Airbus A319. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016) - page 2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0
Visibility from Cockpit in Static Position
**ON A/C A319-100 A319neo
Visibility from Cockpit in Static Position
1.
This section gives the visibility from cockpit in static position.
Page 1
May 01/16
4-4-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
May 01/16
4-4-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0
Runway and Taxiway Turn Paths
**ON A/C A319-100 A319neo
Runway and Taxiway Turn Paths
1.
Runway and Taxiway Turn Paths.
Page 1
May 01/16
4-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1
135˚ Turn - Runway to Taxiway
**ON A/C A319-100 A319neo
135˚ Turn - Runway to Taxiway
1.
This section gives the 135˚ turn - runway to taxiway.
Page 1
May 01/16
4-5-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
APPROX 5.1 m
(17 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_0020101_01_02
135˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-1-991-002-A01
Page 2
May 01/16
4-5-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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_0030101_01_02
135˚ Turn - Runway to Taxiway
Judgemental Oversteering Method
FIGURE-4-5-1-991-003-A01
Page 3
May 01/16
4-5-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2
90˚ Turn - Runway to Taxiway
**ON A/C A319-100 A319neo
90˚ Turn - Runway to Taxiway
1.
This section gives the 90˚ turn - runway to taxiway.
Page 1
May 01/16
4-5-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 6.4 m
(21 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_0020101_01_01
90˚ Turn - Runway to Taxiway
Cockpit Over Centerline Method
FIGURE-4-5-2-991-002-A01
Page 2
May 01/16
4-5-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 9 m
(29 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_0030101_01_01
90˚ Turn - Runway to Taxiway
Judgemental Oversteering Method
FIGURE-4-5-2-991-003-A01
Page 3
May 01/16
4-5-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3
180˚ Turn on a Runway
**ON A/C A319-100 A319neo
180˚ Turn on a Runway
1.
This section provides the 180˚ turn on a runway.
Page 1
May 01/16
4-5-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
RUNWAY CENTERLINE
6.6 m
(22 ft)
3 m
(10 ft)
R3 = 11.7 m
(39 ft)
R5 = 16.5 m
(55 ft)
NLG PATH
R4
WINGTIP PATH:
WINGTIP FENCES:
R4 = 21.1 m (70 ft)
SHARKLETS:
R4 = 22 m (72 ft)
NOSE PATH
MLG PATH
30 m
(100 ft)
NOTE:
TYPE 1 VALUES.
N_AC_040503_1_0010101_01_03
180˚ Turn on a Runway
Edge of Runway Method (Sheet 1 of 2)
FIGURE-4-5-3-991-001-A01
Page 2
May 01/16
4-5-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
RUNWAY CENTERLINE
R5 = 16.5 m
(55 ft)
R4
R3 = 11.7 m
(38 ft)
4.75 m
(16 ft)
5.22 m
(17 ft)
NLG PATH
WINGTIP PATH:
WINGTIP FENCES:
25°
R4 = 21.1 m (70 ft)
SHARKLETS:
R4 = 22 m (72 ft)
NOSE PATH
MLG PATH
30 m
(100 ft)
NOTE:
TYPE 1 VALUES.
N_AC_040503_1_0010102_01_01
180˚ Turn on a Runway
Center of Runway Method (Sheet 2 of 2)
FIGURE-4-5-3-991-001-A01
Page 3
May 01/16
4-5-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4
135˚ Turn - Taxiway to Taxiway
**ON A/C A319-100 A319neo
135˚ Turn - Taxiway to Taxiway
1.
This section gives the 135˚ turn - taxiway to taxiway.
Page 1
May 01/16
4-5-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
APPROX 5.8 m
(19 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_0050101_01_00
135˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-4-991-005-A01
Page 2
May 01/16
4-5-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
APPROX 3.3 m
(11ft)
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_0050102_01_00
135˚ Turn - Taxiway to Taxiway
Judgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-4-991-005-A01
Page 3
May 01/16
4-5-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5
90˚ Turn - Taxiway to Taxiway
**ON A/C A319-100 A319neo
90˚ Turn - Taxiway to Taxiway
1.
This section gives the 90˚ turn - taxiway to taxiway.
Page 1
May 01/16
4-5-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 6.1 m
TAXIWAY CENTERLINE
(20 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_0030101_01_00
90˚ Turn - Taxiway to Taxiway
Cockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-5-991-003-A01
Page 2
May 01/16
4-5-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FAA LEAD−IN FILLET
L = 45 m (150 ft)
15 m
(50 ft)
APPROX 9 m
TAXIWAY CENTERLINE
(29 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_0030102_01_00
90˚ Turn - Taxiway to Taxiway
Judgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-5-991-003-A01
Page 3
May 01/16
4-5-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0
Runway Holding Bay (Apron)
**ON A/C A319-100 A319neo
Runway Holding Bay (Apron)
1.
This section gives the runway holding bay (Apron).
Page 1
May 01/16
4-6-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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: LAYOUT IN ACCORDANCE WITH THE REQUIREMENTS OF NAS 3601, CHAPTER 4,
AND AN/865, CHAPTER 3.
OUTER PARKED AIRCRAFT TURNED THRU MIN. TURN RADIUS TO PARKED POSITION.
N_AC_040600_1_0020101_01_02
Runway Holding Bay (Apron)
FIGURE-4-6-0-991-002-A01
Page 2
May 01/16
4-6-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0
Minimum Line-Up Distance Corrections
**ON A/C A319-100 A319neo
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 4-7-0-991-017-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 4-7-0-991-018-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 4-7-0-991-019-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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
3 m
(10 ft)
TODA
ASDA
TAXIWAY
> 3 m
CENTERLINE
(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
MAX
AIRCRAFT
STEERING
MINIMUM LINE−UP
TYPE
ANGLE
DISTANCE CORRECTION
ON TODA
ON ASDA
A319
75°
11.1 m
36 ft
22.1 m
73 ft
N_AC_040700_1_0170101_01_00
Minimum Line-Up Distance Corrections
90˚ Turn on Runway Entry
FIGURE-4-7-0-991-017-A01
Page 2
May 01/16
4-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
MINIMUM PAVEMENT WIDTH
3 m
(10 ft)
> 3 m
3 m
TODA
(10 ft)
(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
A319
75°
15.0 m
49 ft
26.0 m
85 ft
29.7 m
97 ft
N_AC_040700_1_0180101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Turn Pad
FIGURE-4-7-0-991-018-A01
Page 3
May 01/16
4-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
A319
75°
15.0 m
49 ft
26.0 m
85 ft
N_AC_040700_1_0190101_01_00
Minimum Line-Up Distance Corrections
180˚ Turn on Runway Width
FIGURE-4-7-0-991-019-A01
Page 4
May 01/16
4-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-8-0
Aircraft Mooring
**ON A/C A319-100 A319neo
Aircraft Mooring
1.
This section provides information on aircraft mooring.
Page 1
May 01/16
4-8-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-1-1
Aircraft Servicing Arrangements
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2
Typical Ramp Layout - Open Apron
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FEET
0
5
10 15 20
0
2
4
6
8
METERS
AS
TOW
BULK
CAT
CB
FUEL
BULK
CB
LV
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUT
APPLICABLE TO AIRCRAFT
WITH OR WITHOUT SHARKLETS.
