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AIRBUS I NDUSTRIE A320 / A321 GROUND OPERATIONS MANUAL 地面操作手册 [复制链接]

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GROUND OPERATIONS MANUAL
___________________________________________________________________
Aircraft Data, Limitation and Description
Chapter:
Page:
Rev:
Date:
1.1.
1
15
05/03
AIRBUS I NDUSTRIE A320 / A321
1.0. Aircraft Data, Limitation and Description
1.1. Airbus A320/A321
Contents
1.1.1. Aircraft Dimensions and Vertical Clearances 3
1.1.2. Airplane Servicing Arrangement A320/A321 4
1.1.3. Service Points A320/A321 5
1.1.4. Description of Cargo Compartments 7
1.1.4.1. Cargo Compartments of A320-214 7
1.1.4.1.1. Load Securing A320 (bulk loaded) 8
1.1.4.1.2. Dimensions of Cargo Compartments A320 8
1.1.4.1.2.1. Forward Cargo Compartment 8
1.1.4.1.2.2. Aft Cargo Compartment 8
1.1.4.1.2.3. Bulk Cargo Compartment 8
1.1.4.2. Cargo Compartments of A321-211 9
1.1.4.2.1. Load Securing A321 (bulk loaded) 10
1.1.4.2.2. Dimensions of Cargo Compartments A321 11
1.1.4.2.2.1. Forward Cargo Compartment 11
1.1.4.2.2.2. Aft Cargo Compartment 11
1.1.4.2.2.3. Bulk Cargo Compartment 11
1.1.4.3. Cargo Door Operations A320/A321 13
1.1.4.3.1. Door of FWD Cargo Compartment and AFT Cargo Compartment 13
1.1.4.3.2. Door of Compartment 5 (bulk cargo door) 13
1.1.4.4. Loadable ULD A320 / A321 15
1.1.4.5. Cargo Loading System - A320 / A321 15
1.1.4.5.1. Control Panel 15
1.1.4.5.2. Loading/Unloading of Cargo Compartments 17
1.1.4.5.3. Missing or Inoperative Restraints Load Limits 18
1.1.5. Package Tables 19
1.1.5.1. Package Size Dimensions 19
1.1.5.1.1. Forward Cargo Compartment - A320 19
1.1.5.1.2. Forward Cargo Compartment - A321 19
1.1.5.1.3. AFT Cargo Compartment - A320 20
1.1.5.1.4. AFT Cargo Compartment - A321 20
1.1.5.1.5. Packages lift assisted AFT Compartment 5 (BULK) - A320/A321 20
GROUND OPERATIONS MANUAL
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Aircraft Data, Limitation and Description
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AIRBUS I NDUSTRIE A320 / A321
1.1.6. Temperature Control and Ventilation of Cargo Compartments 21
1.1.7. Potable Water Service 21
1.1.8. Lavatory System 21
1.1.7. Configuration and Cabin Layout 23
1.1.7.1. A320-214 Y174 23
1.1.7.2. A321-211 Y210 24
List of Tables and Figures
table 1 clearances ..........................................................................................................................3
table 2 cargo capacities ..................................................................................................................7
table 3 cargo capacities A321..........................................................................................................9
table 4 package size dimensions FWD - A320 ................................................................................19
table 5 package size dimensions FWD - A321 ................................................................................19
table 6 package size dimensions AFT - A320..................................................................................20
table 7 package size dimensions FWD - A321 ................................................................................20
table 8 package size dimensions AFT - hold 5.................................................................................20
figure 1 dimensions ........................................................................................................................3
figure 2 ground servicing.................................................................................................................4
figure 3 service points.....................................................................................................................5
figure 4 cargo compartments...........................................................................................................7
figure 5 sizes of cargo compartments...............................................................................................7
figure 6 FWD hold - A320 ...............................................................................................................8
figure 7 AFT hold -A320..................................................................................................................8
figure 8 bulk - A320 / A321..............................................................................................................8
figure 9 FWD hold A321 ...............................................................................................................11
figure 10 AFT hold A321 ...............................................................................................................11
figure 11 bulk - A320/A321............................................................................................................11
figure 12 cargo door service panel - location ..................................................................................13
figure 13 cargo door ....................................................................................................................13
