(c)
Under the pack-assembly (9) disengage the straps (21), between the decorative-cover (20) and the girt assembly (11).
(d)
Carefully lower, and lock the door with the door control-handle (2).
(e)
Types 1 and 2:
(f)
Type 3: 1 Pull the lower edge of the decorative-cover (20) away from the
1_ Pull the lower edge of the decorative-cover (20) away from the
pack-assembly (9), to disengage the spring clips.
2_ Carefully pull the top edge of the decorative-cover (20), from
the attach-strips (16), and remove it.
_
pack-assembly (9), to disengage the spring clips. 2 Disengage the spring loaded bolts (73) and remove the
_ decorative-cover (20).
EFF : ALL
25-62-44Page 430
(g) keep the decorative-cover (20) with the aircraft.
(2) Safety the inflation reservoir of the escape-slide raft: WARNING : MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY INSTALLED
_______ IN THE REGULATOR VALVE ASSEMBLY OF THE INFLATION RESERVOIR. THIS PREVENTS ACCIDENTAL:
-DISCHARGE OF THE INFLATION RESERVOIR
-DEPLOYMENT OF THE ESCAPE-SLIDE WHICH CAN CAUSE INJURY AND/OR DAMAGE.
(a) Install the lock pin (18) in the regulator valve assembly (19). NOTE : The lock pin (18) is kept in a pocket (75) on the
____ soft-cover (12) of the pack-assembly (9).
(3) Get access to the girt bar (10) and the floor fittings (26): CAUTION : DO NOT OPEN THE PASSENGER/CREW DOOR. IF YOU DO, YOU WILL
_______ START THE SEQUENCE OF STEPS THAT PULLS THE INFLATABLE ASSEMBLY OUT OF THE PACK-ASSEMBLY.
(a)
Remove the SAFETY PIN - SLIDE ARMING (98D52103500000) (4) and set the emergency control-handle (3) to the ARMED/AUTOMATIC position.
(b)
Carefully lift the door with the door control-handle (2).
(c)
hold the door in this position, to prevent it to open fully.
(d)
Remove the girt bar (10): CAUTION : DO NOT PULL THE GIRT ASSEMBLY. IF YOU DO, YOU WILL OPEN
(e)
Carefully lower, and lock the door with the door control-handle (2).
(f)
Set the emergency control-handle (3) to the DISARMED/MANUAL position, and install the SAFETY PIN - SLIDE ARMING (98D52103500000) (4).
_______
THE PACK ASSEMBLY.
1_ Push the spring pawls (29), to release the girt bar (10).
2_ Pull the girt bar (10) inboard from the floor fittings (26).
3_ Put the girt bar (10) on the cabin floor, inboard of the floor
fittings (26).
R EFF : 003-049, 051-099, 101-149, 151-199, 25-62-44Page 431 201-299, 301-399, 401-499, Aug 01/05
CES (4) Remove the pack-assembly (9) from the door:
(a)
Remove the upper attachments of the pack-assembly (9) with one of the two procedures:
(b)
Procedure 1:
(c)
Or.
(d)
Procedure 2: 1 Loosen the link nut (46).
1_ Hold the pack-assembly (9).
2_ Pull the PULL handles (44), to disengage the quick-release
latches (43) from the mounting pins (42).
_ 2 Remove the attach-link (48) and PULL handle (47), from the
_ stud assembly (45).
3 Keep the attach-link (48) and PULL handle (47), with the
_ pack-assembly (9).
4 Hold the pack-assembly (9).
_ 5 Remove the stud assemblies (45) with the allen key (49) from
_ the door.
NOTE : Make sure the allen key (49) goes through the wire loop
____ (50).
6 Keep the stud assemblies (45) with the pack-assembly (9).
_
(e)
Let the pack-assembly (9) fall inboard on the supports (14), and continue to hold it.
(f)
Disconnect the electrical connector (15):
-
FOR 7500MM 2871VC-A.
-
FOR 7501MM 2870VC-A.
-
FOR 7502MM 2873VC-A.
-
FOR 7503MM 2872VC-A.
R EFF : 003-049, 051-099, 101-149, 151-199, 25-62-44Page 432 201-299, 301-399, 401-499, Aug 01/05
CES
(g)
Put blanking caps on the disconnected electrical connectors.
(h)
Lift the pack-assembly (9) from the supports (14) and put it on the cabin floor.
NOTE : The pack-assembly (9) weighs approximately 50.0 kg (110.23
____
lb).
(5) Remove the girt bar (10) from the girt assembly (11): CAUTION : DO NOT PULL THE GIRT ASSEMBLY. IF YOU DO, YOU WILL OPEN THE
_______
PACK ASSEMBLY.
(a)
Pull open the burr-strips of the girt assembly (11).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备4(116)