N_AC_050102_1_0020101_01_03
Typical Ramp Layout
Open Apron - Bulk Loading
FIGURE-5-1-2-991-002-A01
Page 2
May 01/16
5-1-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FEET
0
5
10 15 20
0
2
4
6
8
METERS
AS
TOW
ULD
CAT
LD CL
FUEL
ULD
LD CL
LV
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUT
APPLICABLE TO AIRCRAFT
WITH OR WITHOUT SHARKLETS.
N_AC_050102_1_0080101_01_00
Typical Ramp Layout
Open Apron - ULD Loading
FIGURE-5-1-2-991-008-A01
Page 3
May 01/16
5-1-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3
Typical Ramp Layout - Gate
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
FEET
0
5
10 15 20
0
2
4
6
8
METERS
AS
TOW
ULD
CAT
LD CL
FUEL
ULD
LD CL
LV
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUT
APPLICABLE TO AIRCRAFT
WITH OR WITHOUT SHARKLETS.
N_AC_050103_1_0010101_01_03
Typical Ramp Layout
Gate
FIGURE-5-1-3-991-001-A01
Page 2
May 01/16
5-1-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0
Terminal Operations - Full Servicing Turn Round Time Chart
**ON A/C A319-100 A319neo
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
124 pax: 8 F/C + 116 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:
-
124 pax at door L1
-
Deplaning rate = 20 pax/min per door
-
Priority deplaning for premium passengers.
Boarding:
-
124 pax at door L1
-
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: 2 containers
-
AFT cargo compartment: 2 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:
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5-2-0
@A319
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: 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
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@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
TRT: 37 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
BULK
REFUELING
POTABLE WATER SERVICING
TOILET SERVICING
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
N_AC_050200_1_0050101_01_02
Full Servicing Turn Round Time Chart
FIGURE-5-2-0-991-005-A01
Page 3
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5-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0
Terminal Operation - Outstation Turn Round Time Chart
**ON A/C A319-100 A319neo
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
156 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:
-
78 pax at door L1
-
78 pax at door L2
-
Deplaning rate = 18 pax/min per door.
Boarding:
-
78 pax at door L1
-
78 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: 2 containers
-
AFT cargo compartment: 2 containers.
Container unloading/loading times:
-
Unloading = 1.5 min/container
-
Loading = 1.5 min/container.
C.
REFUELING
No refueling.
Page 1
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@A319
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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_0020101_01_02
Outstation Turn Round Time Chart
FIGURE-5-3-0-991-002-A01
Page 3
May 01/16
5-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1
Ground Service Connections
**ON A/C A319-100 A319neo
Ground Service Connections Layout
1.
This section provides the ground service connections layout.
Page 1
May 01/16
5-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
2
10
12
13
9
11
7
8
1
3
10
4
5
18
9
6
8
11
15
16
12
14
18
14
1715
13
20
10
19
10
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_0020101_01_02
Ground Service Connections Layout
FIGURE-5-4-1-991-002-A01
Page 2
May 01/16
5-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2
Grounding Points
**ON A/C A319-100 A319neo
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
16.11 m
3.79 m
1.07 m
-
Gear leg:
(52.85 ft)
(12.43 ft)
(3.51 ft)
On right Main Landing
16.11 m
3.79 m
1.07 m
-
Gear leg:
(52.85 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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
A
NOSE LANDING GEAR
MAIN LANDING GEAR
LANDING
GEAR
GROUNDING (EARTHING) POINT
GROUNDING (EARTHING) CABLE
A
TYPICAL
N_AC_050402_1_0030101_01_01
Ground Service Connections
Grounding (Earthing) Points - Landing Gear
FIGURE-5-4-2-991-003-A01
Page 2
May 01/16
5-4-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
A
RIB20
RIB19
B
A
FOR SPECIFICATIONS REFER
TO FLIGHT MANUAL
NOTE: R SIDE SYMMETRICAL
F
W
B
D
N_AC_050402_1_0040101_01_00
Ground Service Connections
Grounding (Earthing) Points - Wing (If Installed)
FIGURE-5-4-2-991-004-A01
Page 3
May 01/16
5-4-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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_0120101_01_00
Ground Service Connections
Grounding (Earthing) Point - Avionics Compartment Door-Frame
FIGURE-5-4-2-991-012-A01
Page 4
May 01/16
5-4-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
A
PHONE JACK
GROUNDING (EARTHING) POINT
A
N_AC_050402_1_0130101_01_00
Ground Service Connections
Grounding (Earthing) Point - Engine Air Intake (If Installed)
FIGURE-5-4-2-991-013-A01
Page 5
May 01/16
5-4-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3
Hydraulic System
**ON A/C A319-100 A319neo
Hydraulic Servicing
1.
Access
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Green System:
17.57 m
1.27 m
1.76 m
Access Door 197CB
(57.64 ft)
(4.17 ft)
(5.77 ft)
Yellow System:
17.57 m
1.27 m
1.76 m
Access Door 198CB
(57.64 ft)
(4.17 ft)
(5.77 ft)
Blue System:
18.92 m
1.27 m
1.76 m
Access Door 197EB
(60.07 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
14.05 m
0.25 m
1.74 m
Access Door 195BB
(46.10 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
14.05 m
0.25 m
1.74 m
Accumulator:
(46.10 ft)
(0.82 ft)
(5.71 ft)
Access Door 196BB
Page 1
May 01/16
5-4-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Green System
15.67 m
0.25 m
3.20 m
Accumulator:
(51.41 ft)
(0.82 ft)
(10.50 ft)
Left MLG Door
Blue System
14.05 m
0.25 m
1.74 m
Accumulator:
(46.10 ft)
(0.82 ft)
(5.71 ft)
Access Door 195BB
Yellow System Braking
14.05 m
0.25 m
1.74 m
Accumulator:
(46.10 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
17.57 m
1.27 m
1.76 m
Access Door 197CB
(57.64 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:
14.05 m
0.25 m
1.74 m
Access Door 196BB
(46.10 ft)
(0.82 ft)
(5.71 ft)
Green System:
15.67 m
0.25 m
3.20 m
Left MLG Door
(51.41 ft)
(0.82 ft)
(10.50 ft)
Page 2
May 01/16
5-4-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCE
FROM AIRCRAFT CENTERLINE
MEAN HEIGHT
ACCESS
AFT OF NOSE
FROM
LH SIDE
RH SIDE
GROUND
Blue System:
18.92 m
1.27 m
1.76 m
Access Door 197EB
(62.07 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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4
Electrical System
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5
Oxygen System
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6
Fuel System
**ON A/C A319-100 A319neo
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:
14.8 m
1.8 m
1.8 m
-
Access Door
(48.56 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:
15.99 m
9.83 m
3.65 m
Access Panel
-
(52.46 ft)
(32.25 ft)
(11.98 ft)
522HB
(Optional)
Refuel/Defuel
Coupling, Right:
15.99 m
9.83 m
3.65 m
-
Access Panel
(52.46 ft)
(32.25 ft)
(11.98 ft)
622HB
Overwing Gravity-
17.5 m
12.4 m
12.4 m
3.7 m
Refuel Cap
(57.41 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
@A319
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-
18.76 m
14.9 m
14.9 m
4.32 m
Protector:
(61.55 ft)
(48.88 ft)
(48.88 ft)
(14.17 ft)
Access Panel
550CB (650CB)
Inner Cell
Overpressure-
17.5 m
9.19 m
9.19 m
4.1 m
Protector:
(57.41 ft)
(30.15 ft)
(30.15 ft)
(13.45 ft)
Access Panel
540HB (640HB)
NACA Vent Intake:
18.2 m
13.7 m
13.7 m
4.02 m
Access Panel
(59.71 ft)
(44.95 ft)
(44.95 ft)
(13.19 ft)
550AB (650AB)
NOTE : Distances are approximate.