figure 14 cargo door - vent door ....................................................................................................13
figure 15 cargo door - indication window........................................................................................13
figure 16 loadable ULD A320 - AKH...............................................................................................15
figure 17 cargo loading system control panel ..................................................................................15
figure 18 cargo loading system - FWD...........................................................................................17
figure 19 cargo loading system - AFT.............................................................................................17
figure 20 package size dimensions FWD - A320.............................................................................19
figure 21 package size dimensions AFT - A320...............................................................................20
figure 22 package size dimensions AFT - hold 5 .............................................................................20
figure 23 potable water - AFT service panel ....................................................................................21
figure 24 lavatory/waste panel........................................................................................................21
figure 25 configuration A320-214 Y174 ..........................................................................................23
figure 26 configuration A321-211 Y210 ..........................................................................................24
GROUND OPERATIONS MANUAL
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1.1.1. Aircraft Dimensions and Vertical Clearances
figure 1 dimensions
Note: Passenger Exit doors A320/A321 L1 and L4
(A320 L2/R2 and L3/R3 overwing emergency exits
A321 L2/R3 and L3/R3 emergency exits only)
vertical clearances door sizes
A320 A321
minimum [m] maximum [m] minimum [m] maximum [m] width x height [m]
A 3.39 3.46 3.40 3.53
B 1.99 2.06 2.01 2.11 1.81 x 1.24
C 1.99 2.11 2.04 2.11 1.81 x 1.24
D 2.14 2.30 2.25 2.35 0.94 x 0.86
E 3.36 3.55 3.42 3.71
F 11.68 11.91 11.73 12.10
Maximum and minimum ground clearances reflect the airplane loading within the boundaries
of normal operational C.G. envelopes.
table 1 clearances
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AIRBUS I NDUSTRIE A320 / A321
1.1.2. Airplane Servicing Arrangement A320/A321
figure 2 ground servicing
or Highlifter
Highlifter or
GROUND OPERATIONS MANUAL
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1.1.3. Service Points A320/A321
figure 3 service points
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GROUND OPERATIONS MANUAL
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AIRBUS I NDUSTRIE A320 / A321
A320
1.1.4. Description of Cargo Compartments
1.1.4.1. Cargo Compartments of A320-214
The cargo compartments are located in the lower fuselage, below the passenger cabin. They are divided
into one forward hold (compartment 1) and three aft holds (compartment 3, 4 and 5 = bulk).
All compartments meet the FAR, Part 25, Class D requirements.
The access doors to the cargo compartments are electrically operated from control panels adjacent to
each door. The door may be operated manually in case of power failure with a door hand crank.
A semi-automatic cargo loading system is installed in the FWD (CMPT 1) and AFT compartment (CMPT
3/4). Each system is similar and can be operated by one person. A control panel, installed on the
compartment door controls the electrical POWER DRIVE UNITS (PDU) and the door sill latches.
If bulk load is loaded
in FWD or AFT the
section-nets must be
installed and the
limitations for A320
(bulk loaded) will apply.
figure 4 cargo compartments
CARGO COMPARTMENT CAPACITIES
Hold 1 Hold 3 Hold 4 Hold 5 TOTAL
VOLUME [m3] 13.2 9.7 8.5 5.88 37.28
A320 (bulk loaded)
structural
WEIGHT LIMIT [kg]
3402 2426 2110 1497 9435
max weight 11 12 13 31 32 41 42 51 52 53
per net section [kg] 1045 1225 1132 1301 1125 928 1182 374 353 770
The cargo compartment floor is designed for an evenly distributed load of 732
kg/m2 of bulk loads with a maximum load density of 240 kg/m3.
A320-214
structural
WEIGHT LIMIT [kg]
3402 4536 1497 9435
max floor limit 488 kg/m2 732 kg/m2
amount of AKH (volume 3.6m3) 3 2 2
max gross weight of
AKH on all positions
1134 kg
table 2 cargo capacities
figure 5 sizes of cargo compartments
Ä
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AIRBUS I NDUSTRIE A320 / A321
A320
1.1.4.1.1. Load Securing A320 (bulk loaded)
The divider and door net in each compartment must be closed at any time. Additional tie-down is
normally not required except for individual items of load which by their nature, shape or density may
constitute a hazard. They must be restrained, which can be achieved by filling the cargo hold or net
section volumetrically, or by tie-down.
When filled up to ¾ of height, the cargo hold or net section is considered to be volumetrically full.
