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REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific access platform 3.5 m (11 ft. 6 in.)
 B. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
 -------------------------------------------------------------------------------
2 cotter pin 52-11-11 18 -090 7 cotter pin 52-11-11 18 -200
 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
25-23-46-400-002 Installation of the Door Linings at the AFT Passenger/Crew Doors R 25-62-44-400-001 Installation of the Escape-Slide Pack-Assembly 52-10-00-080-001 Removal of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide 52-10-00-080-001 Removal of the Passenger/Crew Door Ballast Weight
 (98D52103501000) for Escape Slide/Raft 52-10-00-410-001 Closing of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
 Door 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew Door
 1EFF : ALL 1 52-13-31Page 406 1 1 Feb 01/04 1 1 1CES 1

 3. Job Set-up
__________ Subtask 52-13-31-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the access platform is in position at the applicable passenger/crew door.

 (2)
 Make sure that the door lining panels, the door frame lining panels and the insulation are removed.

 (3)
 Obey the special precautions before you start work on the door (Ref. TASK 52-10-00-860-001).

 (4)
 Make sure that the parts retained from the removed component are clean and in the correct conditions.

 Subtask 52-13-31-865-052
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged 13WN, 15WN, 48WV
 4. Procedure
_________ Subtask 52-13-31-420-050
 A. Installation of the Lining Flap
 (1) Engage the lining flap (5) on the bellcrank assy (6) and on the rods
 (1)
 and install the components below:

 (a)
 Install the pins (8) and the washers (9).

 (b)
 Install new cotter pin (7).

 (c)
 Install the pins (3) and the washers (4).

 (d)
 Install new cotter pin (2).

 1EFF : ALL 1 52-13-31Page 407 1 1 May 01/98R 1 1 1CES 1

 5. Close-up
________
 **ON A/C 001-002,

 Subtask 52-13-31-410-050
 A. Installation of Components
 (1)
 Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).

 (2)
 Install the door insulation.

 (3)
 Install the door lining panels (Ref. TASK 25-23-46-400-002).

 (4) Install the escape slide (Ref. TASK 25-62-44-400-001). R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-13-31-410-050-A
 A. Installation of Components
 (1)
 Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).

 (2)
 Install the door insulation.

 (3)
 Install the door lining panels (Ref. TASK 25-23-46-400-002).

 (4) Install the escape slide/raft (Ref. TASK 25-62-44-400-001).
 **ON A/C ALL

 Subtask 52-13-31-865-053
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
 1EFF : ALL 1 52-13-31Page 408 1 1 Aug 01/05 1 1 1CES 1 Subtask 52-13-31-410-051

 C. Close Access
 (1)
 Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).

 (2)
 Remove all the ground support equipment, the maintenance equipment, the standard and special tools and all other items.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (4)
 Close the passenger/crew door 832 (842) (Ref. TASK 52-10-00-410-001).

 (5)
 Remove the access platform(s).

 1EFF : ALL 1 52-13-31Page 409 1 1 May 01/98R 1 1 1CES 1
　
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