Page 2
May 01/16
5-4-6
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7
Pneumatic System
**ON A/C A319-100 A319neo
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:
11.38 m
0.84 m
1.76 m
-
Access Door 191DB
(37.34 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:
10.85 m
1.11 m
1.73 m
-
Access Door 191CB
(35.6 ft)
(3.64 ft)
(5.68 ft)
A. Connector:
-
One standard 8 in. SAE AS4262 connection.
Page 1
May 01/16
5-4-7
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8
Oil System
**ON A/C A319-100 A319neo
Oil System
**ON A/C A319-100
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:
11.56 m
6.63 m
4.82 m
1.46 m
Access door: 437BL
(37.93 ft)
(21.75 ft)
(15.81 ft)
(4.79 ft)
(LH),
447BL (RH)
Engine Oil Pressure
11.40 m
6.49 m
4.74 m
1.42 m
Filling Port:
(37.40 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:
10.60 m
6.90 m
5.52 m
0.68 m
Access door: 438AR
(34.78 ft)
(22.64 ft)
(18.11 ft)
(2.23 ft)
(LH),
448AR (RH)
Page 1
May 01/16
5-4-8
@A319
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
11.40 m
5.30 m
6.20 m
0.76 m
Connection:
(37.40 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:
10.64 m
6.56 m
4.92 m
1.22 m
Access door: 437BL
(34.91 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: OMP 2506-2 plus one overflow connection: OMP 2505-2.
Page 2
May 01/16
5-4-8
@A319
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
11.04 m
5.30 m
6.14 m
0.75 m
Connection:
(36.22 ft)
(17.39 ft)
(20.14 ft)
(2.46 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
11.04 m
5.30 m
6.14 m
0.75 m
Connection:
(36.22 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 A319-100 A319neo
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
31.76 m
0.30 m
4.83 m
-
GTCP 36-300
(104.20 ft)
(0.98 ft)
(15.85 ft)
31.76 m
0.30 m
4.78 m
-
APS 3200
(104.20 ft)
(0.98 ft)
(15.68 ft)
31.66 m
0.35 m
4.32 m
-
131-9
(103.87 ft)
(1.15 ft)
(14.17 ft)
NOTE : Distances are approximate.
Page 3
May 01/16
5-4-8
@A319
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
May 01/16
5-4-8
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
May 01/16
5-4-8
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
May 01/16
5-4-8
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
May 01/16
5-4-8
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9
Potable Water System
**ON A/C A319-100 A319neo
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
27.5 m
0.3 m
2.6 m
-
Service Panel:
(90.22 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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10
Waste Water System
**ON A/C A319-100 A319neo
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
27.5 m
0.8 m
2.8 m
-
Panel:
(90.22 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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0
Engine Starting Pneumatic Requirements
**ON A/C A319-100 A319neo
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
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
40
45
50
ABSOLUTE PRESSURE (psia)
50
45
40
−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 20° C (68° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 150° C (302° F)
AT HPGC:
− THE REQUIRED PRESSURE AT HPGC IS 42 psia
− THE REQUIRED AIRFLOW AT A/C CONNECTION IS 55 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_0080101_01_00
Example for Use of the Charts
FIGURE-5-5-0-991-008-A01
Page 2
May 01/16
5-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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_0090101_01_00
Engine Starting Pneumatic Requirements
IAE V2500 Series Engine
FIGURE-5-5-0-991-009-A01
Page 3
May 01/16
5-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
40
45
50
ABSOLUTE PRESSURE (psia)
50
45
40
−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_0100101_01_00
Engine Starting Pneumatic Requirements
CFM56 Series and CFM LEAP-1A NEO Engine
FIGURE-5-5-0-991-010-A01
Page 4
May 01/16
5-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
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_0110101_01_00
Engine Starting Pneumatic Requirements
PW 1100G NEO Engine
FIGURE-5-5-0-991-011-A01
Page 5
May 01/16
5-5-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0
Ground Pneumatic Power Requirements
**ON A/C A319-100 A319neo
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).
Page 1
May 01/16
5-6-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
Page 2
May 01/16
5-6-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
Page 3
May 01/16
5-6-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0
Preconditioned Airflow Requirements
**ON A/C A319-100 A319neo
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).
Page 1
May 01/16
5-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
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
FOR OPERATION
C
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 −38° C ( −36.4° F); EMPTY CABIN; IFE OFF; LIGHTS ON; NO SOLAR LOAD; RECIRCULATION
FANS ON; GALLEYS OFF
N_AC_050700_1_0010101_01_04
Preconditioned Airflow Requirements
FIGURE-5-7-0-991-001-A01
Page 2
May 01/16
5-7-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0
Ground Towing Requirements
**ON A/C A319-100 A319neo
Ground Towing Requirements
1.
This section provides information on aircraft towing.
This aircraft is designed with means for conventional or towbarless towing. Information/procedures
can be found for both in AMM 09.
Status on towbarless towing equipment qualification can be found in ISI 09.11.00001.
One towbar fitting is installed at the front of the leg.
The main landing gears have attachment points for towing or debogging (for details, refer ARM 07).
This section shows the chart to determine the drawbar pull and tow tractor mass requirements as a
function of the following physical characteristics:
-
Aircraft weight,
-
Number of engines at idle,
-
Slope.
The chart is based on the engine type with the highest idle thrust level.
2.
Towbar design guidelines
The aircraft towbar shall comply with the following standards:
-
ISO 8267-1, ”Aircraft - Towbar Attachment Fitting - Interface Requirements - Part 1: Main Line
Aircraft”,
-
SAE AS 1614, ”Main Line Aircraft Towbar Attach Fitting Interface”,
-
SAE ARP 1915, ”Aircraft Towbar”,
-
ISO 9667, ”Aircraft Ground Support Equipment - Towbar - Connection to Aircraft and Tractor”,
-
EN 12312-7, ”Aircraft Ground Support Equipment - Specific Requirements - Part 7: Aircraft
Movement Equipment”,
-
IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Towbar”.
A conventional type towbar is required which should be equipped with a damping system (to protect
the nose gear against jerks) and with towing shear pins:
-
A traction shear pin calibrated at 9 425 daN (21 188 lbf),
-
A torsion pin calibrated at 826 m.daN (6 092 lbf.ft).