Packages weighing more than 150kg shall be restraint or individually tied-down. Single packages should
be tied-down. Tie-down of loads to aircraft structure is achieved by straps or nets connected to the tiedown
points located on the cargo hold floor. Each tie-down point is designed to an ultimate load of
906kg, in any direction.
A minimum clearance of 5 cm must be kept between any load and compartment hold ceiling.
1.1.4.1.2. Dimensions of Cargo Compartments A320
1.1.4.1.2.1. Forward Cargo Compartment
figure 6 FWD hold - A320
1.1.4.1.2.2. Aft Cargo Compartment
figure 7 AFT hold -A320
1.1.4.1.2.3. Bulk Cargo Compartment
figure 8 bulk - A320 / A321
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AIRBUS I NDUSTRIE A320 / A321
A321
1.1.4.2. Cargo Compartments of A321-211
The cargo compartments are located in the lower fuselage, below the passenger cabin. They are divided
into one forward hold (compartment 1) and three aft holds (compartment 3, 4 and 5 = bulk).
All compartments meet the FAR, Part 25, Class D requirements.
The access doors to the cargo compartments are electrically operated from control panels adjacent to
each door. The door may be operated manually in case of power failure with a door hand crank.
A semi-automatic cargo loading system is installed in the FWD (CMPT 1) and AFT compartment (CMPT
3/4). Each system is similar and can be operated by one person. A control panel, installed on the
compartment door controls the electrical POWER DRIVE UNITS (PDU) and the door sill latches.
Two additional center tanks (ACT) are installed in compartment 3 - position 31 and 32.
CARGO COMPARTMENT CAPACITIES
Hold 1 Hold 2 Hold 3 Hold 4 Hold 5 TOTAL
VOLUME [m3] 8.86 13.95 9.41 8.52 5.88 46.62
A321 (containerized - ULD loading)
* 2 ACT installed on position 31 + 32 - further limitation according actual fuel load in ACT
** 1 ACT installed on position 31
structural
WEIGHT LIMIT [kg]
2202 3468 1121 * / 2298 ** 2083 * 1497 * 11548 *
max weight 11 12 21 22 23 31 32 * 33 41 42
per position [kg] 1134 1134 1134 1134 1134 ACT ACT
**(1134)
112
1
1134 1134
The compartment floor is designed for an evenly distributed load of 732 kg/m2
A321 (bulk loaded)
* 2 ACT installed on section 31 + 32 - further limitation according actual fuel load in ACT
** 1 ACT installed on section 31
structural
WEIGHT LIMIT [kg]
2202 3468 1121 * / 2298 ** 2083 * 1497 * 11548 *
max weight 11 12 21 22 23 31 32 * 33 41 42
per net section [kg] 1013 1189 1189 1189 1090 ACT ACT
**(1134)
112
1
919 1164
The compartment floor is designed for an evenly distributed load of 732 kg/m2 with a maximum load density of 240 kg/m3.
* 2 ACT installed (position 31 + 32)
loading of AFT and BULK HOLD (compartment 3, 4 and 5)
is limited by the maximum section load, furthermore by
the actual fuel load of the ACT and the maximum
remaining load capacity:
ACTs empty (TOF < 18600) = 4899 kg
1st ACT full (TOF > 18600) = 3925 kg
2nd ACT full (TOF > 21000) = 1459 kg
** 1 ACT installed (position 31)
loading of AFT and BULK HOLD (compartment 3, 4 and 5) is
limited by the maximum section load, furthermore by the
actual fuel load of the ACT and the maximum remaining
load capacity:
ACT empty (TOF < 18600) = 5878 kg
ACT filled (TOF > 18600) = 4832 kg
table 3 cargo capacities A321
Loading of following articles is strictly prohibited in AFT/BULK (compartment 3+4+5) in all cases:
- any dangerous goods in class 8 (RCM) CORROSIVE
- any dangerous goods in division 1.4S (RXS) EXPLOSIVE
- any dangerous goods in division 2.1 (RFG) FLAMMABLE GAS
- any dangerous goods in class 3 (RFL) FLAMMABLE LIQUIDS
- any cargo items with a front section equal or less than 40x40cm and a length exceeding 1.9m
- any package weighing more than 150kg (HEA)
Above articles may be loaded FWD only.
