AIRBUS I NDUSTRIE A320 / A321 GROUND OPERATIONS MANUAL 地面操作手册

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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 ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 2 14 04/02 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 ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 3 14 04/02 AIRBUS I NDUSTRIE A320 / A321 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 maximum minimum maximum width x height 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 GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 4 15 05/03 AIRBUS I NDUSTRIE A320 / A321 1.1.2. Airplane Servicing Arrangement A320/A321 figure 2 ground servicing or Highlifter Highlifter or GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 5 14 04/02 AIRBUS I NDUSTRIE A320 / A321 1.1.3. Service Points A320/A321 figure 3 service points GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 6 14 04/02 AIRBUS I NDUSTRIE A320 / A321 intentionally left blank GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 7 15 05/03 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 13.2 9.7 8.5 5.88 37.28 A320 (bulk loaded) structural WEIGHT LIMIT 3402 2426 2110 1497 9435 max weight 11 12 13 31 32 41 42 51 52 53 per net section 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 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 GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 8 14 04/02 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 GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 9 15 05/03 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 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 2202 3468 1121 * / 2298 ** 2083 * 1497 * 11548 * max weight 11 12 21 22 23 31 32 * 33 41 42 per position 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 2202 3468 1121 * / 2298 ** 2083 * 1497 * 11548 * max weight 11 12 21 22 23 31 32 * 33 41 42 per net section 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 GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 10 15 05/03 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 ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 11 15 05/03 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 D GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 12 14 04/02 AIRBUS I NDUSTRIE A320 / A321 A321 intentionally left blank GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 13 14 04/02 AIRBUS I NDUSTRIE A320 / A321 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. GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 14 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. 15 15 05/03 AIRBUS I NDUSTRIE A320 / A321 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 GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 16 15 05/03 AIRBUS I NDUSTRIE A320 / A321 A320 / A321 intentionally left blank GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 17 15 05/03 AIRBUS I NDUSTRIE A320 / A321 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 GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 18 15 05/03 AIRBUS I NDUSTRIE A320 / A321 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). GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 19 14 04/02 AIRBUS I NDUSTRIE A320 / A321 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 WIDTH 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 164 LENGTH 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 WIDTH 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 up to LENGTH 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 GROUND OPERATIONS MANUAL ___________________________________________________________________ Aircraft Data, Limitation and Description Chapter: Page: Rev: Date: 1.1. 20 14 04/02 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 WIDTH 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 171 LENGTH 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 WIDTH 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 up to LENGTH 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 WIDTH 10 20 30 40 50 60 70 80 85 LENGTH 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 14 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. 23 15 05/03 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 15 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 ¨

ting4520 发表于 2010-9-3 23:04:33

看看。
:loveliness:

chendu1987 发表于 2010-9-7 23:10:57

谢谢！！！

jacques0105 发表于 2010-9-17 19:08:47

谢谢诶

:loveliness:

zhengluanfeng 发表于 2010-10-31 22:51:40

回复 1# 航空的帖子

:) bfgcuyuvygi

享受和平 发表于 2010-11-17 23:11:05

回复看看

回复看看，回复看看

ceskhb 发表于 2010-12-6 00:25:03

貌似很复杂的样子

yw_1221 发表于 2010-12-13 10:41:02

回复看看不知道怎么样

blueguard2007 发表于 2010-12-15 23:03:26

收下了，楼主

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