(b)
 Remove the loop (35) of the survival-kit lanyard (white) (36), from the trigger lever (37).

 (c)
 Pull open the blue (38) and the green (39) burr-strips.

 (d)
 Remove the release strap (yellow) (40) from the trigger lever (37).

 (e)
 Pull the HANDLE (31), and open the lace-up joint (34).

 (f)
 Remove the mooring line (32) from the girt bar (10).

 (g)
 Remove the girt bar (10) from the opened girt assembly (11).

 (h)
 Keep the girt bar (10) with the door.

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

 -Attach-link (46) and PULL handle (47).
 -Stud assemblies (45).
R  EFF : 003-049, 051-099, 101-149, 151-199, 25-62-44Page 433 201-299, 301-399, 401-499, Aug 01/05
 CES  **ON A/C ALL

 TASK 25-62-44-400-001
 Installation 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 -------------------------------------------------------------------------------
R No specific nylon cord No specific Allen key 0.156 in. (3.9623 mm) R No specific 1 WARNING NOTICE No specific Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN)
 No specific Torque Wrench : range 0.20 to 3.60 m.daN

 (2.00 to 26.00 lbf.ft) 98D52103500000 2 SAFETY PIN - SLIDE ARMING
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002  USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)  C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
11-00-00-400-007 23-73-00-861-001 24-41-00-862-002  Installation of the ESSO (Scotchcal Labels)Energize the Cabin Intercommunication Data System (CIDS)De-energize the Aircraft Electrical Circuits Supplied from the External Power
 24-42-00-861-001  Energize the Ground Service Network from the External Power
 33-51-00-710-001  Operational Test of Emergency Lights by 'TEST EMER LIGHT SYS' Pushbutton
 52-10-00-410-001 52-10-00-610-001 52-10-00-860-001  Closing of the Passenger/Crew DoorReplacement of the Diaphragm in the Percussion Mechanism of the Door Damper and Emergency Operation Cylinder of the Passenger/Crew DoorsSpecial Precautions before Work on the Passenger/Crew Door
 52-10-00-860-002  Special Precautions after Work on the Passenger/Crew Door

 AMM 11-32-52 P. Block 001 **ON A/C 001-002,
R  25-62-44-991-021 Fig. 402 **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 25-62-44-991-021-A **ON A/C ALL Fig. 402A
R  25-62-44-991-003 Fig. 403 **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 25-62-44-991-016  Fig. 404

 EFF : ALL
25-62-44Page 435

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-002,
 25-62-44-991-019 Fig. 405 R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 25-62-44-991-019-A Fig. 405A
 **ON A/C ALL

 25-62-44-991-017 Fig. 406
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,

 25-62-44-991-026 Fig. 407 R **ON A/C 106-149, 301-399, 401-499,
 25-62-44-991-026-A Fig. 407A
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 25-62-44-860-051

 A. Aircraft Maintenance Configuration
 **ON A/C 001-002,

 (Ref. Fig. 402/TASK 25-62-44-991-021) R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 402A/TASK 25-62-44-991-021-A)
 EFF : ALL
25-62-44Page 436

 **ON A/C ALL
 (1)
 Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).

 (2)
 In the cockpit, on the overhead panel 25VU (SIGNS), make sure that the EMER EXIT LT switch (1) is set to the OFF position.
　
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