If A321 is bulk loaded in FWD or AFT, the section nets must be installed and the limitations for
A321 (bulk loaded) will apply and loading instructions and limitations of AFT/BULK must be
adhered (see also next page).
D
D
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AIRBUS I NDUSTRIE A320 / A321
A321
1.1.4.2.1. Load Securing A321 (bulk loaded)
The divider and door net in each compartment must be closed at any time. Additional tie-down is
normally not required except for individual items of load which by their nature, shape or density may
constitute a hazard. They must be restrained, which can be achieved by filling the cargo hold or net
section volumetrically, or by tie-down.
When filled up to 80% of height, the cargo hold or net section is considered to be volumetrically full.
Packages weighing more than 150kg shall be restraint or individually tied-down. Single packages should
be tied-down. Tie-down of loads to aircraft structure is achieved by straps or nets connected to the tiedown
points located on the cargo hold floor. Each tie-down point is designed to an ultimate load of
906kg, in any direction.
A minimum clearance of 5 cm must be kept between any load and compartment hold ceiling.
AFT cargo loading limitation due to ACT installation:
· The loading of following articles is strictly prohibited in AFT and BULK (CMPTs 3+4+5):
- any dangerous goods in class 8 (RCM) CORROSIVE
- any dangerous goods in division 1.4S (RXS) EXPLOSIVE
- any dangerous goods in division 2.1 (RFG) FLAMMABLE GAS
- any dangerous goods in class 3 (RFL) FLAMMABLE LIQUIDS
- any cargo items with a front section equal or less than 40x40cm and a length exceeding 1.9m
- non unitized cargo
- any package weighing more than 150kg (HEA)
above articles or packages must be loaded FWD only
· Beginning behind the ACT, each section has to be filled up to at least 80% of its volume, before the
next section can be loaded. If a net section in CMPT 3 or CMPT 4 is not filled up to at least 80% of
its volume, the BULK (CMPT 5) is restricted to a maximum of 250kg in total.
GROUND OPERATIONS MANUAL
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AIRBUS I NDUSTRIE A320 / A321
A321
1.1.4.2.2. Dimensions of Cargo Compartments A321
1.1.4.2.2.1. Forward Cargo Compartment
figure 9 FWD hold A321
1.1.4.2.2.2. Aft Cargo Compartment
2 ACTs installed 1 ACT installed
figure 10 AFT hold A321
1.1.4.2.2.3. Bulk Cargo Compartment
dimensions of BULK (compartment 5)
are equal to A320
figure 11 bulk - A320/A321
D
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A320 / A321
1.1.4.3. Cargo Door Operations A320/A321
1.1.4.3.1. Door of FWD Cargo Compartment and AFT Cargo Compartment
figure 12 cargo door service panel - location
To open
· Turn the door locking handle downward (105°) to the UNLOCKED position.
(make sure vent door will open)
· open the door service panel
· move the selector switch to the open position and hold it until green indicator light comes on
In case of an electrical failure or if the pump fails, the door can be opened or closed manually with the
hand pump. The crank is inserted into socket fittings located in the lower fuselage, aft of right-hand main
landing gear (yellow system - ground service panel).
To close
· move the selector switch to the CLOSE position and hold it until the compartment door is closed
(Note: the green indicator light goes off when the door starts to close)
· turn the door locking handle up to the LOCKED position and push it into the recess of the handle flap
· make sure that the green mark is visible through each cargo door indication window
Note: the following external indications show that the cargo door is not correctly closed:
- vent door stays in open position
- door locking handle stays away from the outer contour of the door
- red mark is visible through cargo door indication window
If one of these signs is visible call the ground engineer. Do not attempt to open the door immediately
after it has been closed, as the pressure of the hydraulic system prevents the door from moving to the
vertical position
figure 13 cargo door figure 14 cargo door - vent door figure 15 cargo door - indication window
1.1.4.3.2. Door of Compartment 5 (bulk cargo door)
The bulk cargo door is completely manual operated.
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A320 / A321
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A320 / A321
1.1.4.4. Loadable ULD A320 / A321
Only NAS3610 2K2C IATA code AKH (LD3-46) ULDs are available within LTU.
tare weight : 80 kg maximum net weight: 1054 kg
standard weights for baggage loading
(average baggage density 170 kg/m)
including tare weight:
max gross weight: 1134 kg
3
AKH LD3-46
full
¾ 50
½
¼
empty
660 kg
0 kg
360 kg
220 kg
80 kg
LD3 - 46 Container
AKH
figure 16 loadable ULD A320 - AKH
Also one AKG or AKJ containers or 60.4"x61.5" pallet with a maximum height of 46" (116cm) are
loadable per position.