The towing head is designed according to ISO 8267-1, cat. I.
Page 1
May 01/16
5-8-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
10
BREAKAWAY RESISTANCE 4%
# OF ENGINES ON FOR PB: 1
ENGINE THRUST 525 daN
70
60
65
1.5% SLOPE
60
5.0
1 ENGINE ON
55
5
50
45
40
8.83
0
0
10
20
30
40
50
60
70
80
0
1
2
0
0.5
1.0
1.5
2.0
TOTAL TRACTION WHEEL LOAD (x 1 000 kg)
No. OF ENGINES
SLOPE ( % )
AT IDLE
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A319 AT 60 000 kg, AT 1.5% SLOPE,
1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (60 000 kg),
− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),
− FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 2,
− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED No. OF ENGINES (1),
− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,
− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5 000 kg),
− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE.
THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (8 830 kg).
N_AC_050800_1_0010201_01_04
Ground Towing Requirements
FIGURE-5-8-0-991-001-B01
Page 2
May 01/16
5-8-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0
De-Icing and External Cleaning
**ON A/C A319-100 A319neo
De-Icing and External Cleaning
1.
De-Icing and External Cleaning on Ground
The mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heights
up to approximately 13 m (43 ft).
2.
De-Icing
Wingtip Devices
Wing Top Surface
(Both Inside and
HTP Top Surface
VTP
AIRCRAFT TYPE
(Both Sides)
Outside Surfaces)
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
m2
ft2
A319
100
1 076
2
22
27
291
43
463
A319 Sharklet/neo
100
1 076
10
108
27
291
43
463
Nacelle and Pylon
Fuselage Top Surface
(Top Third - 120˚ Arc)
Total De-Iced Area
AIRCRAFT TYPE
(Top Third - 120˚ Arc)
(All Engines)
m2
ft2
m2
ft2
m2
ft2
A319
122
1 313
24
258
317
3 412
A319 Sharklet/neo
122
1 313
24
258
325
3 498
NOTE : Dimensions are approximate.
3.
External Cleaning
Wing Lower Surface
Wingtip Devices
Wing Top Surface
(Including Flap Track
(Both Inside and
AIRCRAFT TYPE
(Both Sides)
Fairing)
Outside Surfaces)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A319
100
1 076
103
1 109
2
22
A319 Sharklet/neo
100
1 076
103
1 109
10
108
HTP Top Surface
HTP Lower Surface
VTP
AIRCRAFT TYPE
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A319
27
291
27
291
43
463
Page 1
May 01/16
5-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HTP Top Surface
HTP Lower Surface
VTP
AIRCRAFT TYPE
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A319 Sharklet/neo
27
291
27
291
43
463
Fuselage and
Nacelle and Pylon
Total Cleaned Area
AIRCRAFT TYPE
Belly Fairing
(All Engines)
m2
ft2
m2
ft2
m2
ft2
A319
374
4 026
73
786
750
8 073
A319 Sharklet/neo
374
4 026
73
786
758
8 159
NOTE : Dimensions are approximate.
Page 2
May 01/16
5-9-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0
Engine Exhaust Velocities and Temperatures
**ON A/C A319-100 A319neo
Engine Exhaust Velocities and Temperatures
**ON A/C A319-100
1.
General
This section provides the estimated engine exhaust efflux velocities and temperatures contours for
Ground Idle, Breakaway and Maximum Take-Off (MTO) conditions.
**ON A/C A319neo
2.
General
This section provides the estimated engine exhaust velocity and temperature contours for MTO,
Breakaway 12% MTO, Breakaway 24% MTO and Ground Idle conditions for the CFM LEAP-1A and
PW 1100G engines.
The MTO data are presented at the maximum thrust rating. The Breakaway data are presented at a
rating that corresponds to the minimum thrust level necessary to start the movement of the A/C
from a static position at its maximum ramp weight. Breakaway thrust corresponds to 12% MTO if
applied on both engines and 24% MTO when applied on a single engine (Idle thrust on the other
engine).
The Idle data, provided by the engine manufacturer, are calculated for operational conditions ISA
+15K (+15˚C), Sea Level, Static and no headwind. In the charts, the longitudinal distances are
measured from the inboard engine core-nozzle exit section. The lateral distances are measured from
the aircraft fuselage centerline.
The effects of on-wing installation are not taken into account. The effects of ground proximity are
not taken into account for PW 1100G engines, but they are taken into account for the CFM
LEAP-1A engines.
The velocity contours are presented at 50 ft/s (15 m/s), 100 ft/s (30 m/s) and 150 ft/s (46 m/s).
The temperature contours are shown at 313K (+40˚C), 323K (+50˚C) and 333K (+60˚C). The
velocity and temperature contours do not take into account possible variations affecting performance,
such as ambient temperature, field elevation or failure cases leading to an abnormal bleed
configuration. To evaluate the impact of these specific variables on the exhaust contours, a specific
study of the airport where the aircraft is intended to operate should be carried out.
Page 1
May 01/16
6-1-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A319-100 A319neo
Engine Exhaust Velocities Contours - Ground Idle Power
1.
This section provides engine exhaust velocities contours at ground idle power.
Page 1
May 01/16
6-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060101_1_0030101_01_01
Engine Exhaust Velocities
Ground Idle Power -- CFM56 Series Engine
FIGURE-6-1-1-991-003-A01
Page 2
May 01/16
6-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060101_1_0040101_01_00
Engine Exhaust Velocities
Ground Idle Power -- IAE V2500 Series Engine
FIGURE-6-1-1-991-004-A01
Page 3
May 01/16
6-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060101_1_0090101_01_00
Engine Exhaust Velocities
Ground Idle Power -- CFM LEAP-1A Engine
FIGURE-6-1-1-991-009-A01
Page 4
May 01/16
6-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060101_1_0100101_01_00
Engine Exhaust Velocities
Ground Idle Power -- PW 1100G Engine
FIGURE-6-1-1-991-010-A01
Page 5
May 01/16
6-1-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A319-100 A319neo
Engine Exhaust Temperatures Contours - Ground Idle Power
1.
This section provides engine exhaust temperatures contours at ground idle power.
Page 1
May 01/16
6-1-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060102_1_0030101_01_01
Engine Exhaust Temperatures
Ground Idle Power -- CFM56 Series Engine
FIGURE-6-1-2-991-003-A01
Page 2
May 01/16
6-1-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060102_1_0040101_01_01
Engine Exhaust Temperatures
Ground Idle Power -- IAE V2500 Series Engine
FIGURE-6-1-2-991-004-A01
Page 3
May 01/16
6-1-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060102_1_0090101_01_00
Engine Exhaust Temperatures
Ground Idle Power -- CFM LEAP-1A Engine
FIGURE-6-1-2-991-009-A01
Page 4
May 01/16
6-1-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060102_1_0100101_01_00
Engine Exhaust Temperatures
Ground Idle Power -- PW 1100G Engine
FIGURE-6-1-2-991-010-A01
Page 5
May 01/16
6-1-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A319neo
Engine Exhaust Velocities Contours - Breakaway Power
1.
