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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 [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
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
　
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