1.1.4.5. Cargo Loading System - A320 / A321
1.1.4.5.1. Control Panel
The control panel is installed on the FWD and AFT cargo door.
figure 17 cargo loading system control panel
D
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A320 / A321
1.1.4.5.2. Loading/Unloading of Cargo Compartments
Door Sill Latches
Each cargo compartment door sill is equipped with two door sill latches. Each door sill latch has two
independently operated latches:
· One latch, when raised, stops the inadvertent roll-out of an ULD during load/unload operations. It is
overridable in the load direction. This latch is lowered electrically from a switch on the control panel.
· The other latch locks the ULD in the door area position at the door sill and is manually operated.
Unloading of FWD (Compartment 1):
1. open cargo compartment door
2. lower door sill latches manually
3. set POWER switch to ON
4. set SILL LATCH switch to down and hold to
lower second latch of door sill latches
5. set joystick to out and hold until ULD in door
area (pos 11) moves from compartment
6. release SILL LATCH switch when ULD is
above door sill latches
7. lower XZ-latch at next ULD
8. set joystick to FWD and hold until ULD is in
line with doorway
9. do again steps 4. - 6. to unload ULD
Loading of FWD (Compartment 1):
1. move ULD onto PDU on ball mat (door area)
2. set joystick to in and hold until ULD is fully in
compartment
figure 18 cargo loading system - FWD
3. lock in position by raising XZ-latch
When compartment is not fully loaded, latches must be raised in empty positions
4. raise door sill latches and close compartment door
Unloading of AFT (Compartment 3/4):
1. open cargo compartment door
2. lower door sill latches manually
3. set POWER switch to ON
4. set SILL LATCH switch to down and hold to
lower second latch of door sill latches
5. set joystick to out and hold until ULD in door
area (pos 41) moves from compartment
6. release SILL LATCH switch when ULD is
above door sill latches
7. lower XZ-latch at next ULD
8. set joystick to FWD/AFT and hold until ULD is
in line with doorway
9. do again steps 4. - 6. to unload ULD
Loading of AFT (Compartment 3/4):
1. move ULD onto PDU on ball mat (door area)
2. set joystick to in and hold until ULD is fully in
compartment.
3. set joystick to FWD/AFT and hold until ULD is
in loading position
figure 19 cargo loading system - AFT
4. lock in position by raising XZ-latch
When compartment is not fully loaded, latches must be raised in empty positions
5. raise door sill latches and close compartment door
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A320 / A321
1.1.4.5.3. Missing or Inoperative Restraints Load Limits
For the FWD and AFT cargo compartment the following limits apply:
If any latch is missing or inoperative the position must be kept unloaded (or max. an empty ULD), except
for the YZ-latches at the side guide rail, as the load must be reduced to 794kg if one unit or one unit on
each side is missing or inoperative; if two or more units are missing or inoperative the position must be
kept unloaded (or max. an empty ULD).
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A320 / A321
1.1.5. Package Tables
These tables show maximum package size dimensions which will pass through the cargo door openings.
Package sizes are approximate: Tilting, twisting bending and/or rotating packages through openings will
allow additional lengths in many cases, but should be determined for each situation. A trial loading is
recommended for packages with dimensions close to maximum dimensions indicated in the tables.
The height dimensions do not include allowances for items increasing package height such as fork lift
tine thickness, pallet depths, skid tub heights, etc. Any such devices must be accounted for the total
package height.