This section provides engine exhaust velocities contours at breakaway power.
Page 1
May 01/16
6-1-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060103_1_0090101_01_00
Engine Exhaust Velocities
Breakaway Power 12% MTO -- CFM LEAP-1A Engine
FIGURE-6-1-3-991-009-A01
Page 2
May 01/16
6-1-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060103_1_0100101_01_00
Engine Exhaust Velocities
Breakaway Power 12% MTO -- PW 1100G Engine
FIGURE-6-1-3-991-010-A01
Page 3
May 01/16
6-1-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060103_1_0170101_01_00
Engine Exhaust Velocities
Breakaway Power 24% MTO -- CFM LEAP-1A Engine
FIGURE-6-1-3-991-017-A01
Page 4
May 01/16
6-1-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060103_1_0180101_01_00
Engine Exhaust Velocities
Breakaway Power 24% MTO -- PW 1100G Engine
FIGURE-6-1-3-991-018-A01
Page 5
May 01/16
6-1-3
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A319neo
Engine Exhaust Temperatures Contours - Breakaway Power
1.
This section provides engine exhaust temperatures contours at breakaway power.
Page 1
May 01/16
6-1-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060104_1_0130101_01_00
Engine Exhaust Temperatures
Breakaway Power 12% MTO - CFM LEAP-1A Engine
FIGURE-6-1-4-991-013-A01
Page 2
May 01/16
6-1-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060104_1_0140101_01_00
Engine Exhaust Temperatures
Breakaway Power 12% MTO - PW 1100G Engine
FIGURE-6-1-4-991-014-A01
Page 3
May 01/16
6-1-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060104_1_0150101_01_00
Engine Exhaust Temperatures
Breakaway Power 24% MTO - CFM LEAP-1A Engine
FIGURE-6-1-4-991-015-A01
Page 4
May 01/16
6-1-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060104_1_0160101_01_00
Engine Exhaust Temperatures
Breakaway Power 24% MTO - PW 1100G Engine
FIGURE-6-1-4-991-016-A01
Page 5
May 01/16
6-1-4
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5
Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A319-100 A319neo
Engine Exhaust Velocities Contours - Takeoff Power
1.
This section provides engine exhaust velocities contours at takeoff power.
Page 1
May 01/16
6-1-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060105_1_0030101_01_01
Engine Exhaust Velocities
Takeoff Power -- CFM56 Series Engine
FIGURE-6-1-5-991-003-A01
Page 2
May 01/16
6-1-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060105_1_0040101_01_00
Engine Exhaust Velocities
Takeoff Power -- IAE V2500 Series Engine
FIGURE-6-1-5-991-004-A01
Page 3
May 01/16
6-1-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060105_1_0090101_01_00
Engine Exhaust Velocities
Takeoff Power -- CFM LEAP-1A Engine
FIGURE-6-1-5-991-009-A01
Page 4
May 01/16
6-1-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060105_1_0100101_01_00
Engine Exhaust Velocities
Takeoff Power -- PW 1100G Engine
FIGURE-6-1-5-991-010-A01
Page 5
May 01/16
6-1-5
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A319-100 A319neo
Engine Exhaust Temperatures Contours - Takeoff Power
1.
This section provides engine exhaust temperatures contours at takeoff power.
Page 1
May 01/16
6-1-6
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060106_1_0030101_01_01
Engine Exhaust Temperatures
Takeoff Power -- CFM56 Series Engine
FIGURE-6-1-6-991-003-A01
Page 2
May 01/16
6-1-6
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_060106_1_0040101_01_01
Engine Exhaust Temperatures
Takeoff Power -- IAE V2500 Series Engine
FIGURE-6-1-6-991-004-A01
Page 3
May 01/16
6-1-6
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060106_1_0090101_01_00
Engine Exhaust Temperatures
Takeoff Power -- CFM LEAP-1A Engine
FIGURE-6-1-6-991-009-A01
Page 4
May 01/16
6-1-6
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
N_AC_060106_1_0100101_01_00
Engine Exhaust Temperatures
Takeoff Power -- PW 1100G Engine
FIGURE-6-1-6-991-010-A01
Page 5
May 01/16
6-1-6
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0
Danger Areas of Engines
**ON A/C A319-100
Danger Areas of Engines
1.
Danger Areas of the Engines.
Page 1
May 01/16
6-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1
Ground Idle Power
**ON A/C A319-100 A319neo
Ground Idle Power
1.
This section provides danger areas of the engines at ground idle power conditions.
Page 1
May 01/16
6-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RADIUS = 15 ft (4.6 m)
INLET DANGER AREAS
INCLUDE (WORST CASE)
INLET HAZARD
GROUND PLANE
DIMENSIONS CALCULATED
HEADWIND (20 kts)
ON 40 ft/sec (12 m/sec)
CRITICAL VELOCITY
WITH A 3 ft (0.9 m)
ADJUSTMENT FOR SAFETY
CLOSE ENTRY CORRIDOR
45°
3.4 ft (1 m)
FOR WIND DIRECTION > 90°
B
C
NO ENTRY 82 ft (25 m)
D
AFT OF NOZZLE EXIT
NOT TO SCALE
WIDTH
E
72 ft (22 m)
EXHAUST DANGER AREAS
INCLUDE (WORST CASE)
GROUND PLANE
TO 199 ft (61 m)
HEADWIND (20 kts)
APPROX. WIND
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON
AREA
VELOCITY
"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIAL
mph (km/h)
WEAPONS PROJECT, NOV. 1951.
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BE
210−145
A
COMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:
(338−233)
COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGE
145−105
B
NEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGID
(233−169)
STEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.
105−65
MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPE
C
(169−105)
AIRCRAFT.
65−20
D
LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT.
(105−32)
E
< 20 (32)
BEYOND DANGER AREA.
NOTE:
INLET SUCTION
EXHAUST WAKE DANGER AREA
DANGER AREA
65 mph (105 km/h) OR GREATER
EXHAUST WAKE DANGER AREA
ENTRY CORRIDOR
65 mph (105 km/h) OR LESS
N_AC_060301_1_0030101_01_02
Danger Areas of the Engines
CFM56 Series Engine
FIGURE-6-3-1-991-003-A01
Page 2
May 01/16
6-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
R = 4.6 m
(15 ft)
0.76 m
(2.5 ft)
30°
TO 235 m (770 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060301_1_0040101_01_01
Danger Areas of the Engines
IAE V2500 Series Engine
FIGURE-6-3-1-991-004-A01
Page 3
May 01/16
6-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
R = 2.9 m
1 m
(9.5 ft)
(3.3 ft)
30°
TO 38.7 m (127 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060301_1_0110101_01_00
Danger Areas of the Engines
CFM LEAP-1A Engine
FIGURE-6-3-1-991-011-A01
Page 4
May 01/16
6-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
R = 2.8 m
1 m
(9 ft)
(3.3 ft)
30°
TO 40.3 m (132 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060301_1_0120101_01_00
Danger Areas of the Engines
PW 1100G Engine
FIGURE-6-3-1-991-012-A01
Page 5
May 01/16
6-3-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2
Takeoff Power
**ON A/C A319-100 A319neo
Takeoff Power
1.
