曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
航空资料4(139)