1.1.5.1. Package Size Dimensions
1.1.5.1.1. Forward Cargo Compartment - A320
figure 20 package size dimensions FWD - A320
clear opening of forward cargo door 181 cm x 124 cm
HEIGHT
[cm]
WIDTH [cm]
10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 164
LENGTH [cm]
115 415 395 375 355 335 315 294 274 254 234 214 194 173 165 143 143
97 475 475 455 435 414 394 374 354 334 314 294 273 253 233 212 200
70 475 475 475 475 475 465 444 424 403 382 362 341 319 298 275 253
table 4 package size dimensions FWD - A320
1.1.5.1.2. Forward Cargo Compartment - A321
HEIGHT
[cm]
WIDTH [cm]
10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170
up to
LENGTH [cm]
119 399 379 359 339 319 299 279 259 238 218 197 177 164 164 -- -- --
101 494 474 454 434 414 394 373 353 333 313 293 273 252 232 211 199 --
79 565 545 525 505 484 464 443 423 402 382 361 340 319 297 274 252 --
table 5 package size dimensions FWD - A321
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AIRBUS I NDUSTRIE A320 / A321
A320 / A321
1.1.5.1.3. AFT Cargo Compartment - A320
clear opening of aft cargo door
181 cm x 124 cm
figure 21 package size dimensions AFT - A320
HEIGHT
[cm]
WIDTH [cm]
10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 171
LENGTH [cm]
115 424 404 384 364 344 324 304 284 264 243 223 203 182 172 143 143 143
97 485 485 465 445 425 405 384 364 344 324 304 284 264 243 223 202 200
70 485 485 485 485 485 475 455 435 414 394 373 352 331 310 288 266 253
table 6 package size dimensions AFT - A320
1.1.5.1.4. AFT Cargo Compartment - A321
The transport of non unitized load behind the ACT is not allowed. Tie-down points not required for net
fastening are not allowed to use for individual restraint of packages. All nets must be installed, therefore
the largest net section is section 41 and 42. Larger packages may be loaded FWD.
HEIGHT
[cm]
WIDTH [cm]
10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170
up to
LENGTH [cm]
114 330 330 330 330 328 308 288 268 247 272 206 185 152 -- -- -- --
101 330 330 330 330 330 310 310 310 310 310 303 283 263 243 222 202 152
79 330 330 330 330 330 310 310 310 310 310 310 300 300 300 288 265 252
table 7 package size dimensions FWD - A321
1.1.5.1.5. Packages lift assisted AFT Compartment 5 (BULK) - A320/A321
clear opening of bulk cargo door 94 cm x 86 cm
HEIGHT
[cm]
WIDTH [cm]
10 20 30 40 50 60 70 80 85
LENGTH [cm]
65 279 261 243 225 205 186 165 148 141
table 8 package size dimensions AFT - hold 5
figure 22 package size dimensions AFT - hold 5
GROUND OPERATIONS MANUAL
___________________________________________________________________
Aircraft Data, Limitation and Description
Chapter:
Page:
Rev:
Date:
1.1.
21
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04/02
AIRBUS I NDUSTRIE A320 / A321
A320 / A321
1.1.6. Temperature Control and Ventilation of Cargo Compartments
Only the BULK (CMPT 5) is equipped with a heating and ventilation system.
A320 / A321
max 3 AVI/H (full size kennels) in BULK (CMPT 5)
as the capacity of BULK is limited there is a maximum of either 3 AVI/H (full size kennels) or 3
surfboards or 3 bikes or any combination thereof.
1.1.7. Potable Water Service
To fill the tank (max 200 l) the hose must be connected to the fill/drain port of the AFT fill and drain
panel. Turn the fill/drain handle to the pull to fill position and pull the handle out to the mechanical stop.
Switch the pump of the service vehicle on (do not exceed
water pressure 3.45 bar). The quantity indicator shows the
required quantity. The fill/drain handle will automatically
return to the normal position when the tank full light comes
on. If the tank is overfilled, water will flow from the overflow
port.
figure 23 potable water - AFT service panel
If the system must be drained and electrical power is not available, all panels (forward, center, aft) must
be serviced simultaneously.
1.1.8. Lavatory System
To drain the waste tank (max capacity 200 l) the
hose must be connected to the toilet drain
connection (AFT). Push the open lever and pull
the drain valve control handle from the NORMAL
to the DRAIN position and the waste will drain.
Connect the flush/fill hose of the toilet servicing
vehicle to the fill and rinse connection (do not
exceed 2.4 bar) and flush the toilet system with
approximately 20 liters. The drain valve control
handle must be in the DRAIN position during this
operation.
figure 24 lavatory/waste panel
Switch the pump of the servicing vehicle off and put the drain valve control handle in NORMAL position.
Disconnect the adapter and the drain hose. To close the inner flap valve pull the push to open lever until
the lever clicks. Pump 10 l of water as prime charge and disconnect the fill and rinse hose and let the
water in the line drain completely. Close the cap and visually examine for leaks.