This section provides danger areas of the engines at max. takeoff conditions.
Page 1
May 01/16
6-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
INLET DANGER AREAS
RADIUS = 19.5 ft (5.9 m)
INCLUDE (WORST CASE)
GROUND PLANE
HEADWIND (20 KTS)
INLET HAZARD DIMENSIONS
BASED ON 40 ft/sec (12 m/sec)
CRITICAL VELOCITY WITH A
3 ft (0.9 m) ADJUSTMENT
FOR SAFETY
A
B
NO ENTRY 684 ft (208 m)
C
NOT TO SCALE
AFT OF NOZZLE EXIT
D
WIDTH
195 ft (59 m)
EXHAUST DANGER AREAS
E
INCLUDE (WORST CASE)
TO 1160 ft (354 m)
GROUND PLANE
HEADWIND (20 KTS)
EXHAUST WAKE DANGER
EXHAUST WAKE DANGER
INLET SUCTION
AREA 65 MPH (105 km/h)
AREA 65 MPH (105 km/h)
DANGER AREA
OR GREATER
OR LESS
APPROX. WIND
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON
AREA
VELOCITY
"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIAL
MPH (km/h)
WEAPONS PROJECT, NOV. 1951
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BE
210−145
A
COMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:
(338−233)
COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGE
145−105
B
NEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGID
(233−169)
STEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.
105−65
MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPE
C
(169−105)
AIRCRAFT.
65−20
D
LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT
(105−32)
E
< 20 (32)
BEYOND DANGER AREA
N_AC_060302_1_0030101_01_01
Danger Areas of the Engines
CFM56 Series Engine
FIGURE-6-3-2-991-003-A01
Page 2
May 01/16
6-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
R = 5.18 m
(17 ft)
1.5 m
(5 ft)
30°
TO 348 m (1150 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060302_1_0040101_01_01
Danger Areas of the Engines
IAE V2500 Series Engine
FIGURE-6-3-2-991-004-A01
Page 3
May 01/16
6-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
R = 10 m
(32.8 ft)
1.6 m
(5.2 ft)
30°
TO 220.7 m (724 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER
EXHAUST DANGER AREA
N_AC_060302_1_0090101_01_00
Danger Areas of the Engines
CFM LEAP-1A Engine
FIGURE-6-3-2-991-009-A01
Page 4
May 01/16
6-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
R = 6.1 m
(20 ft)
3.1 m
(10 ft)
30°
TO 243 m (797.4 ft) AFT OF COMMON NOZZLE ASSEMBLY (CNA)
NOTE:
INTAKE SUCTION DANGER AREA MAX. TAKEOFF POWER
EXHAUST DANGER AREA
N_AC_060302_1_0100101_01_00
Danger Areas of the Engines
PW 1100G Engine
FIGURE-6-3-2-991-010-A01
Page 5
May 01/16
6-3-2
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1
APU
**ON A/C A319-100 A319neo
APU - APIC & GARRETT
1.
This section gives APU exhaust velocities and temperatures.
Page 1
May 01/16
6-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100 A319neo
300°C
200°C
150°C
120°C
100°C
80°C
572°F
392°F
302°F
248°F
212°F
176°F
METERS
0
PLAN
5
10
15
20
25
FEET
0
16.404
32.808
49.212
65.616
82.02
HEIGHT
45 m/s
30 m/s
20 m/s
10 m/s
5 m/s
147 ft/s
98 ft/s
65 ft/s
32 ft/s
16 ft/s
m
ft
10
32.808
5
16.404
METERS
0
0
0
5
10
15
20
ELEVATION
FEET
0
16.404
32.808
49.212
65.616
N_AC_060401_1_0020101_01_00
Exhaust Velocities and Temperatures
APU -- APIC & GARRETT
FIGURE-6-4-1-991-002-A01
Page 2
May 01/16
6-4-1
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0
General Information
**ON A/C A319-100 A319neo
General Information
1.
A brief description of the pavement charts that follow will help in airport planning.
To aid in the interpolation between the discrete values shown, each aircraft configuration is shown
with a minimum range of five loads on the Main Landing Gear (MLG).
All curves on the charts represent data at a constant specified tire pressure with:
-
The aircraft loaded to the Maximum Ramp Weight (MRW),
-
The CG at its maximum permissible aft position.
Pavement requirements for commercial aircraft are derived from the static analysis of loads imposed
on the MLG struts.
Landing Gear Footprint:
Section 07-02-00 presents basic data on the landing gear footprint configuration, MRW and tire sizes
and pressures.
Maximum Pavement Loads:
Section 07-03-00 shows maximum vertical and horizontal pavement loads for certain critical
conditions at the tire-ground interfaces.
Landing Gear Loading on Pavement:
Section 07-04-00 contains charts to find these loads throughout the stability limits of the aircraft at
rest on the pavement.
These MLG loads are used as the point of entry to the pavement design charts which follow,
interpolating load values where necessary.
Flexible Pavement Requirements - US Army Corps of Engineers Design Method:
Section 07-05-00 uses procedures in Instruction Report No. S-77-1 ”Procedures for Development of
CBR Design Curves”, dated June 1977 and as modified according to the methods described in ICAO
Aerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCN
Method), and utilizing the alpha factors approved by ICAO in October 2007.
The report was prepared by the ”U.S. Army Corps Engineers Waterways Experiment Station, Soils
and Pavement Laboratory, Vicksburg, Mississippi”.
The line showing 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).
Flexible Pavement Requirements - LCN Conversion Method:
Page 1
May 01/16
7-1-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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.
Rigid Pavement Requirements - PCA (Portland Cement Association) Design Method:
Section 07-07-00 gives the rigid pavement design curves that have been prepared with the use of the
Westergaard Equation.
This is in general accordance with the procedures outlined in the Portland Cement Association
publications, ”Design of Concrete Airport Pavement”, 1973 and ”Computer Program for Airport
Pavement Design” (Program PDILB), 1967 both by Robert G. Packard.
Rigid Pavement Requirements - LCN Conversion:
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.
ACN/PCN Reporting System:
Section 07-09-00 provides ACN data prepared according to the ACN/PCN system as referenced in
ICAO Annex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations” Fourth Edition, July
2004, incorporating Amendments 1 to 6.
The ACN/PCN system provides a standardized international aircraft/pavement rating system
replacing the various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world.
ACN is the Aircraft Classification Number and PCN is the corresponding Pavement Classification
Number.
An aircraft having an ACN less than or equal to the PCN can operate without restriction on the
pavement.
Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.
The derived single wheel load is defined as the load on a single tire inflated to 1.25 MPa (181 psi)
that would have the same pavement requirements as the aircraft.
Computationally the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1 for
flexible pavements to calculate ACN values.
