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).
 (c)
 Disengage the straps (21) from the straps on the lower inside edge of the decorative-cover (20).

 (d)
 Keep the straps (21) with the pack-assembly (9).

 (e)
 Keep the decorative-cover (20) with the aircraft.

R  EFF : 003-049, 051-099, 101-149, 151-199, 25-62-44Page 413 201-299, 301-399, 401-499, Aug 01/05
 CES  (8) Remove the pack-assembly (9) from the door:

 (a) Remove the upper attachments of the pack-assembly (9) with one of the two procedures:
 1  Procedure 1:
_
 a Hold the pack-assembly (9).

_ b Pull the PULL handles (44), to disengage the quick-release
_ latches (43) from the mounting pins (42).
 2  Or.
_
 3 Procedure 2:

_
 a Loosen the link nut (46).

_ b Remove the attach-link (48) and PULL handle (47), from the
_
 stud assembly (45).

 c  Keep the attach-link (48) and PULL handle (47), with the
_
 pack-assembly (9).

 d  Hold the pack-assembly (9).
_
 e 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).

 f  Keep the stud assemblies (45) with the pack-assembly (9).
_
 (b)
 Let the pack-assembly (9) fall inboard on the supports (14), and continue to hold it.

 (c)
 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 414 201-299, 301-399, 401-499, Aug 01/05
 CES

 (d)
 Put blanking caps on the disconnected electrical connectors.

 (e)
 Lift the pack-assembly (9) from the supports (14) and remove it from the aircraft.

 NOTE : Make sure that these removed components are kept together
____
 with the pack-assembly (9):

 -Straps (21).
 -Attach-link (48) and PULL handle (47).
 -Stud assemblies (45).
 (9) Procedure out of the aircraft: CAUTION : KEEP OFF THE INFLATED ESCAPE-SLIDE. IF YOU GO ON IT, YOU
_______ CAN CAUSE DAMAGE TO THE SURFACE MATERIAL.
 (a)
 Push in the flapper valves (5) of the aspirator (6) to release the pressure from the escape-slide raft (7).

 (b)
 Roll up the deflated escape-slide raft (7). NOTE : Start from the bottom end of the deflated escape-slide

____
 raft (7).

 (c)
 Carefully put the escape-slide raft (7), the pack-assembly (9) and related components in a clean box, without sharp objects.

 (d)
 Return them to one of the two locations for servicing:

 -The workshop (Ref. CMM 256120).
 -Or, to the manufacturer. **ON A/C ALL
 5. Close-up
________ Subtask 25-62-44-860-058
 A. Aircraft Maintenance Configuration
 (1)
 Replace the diaphragm in the percussion mechanism of the door-damper and emergency-operation cylinder (Ref. TASK 52-10-00-610-001).

 (2)
 Install a serviceable escape-slide/slide raft on the door (Ref. TASK 25-62-44-400-001).

 TASK 25-62-44-000-002
 Removal of the Escape-Slide Pack-Assembly

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
 No specific allen key 0.156 in. (3.9623 mm)
 98D52103500000 2 SAFETY PIN - SLIDE ARMING

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM EQUIPMENT/FURNISHINGS 設(shè)備4(113)