GROUND OPERATIONS MANUAL
___________________________________________________________________
Aircraft Data, Limitation and Description
Chapter:
Page:
Rev:
Date:
1.1.
22
14
04/02
AIRBUS I NDUSTRIE A320 / A321
A320 / A321
intentionally left blank
GROUND OPERATIONS MANUAL
___________________________________________________________________
Aircraft Data, Limitation and Description
Chapter:
Page:
Rev:
Date:
1.1.
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AIRBUS I NDUSTRIE A320 / A321
A320
1.1.7. Configuration and Cabin Layout
1.1.7.1. A320-214 Y174
ROW 1
ROW 12
ROW 2
ROW 3
ROW 4
ROW 5
ROW 6
ROW 7
ROW 8
ROW 9
ROW 10
ROW 11
ROW 14
ROW 15
ROW 16
ROW 17
ROW 18
ROW 19
ROW 20
ROW 21
ROW 22
ROW 23
ROW 24
ROW 25
ROW 26
ROW 27
ROW 28
ROW 29
ROW 30
A B C
A B C
D E F
D E F
Exit L1 Exit R1
A B C D E F
A B C D E F
Emer- L2
gency
Exit L3
Emergency
Exit R2
Emergency
Exit R3
Exit L4 Exit R4
PAX Cmpt 0A
ROW 1-10
TTL 60 seats
PAX Cmpt 0B
ROW 11-21
TTL 60 seats
PAX Cmpt 0C
ROW 22-30
TTL 54 seats
figure 25 configuration A320-214 Y174
A320-214 Y174
Special seats:
UMs SEATS 2 A B C
3 A B C
3 D E F
4 D E F
Handicapped SEAT 4 - 8 C+D
Passengers 15 - 26 C+D
Baby Baskets SEATS 1 ABC (1x)
1 DEF (1x)
Stretcher 28 DEF-30 DEF
Position (to be loaded through L4)
Exits L1/R1 - - - - - -
Emergency L2/R2 ROW 12 A - F
Exits L3/R3 ROW 14 A - F
Exits L4/R4 - - - - - -
No Recline ROW 11 + 12
No PET/C at ROW 1, ROW 12 and ROW14
Max infants (due to infant life jacket) 15
Oxygen supply:
In case of rapid decompression of the aircraft
cabin a passenger oxygen supply system will
be activated automatically.
Above every seat group (ABC + DEF) an
additional mask will fall down.
Boarding Sequence
passenger bridge/jetway or one stair L1
1. preboarding
2. rows 15-30
3. rows 01-14
two stairs L1 + L4
1. preboarding
2. rows 01-14 (front entry) and
¨
GROUND OPERATIONS MANUAL
___________________________________________________________________
Aircraft Data, Limitation and Description
Chapter:
Page:
Rev:
Date:
1.1.
24
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05/03
AIRBUS I NDUSTRIE A320 / A321
A321
1.1.7.2. A321-211 Y210
A321-211 Y210
Special seats:
figure 26 configuration A321-211 Y210
UMs 2 A B C
3 A B C
3 D E F
4 D E F
Handicapped 4 - 8 C+D
Passengers 15 - 24 C+D
Baby Baskets 1 ABC (1x)
2 DEF (1x)
Stretcher 36 DEF-38 DEF
Position
Exits L1/R1 - - - - - -
Emerg L2/R2 ROW 10, ROW 11, 12 ABC
Exits L3/R3 ROW 25, ROW 26, 27 A-C
Exits L4/R4 - - - - - -
No Recline 10 B-E, 25 C D
37 A-C, 38 D-F
No PET/C at ROW 1, 2D-F, ROW10,
ROW11, 12 A-C, ROW 25, ROW 26
and 27 ABC
Max infants (due to infant life jacket) 20
Oxygen supply:
In case of rapid decompression of the aircraft
cabin, a passenger oxygen supply system will be
activated automatically.
Above every seat group (ABC + DEF) an
additional mask will fall down.
Boarding Sequence
passenger bridge/jetway or one stair L1
1. preboarding
2. rows 20-38
3. rows 01-19
two stairs L1 + L4
1. preboarding
2. rows 01-19 (front entry) and
¨

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看看。

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谢谢!!!

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谢谢诶

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回复 1# 航空 的帖子

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貌似很复杂的样子

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回复看看不知道怎么样

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收下了,楼主

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