The Airport Authority must decide on the method of pavement analysis and the results of their
evaluation shown as follows:
PCN
PAVEMENT
SUBGRADE
EVALUATION
TIRE PRESSURE CATEGORY
TYPE
CATEGORY
METHOD
R -- Rigid
A -- High
W -- No pressure limit
T -- Technical
X -- High pressure limited to 1.75
F -- Flexible
B -- Medium
U -- Using Aircraft
MPa (254 psi)
Page 2
May 01/16
7-1-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PCN
PAVEMENT
SUBGRADE
EVALUATION
TIRE PRESSURE CATEGORY
TYPE
CATEGORY
METHOD
Y -- Medium pressure limited to 1.25
C -- Low
MPa (181 psi)
Z -- Low pressure limited to 0.5 MPa
D -- Ultra Low
(73 psi)
For flexible pavements, the four subgrade categories (CBR) are:
- A. High Strength
CBR 15
- B. Medium Strength
CBR 10
- C. Low Strength
CBR 6
- D. Ultra Low Strength
CBR 3
For rigid pavements, the four subgrade categories (k) are:
- A. High Strength
k = 150 MN/m3 (550 pci)
- B. Medium Strength
k = 80 MN/m3 (300 pci)
- C. Low Strength
k = 40 MN/m3 (150 pci)
- D. Ultra Low Strength
k = 20 MN/m3 (75 pci)
Page 3
May 01/16
7-1-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0
Landing Gear Footprint
**ON A/C A319-100 A319neo
Landing Gear Footprint
1.
This section provides data about the landing gear footprint in relation to the aircraft MRW and tire
sizes and pressures.
The landing-gear footprint information is given for all the operational weight variants of the aircraft.
Page 1
May 01/16
7-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
11.039 m
(36.217 ft)
7.590 m
(24.901 ft)
0.500 m
(1.640 ft)
0.927 m
(3.041 ft)
PERCENTAGE
MAXIMUM
NOSE GEAR
MAIN GEAR
OF WEIGHT
NOSE GEAR
MAIN GEAR
WEIGHT VARIANT
RAMP
TIRE
TIRE
ON MAIN
TIRE SIZE
TIRE SIZE
WEIGHT
PRESSURE
PRESSURE
GEAR GROUP
A319−100
64 400 kg
30x8.8R15
11.4 bar
46x17R20
11.9 bar
91.4%
WV000 (CG 36%)
(141 975 lb)
(30x8.8−15)
(165 psi)
(46x16−20)
(173 psi)
A319−100
64 400 kg
30x8.8R15
11.4 bar
46x17R20
11.9 bar
92.6%
WV000 (CG 39%)
(141 975 lb)
(30x8.8−15)
(165 psi)
(46x16−20)
(173 psi)
A319−100
70 400 kg
30x8.8R15
12.5 bar
46x17R20
12.9 bar
92.1%
WV001 (CG 37.5%)
(155 200 lb)
(30x8.8−15)
(181 psi)
(46x16−20)
(187 psi)
A319−100
70 400 kg
30x8.8R15
12.5 bar
46x17R20
12.9 bar
91.5%
WV001 (CG 36%)
(155 200 lb)
(30x8.8−15)
(181 psi)
(46x16−20)
(187 psi)
A319−100
75 900 kg
30x8.8R15
13.2 bar
46x17R20
13.8 bar
91.6%
WV002
(167 325 lb)
(30x8.8−15)
(191 psi)
(46x16−20)
(200 psi)
A319−100
68 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
92.3%
WV003 (CG 38.1%)
(150 800 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
A319−100
68 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
91.5%
WV003 (CG 36%)
(150 800 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
N_AC_070200_1_0040101_01_02
Landing Gear Footprint
(Sheet 1 of 2)
FIGURE-7-2-0-991-004-A01
Page 2
May 01/16
7-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
PERCENTAGE
MAXIMUM
NOSE GEAR
MAIN GEAR
WEIGHT
OF WEIGHT
NOSE GEAR TIRE
MAIN GEAR TIRE
RAMP
TIRE
TIRE
VARIANT
ON MAIN
SIZE
SIZE
WEIGHT
PRESSURE
PRESSURE
GEAR GROUP
A319−100
68 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
92.3%
WV004 (CG 38.1%)
(150 800 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
A319−100
68 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
91.5%
WV004 (CG 36%)
(150 800 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
A319−100
70 400 kg
30x8.8R15
12.5 bar
46x17R20
12.9 bar
92.1%
WV005 (CG 37.5%)
(155 200 lb)
(30x8.8−15)
(181 psi)
(46x16−20)
(187 psi)
A319−100
70 400 kg
30x8.8R15
12.5 bar
46x17R20
12.9 bar
91.5%
WV005 (CG 36%)
(155 200 lb)
(30x8.8−15)
(181 psi)
(46x16−20)
(187 psi)
A319−100
73 900 kg
30x8.8R15
13.5 bar
46x17R20
13.4 bar
91.7%
WV006 (CG 36.52%)
(162 925 lb)
(30x8.8−15)
(196 psi)
(46x16−20)
(194 psi)
A319−100
73 900 kg
30x8.8R15
13.5 bar
46x17R20
13.4 bar
91.5%
WV006 (CG 36%)
(162 925 lb)
(30x8.8−15)
(196 psi)
(46x16−20)
(194 psi)
A319−100
75 900 kg
30x8.8R15
13.2 bar
46x17R20
13.8 bar
91.6%
WV007
(167 325 lb)
(30x8.8−15)
(191 psi)
(46x16−20)
(200 psi)
A319−100
64 400 kg
30x8.8R15
11.4 bar
46x17R20
11.9 bar
92.6%
WV008 (CG 39%)
(141 975 lb)
(30x8.8−15)
(165 psi)
(46x16−20)
(173 psi)
A319−100
64 400 kg
30x8.8R15
11.4 bar
46x17R20
11.9 bar
91.4%
WV008 (CG 36%)
(141 975 lb)
(30x8.8−15)
(165 psi)
(46x16−20)
(173 psi)
A319−100
66 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
92.6%
WV009 (CG 38.8%)
(146 375 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
A319−100
66 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
91.5%
WV009 (CG 36%)
(146 375 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
A319−100
66 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
92.6%
WV011 (CG 38.8%)
(146 375 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
A319−100
66 400 kg
30x8.8R15
12.1 bar
46x17R20
12.5 bar
91.5%
WV011 (CG 36%)
