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 The FWD and AFT cargo compartment doors have a manual locking mechanism and open hydraulically away from the aircraft. It is only possible to open or close the FWD and AFT cargo-compartment doors from the outer side.
 **ON A/C ALL
 2. Component Location
__________________
 **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 (Ref. Fig. 001)
R **ON A/C 151-199, 401-499,
 (Ref. Fig. 001A)
 **ON A/C 201-220, 222-223, 225-227, 229-299, 301-399,
 **ON A/C 201-220, 222-223, 225-227, 229-299,
 (Ref. Fig. 001B)
 **ON A/C 301-399,
 (Ref. Fig. 001C)
 1EFF : ALL 1 52-30-00Page 2 1 1 Aug 01/05 1 1 1CES 1

 Locations of Cargo Compartment Doors
 Figure 001

R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-30-00Page 3 1224-224, 228-228, 1May 01/05 1 1 1CES 1

 Location of Cargo Compartment Doors
 Figure 001A

R 1EFF : 151-199, 401-499, 1 52-30-00Page 4 1 1 Aug 01/05 1 1 1CES 1

 Locations of Cargo Compartment Doors
 Figure 001B

R 1EFF : 201-220, 222-223, 225-227, 229-299, 1 52-30-00Page 5 1 1 Feb 01/05 1 1 1CES 1

R  Location of Cargo Compartment Doors 
R  Figure 001C
 1EFF :  301-399,  1  52-30-00 Page 6 
1  1  Aug 01/04
 1  1
 1CES  1

 **ON A/C ALL

 3. Description
___________
 **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 A. FWD Cargo-Compartment Door (Zone 825) The FWD cargo-compartment door is installed on the right side of the lower fuselage between FR24A and FR28. For more details refer to the subsequent chapters:
 -FWD Cargo-Comparment Door (Ref.52-31-00)
 -Electrical Door Control System (Ref. 52-35-00)
 -Door Hydraulic System (Ref.52-36-00)
 B. AFT Cargo-Compartment Door (Zone 826) The AFT cargo-compartment door is installed on the right side of the lower fuselage between FR52A and FR56. For more details refer to the subsequent chapters:
 -AFT Cargo-Comparment Door (Ref.52-32-00)
 -Electrical Door Control System (Ref. 52-35-00)
 -Door Hydraulic System (Ref.52-36-00)
 C. BULK Cargo-Compartment Door (Zone 827) The BULK cargo-compartment door is installed on the right side of the lower fuselage between FR60 and FR62. For more details refer to the subsequent chapters:
 -BULK Cargo-Comparment Door (Ref.52-32-00)
R **ON A/C 151-199, 401-499,
 A. FWD Cargo-Compartment Door (Zone 825) The FWD cargo-compartment door is installed on the right side of the lower fuselage between FR24A and FR28. For more details refer to the subsequent chapters:
 -FWD Cargo-Comparment Door (Ref.52-31-00)
 -Electrical Door Control System (Ref. 52-35-00)
 -Door Hydraulic System (Ref.52-36-00)
 B. AFT Cargo-Compartment Door (Zone 826) The AFT cargo-compartment door is installed on the right side of the lower fuselage between FR55A and FR59. For more details refer to the subsequent chapters:
 -AFT Cargo-Comparment Door (Ref.52-32-00)
 -Electrical Door Control System (Ref. 52-35-00)
 1EFF : ALL 1 52-30-00Page 7 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 52-30-00Page 8 1 1 May 01/05 1 1 1CES 1

 - Door Hydraulic System (Ref.52-36-00)
 **ON A/C 201-220, 222-223, 225-227, 229-299, 301-399,
 A. FWD Cargo-Compartment Door (Zone 825) The FWD cargo-compartment door is installed on the right side of the lower fuselage between FR24A and FR28. For more details refer to the subsequent chapters: - FWD Cargo-Comparment Door (Ref.52-31-00) - Electrical Door Control System (Ref. 52-35-00) - Door Hydraulic System (Ref.52-36-00)
 B. AFT Cargo-Compartment Door (Zone 826) The AFT cargo-compartment door is installed on the right side of the lower fuselage between FR52A and FR56. For more details refer to the subsequent chapters: - AFT Cargo-Comparment Door (Ref.52-32-00) - Electrical Door Control System (Ref. 52-35-00) - Door Hydraulic System (Ref.52-36-00)
 **ON A/C ALL
 4. Component Description_____________________ 
R  **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228, 
R R R R R R  A. FWD Cargo-Compartment Door The FWD cargo-compartment door is made of sheet metal and machined parts. It is torsion-resistant and safe to operate at wind speeds up to 50 knots. A manually operated locking mechanism is installed internally to keep the FWD cargo-compartment door in the closed position. The electrical door control-system starts the electric pump of the Yellow hydraulic system which pressurizes the door hydraulic system. The door hydraulic system operates the duplex door actuators to open or close the FWD cargo-compartment door. If there is an electrical failure, it is possible to operate the FWD cargo-compartment door with the handpump. The pressurization of the door hydraulic system does not occur when the locking mechanism is in the locked condition. If the FWD cargo-compartment door is not correctly closed, an electrical circuit sends a signal to the door warning system. This signal comes to the Electronic-Centralized Aircraft-Monitoring (ECAM) system and the MASTER CAUTION lights in the cockpit come on.
　
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