings
1.
This section provides the scaled drawings.
NOTE : When printing this drawing, make sure to adjust for proper scaling.
Page 1
May 01/16
8-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FEET
0
10
20
30
40
50
0
5
10
15
METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.
N_AC_080000_1_0020101_01_00
Scaled Drawing
FIGURE-8-0-0-991-002-A01
Page 2
May 01/16
8-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
FEET
0
10
20
30
40
50
0
5
10
15
METERS
NOTE:
WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.
N_AC_080000_1_0050101_01_00
Scaled Drawing
FIGURE-8-0-0-991-005-A01
Page 3
May 01/16
8-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0
AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A319-100 A319neo
Aircraft Rescue and Fire Fighting
1.
Aircraft Rescue and Fire Fighting Charts
This sections provides data related to aircraft rescue and fire fighting.
The figures contained in this section are the figures that are in the Aircraft Rescue and Fire Fighting
Charts poster available for download on AIRBUSWorld and the Airbus website.
Page 1
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0170101_01_03
Front Page
FIGURE-10-0-0-991-017-A01
Page 2
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0180101_01_01
Highly Flammable and Hazardous Materials and Components
FIGURE-10-0-0-991-018-A01
Page 3
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0560101_01_01
Batteries Location and Access
FIGURE-10-0-0-991-056-A01
Page 4
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0190101_01_01
Wheel/Brake Overheat
Wheel Safety Area (Sheet 1 of 2)
FIGURE-10-0-0-991-019-A01
Page 5
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0190102_01_00
Wheel/Brake Overheat
Recommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-019-A01
Page 6
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10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0200101_01_00
Composite Materials
FIGURE-10-0-0-991-020-A01
Page 7
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0210101_01_00
L/G Ground Lock Safety Devices
FIGURE-10-0-0-991-021-A01
Page 8
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0220101_01_02
Emergency Evacuation Devices
FIGURE-10-0-0-991-022-A01
Page 9
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0230101_01_00
Pax/Crew Doors
FIGURE-10-0-0-991-023-A01
Page 10
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0240101_01_00
Emergency Exit Hatch
FIGURE-10-0-0-991-024-A01
Page 11
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0250101_01_00
FWD and AFT Lower Deck Cargo Doors
FIGURE-10-0-0-991-025-A01
Page 12
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0260101_01_00
Control Panels
FIGURE-10-0-0-991-026-A01
Page 13
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0270101_01_00
APU Access Door
FIGURE-10-0-0-991-027-A01
Page 14
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0280101_01_01
Aircraft Ground Clearances
FIGURE-10-0-0-991-028-A01
Page 15
May 01/16
10-0-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
N_AC_100000_1_0290101_01_00
Structural Break-in Points
FIGURE-10-0-0-991-029-A01
Page 16
May 01/16
10-0-0

 

 

 

 

 

 

 

 

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