(146 375 lb)
(30x8.8−15)
(175 psi)
(46x16−20)
(181 psi)
A319−100
62 400 kg
30x8.8R15
11.4 bar
46x17R20
11.9 bar
92.6%
WV012 (CG 39%)
(137 575 lb)
(30x8.8−15)
(165 psi)
(46x16−20)
(173 psi)
A319−100
62 400 kg
30x8.8R15
11.4 bar
46x17R20
11.9 bar
91.4%
WV012 (CG 36%)
(137 575 lb)
(30x8.8−15)
(165 psi)
(46x16−20)
(173 psi)
A319 CJ
75 900 kg
30x8.8R15
13.9 bar
46x17R20
13.8 bar
91.6%
WV002
(167 325 lb)
(30x8.8−15)
(202 psi)
(46x16−20)
(200 psi)
A319 CJ
70 400 kg
30x8.8R15
13.9 bar
46x17R20
13.8 bar
91.6%
WV005
(155 200 lb)
(30x8.8−15)
(202 psi)
(46x16−20)
(200 psi)
A319 CJ
76 900 kg
30x8.8R15
13.9 bar
13.8 bar
91.5%
46x17R20
WV010
(169 525 lb)
(30x8.8−15)
(202 psi)
(200 psi)
A319 CJ
75 900 kg
30x8.8R15
13.9 bar
46x17R20
13.8 bar
91.6%
WV013
(167 325 lb)
(30x8.8−15)
(202 psi)
(46x16−20)
(200 psi)
N_AC_070200_1_0040102_01_01
Landing Gear Footprint
(Sheet 2 of 2)
FIGURE-7-2-0-991-004-A01
Page 3
May 01/16
7-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319neo
11.039 m
(36.217 ft)
7.590 m
(24.901 ft)
0.500 m
(1.640 ft)
0.927 m
(3.041 ft)
PERCENTAGE
MAXIMUM
NOSE GEAR
MAIN GEAR
WEIGHT
OF WEIGHT
NOSE GEAR TIRE
MAIN GEAR TIRE
RAMP
TIRE
TIRE
VARIANT
ON MAIN
SIZE
SIZE
WEIGHT
PRESSURE
PRESSURE
GEAR GROUP
A319NEO
64 400 kg
11.4 bar
11.9 bar
92.6%
30x8.8R15
46x17R20
WV050
(141 975 lb)
(165 psi)
(173 psi)
A319NEO
64 400 kg
11.4 bar
11.9 bar
90.7%
30x8.8R15
46x17R20
WV050 (CG 34%)
(141 975 lb)
(165 psi)
(173 psi)
A319NEO
64 400 kg
11.4 bar
11.9 bar
92.6%
30x8.8R15
46x17R20
WV051
(141 975 lb)
(165 psi)
(173 psi)
A319NEO
70 400 kg
12.5 bar
12.9 bar
92.1%
30x8.8R15
46x17R20
WV052
(155 200 lb)
(181 psi)
(187 psi)
A319NEO
70 400 kg
12.5 bar
12.9 bar
92.1%
30x8.8R15
46x17R20
WV053
(155 200 lb)
(181 psi)
(187 psi)
A319NEO
75 900 kg
13.2 bar
13.8 bar
91.6%
30x8.8R15
46x17R20
WV054
(167 325 lb)
(191 psi)
(200 psi)
A319NEO
75 900 kg
13.2 bar
13.8 bar
90.8%
30x8.8R15
46x17R20
WV054 (CG 34%)
(167 325 lb)
(191 psi)
(200 psi)
A319NEO
75 900 kg
13.2 bar
13.8 bar
91.6%
30x8.8R15
46x17R20
WV055
(167 325 lb)
(191 psi)
(200 psi)
A319NEO
75 900 kg
13.2 bar
13.8 bar
90.8%
30x8.8R15
46x17R20
WV055 (CG 34%)
(167 325 lb)
(191 psi)
(200 psi)
N_AC_070200_1_0370101_01_01
Landing Gear Footprint
FIGURE-7-2-0-991-037-A01
Page 4
May 01/16
7-2-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0
Maximum Pavement Loads
**ON A/C A319-100 A319neo
Maximum Pavement Loads
1.
This section provides maximum vertical and horizontal pavement loads for some critical conditions at
the tire-ground interfaces.
The maximum pavement loads are given for all the operational weight variants of the aircraft.
Page 1
May 01/16
7-3-0
@A319
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_070300_1_0230101_01_02
Maximum Pavement Loads
(Sheet 1 of 3)
FIGURE-7-3-0-991-023-A01
Page 2
May 01/16
7-3-0
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
68 400 kg
9 860 kg
21 %
16 230 kg
31 560 kg
38.1 %
10 630 kg
25 250 kg
WV003
(150 800 lb)
(21 750 lb)
MAC (a)
(35 775 lb)
(69 600 lb)
MAC (a)
(23 425 lb)
(55 675 lb)
(CG 38.1 %)
A319−100
68 400 kg
9 860 kg
21 %
16 230 kg
31 280 kg
36 %
10 630 kg
25 020 kg
WV003
(150 800 lb)
(21 750 lb)
MAC (a)
(35 775 lb)
(68 950 lb)
MAC (a)
(23 425 lb)
(55 175 lb)
(CG 36 %)
A319−100
68 400 kg
9 860 kg
21 %
16 230 kg
31 560 kg
38.1 %
10 630 kg
25 250 kg
WV004
(150 800 lb)
(21 750 lb)
MAC (a)
(35 775 lb)
(69 600 lb)
MAC (a)
(23 425 lb)
(55 675 lb)
(CG 38.1 %)
A319−100
68 400 kg
9 860 kg
21 %
16 230 kg
31 280 kg
36 %
10 630 kg
25 020 kg
WV004
(150 800 lb)
(21 750 lb)
MAC (a)
(35 775 lb)
(68 950 lb)
MAC (a)
(23 425 lb)
(55 175 lb)
(CG 36 %)
A319−100
70 400 kg
10 120 kg
21 %
16 660 kg
32 420 kg
37.5 %
10 940 kg
25 940 kg
WV005
(155 200 lb)
(22 325 lb)
MAC (a)
(36 725 lb)
(71 475 lb)
MAC (a)
(24 125 lb)
(57 175 lb)
(CG 37.5 %)
A319−100
70 400 kg
10 120 kg
21 %
16 660 kg
32 210 kg
36 %
10 940 kg
25 770 kg
WV005
(155 200 lb)
(22 325 lb)
MAC (a)
(36 725 lb)
(71 000 lb)
MAC (a)
(24 125 lb)
(56 800 lb)
(CG 36 %)
A319−100
73 900 kg
10 610 kg
21 %
17 460 kg
33 890 kg
36.52 %
11 480 kg
27 110 kg
WV006
(162 925 lb)
(23 400 lb)
MAC (a)
(38 500 lb)
(74 725 lb)
MAC (a)
(25 325 lb)
(59 775 lb)
(CG 36.52 %)
A319−100
73 900 kg
10 610 kg
21 %
17 460 kg
33 820 kg
36 %
11 480 kg
27 050 kg
WV006
(162 925 lb)
(23 400 lb)
MAC (a)
(38 500 lb)
(74 550 lb)
MAC (a)
(25 325 lb)
(59 650 lb)
(CG 36 %)
75 900 kg
10 720 kg
17 870 kg
34 750 kg
36 %
11 800 kg
27 800 kg
A319−100
21 %
WV007
(167 325 lb)
(23 625 lb)
MAC (b)
(39 400 lb)
(76 600 lb)
MAC (a)
(26 000 lb)
(61 275 lb)
A319−100
64 400 kg
9 300 kg
21 %
15 310 kg
29 830 kg
39 %
10 010 kg
23 860 kg
WV008
(141 975 lb)
(20 500 lb)
MAC (a)
(33 750 lb)
(65 775 lb)
MAC (a)
(22 075 lb)
(52 600 lb)
(CG 39 %)
NOTE:
(a) LOADS CALCULATED USING AIRCRAFT AT MRW.
(b) LOADS CALCULATED USING AIRCRAFT AT 74 500 kg (164 250 lb).