(3)
 Install the bushes (5), (16), (6) and (9) and the washer (10).

 (4)
 Apply COMMON GREASE (Material No. 04-004) on the bolts (8) and (15) before you install them.

 (5)
 Install the bolts (8) and (15), the washers (4) and the lockwasher

 (7) and the nuts (3). R NOTE : If you install new bolts (8) and (15), drill a hole of 2 mm
____
 (0.0787 in.).

 (6) Torque the nuts (3) to between 1.2 and 1.35 m.daN (106.19 and 119.46 lbf.in).
R (7) Safety the bolt (8) with the lockwasher (7).
 1EFF : ALL 1 52-13-12Page 411 1 1 Aug 01/05 1 1 1CES 1

 Door Buffer Figure 404/TASK 52-13-12-991-004- 12 (SHEET 1)
 1EFF : 1 1R 1CES  ALL  1 11 1 52-13-12 Page 412 Aug 01/05

 Door Buffer Figure 404/TASK 52-13-12-991-004- 22 (SHEET 2)
 1EFF : 1 1R 1CES  ALL  1 11 1 52-13-12 Page 413 Aug 01/05

 (8)
 Install a new cotter pin (2).

 (9)
 Install the bonding leads (11) on the supports, the washers (13) and the screws (12).

 NOTE : When you install the bonding leads (11), do an electrical
____ bonding (Ref. TASK 20-28-00-912-004).
 5. Close-up
________
 Subtask 52-13-12-420-054
 A. Installation of the Component
R  (1) Install the door-damper and emergency-operation cylinder (Ref. TASK 52-13-14-400-001).
 (2) Install the Aft passenger/crew door (Ref. TASK 52-13-11-400-001). Subtask 52-13-12-410-053
 B. Close Access
 (1)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 (2)
 Close the Aft passenger/crew door 831 or (841) (Ref. TASK 52-10-00-410-001).

 (3)
 Remove the access platform(s).

 1EFF : ALL 1 52-13-12Page 414 1 1 Aug 01/05 1 1 1CES 1 TASK 52-13-12-000-002

 Removal of the Guide Arms
 WARNING : DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE THAN 65
_______ KNOTS.
 WARNING : BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:
_______
 -
THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.

 -
THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.

 WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES. RESIDUAL
_______ PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 3.50 m (11 ft. 6 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
 Power 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
 Door 52-13-31-000-001 Removal of the Lining Flap 52-13-12-991-005 Fig. 405
 1EFF : ALL 1 52-13-12Page 415 1 1 Feb 01/98 1 1 1CES 1

 3. Job Set-up
__________ Subtask 52-13-12-861-050
 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

 Subtask 52-13-12-010-054
 B. Get Access
 (1)
 Put the access platform in position at the Aft passenger/crew door at the zone 832 or 842.

 (2)
 Open the applicable Aft passenger/crew door 832 or 842 (Ref. TASK 52-10-00-010-001).

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

 Subtask 52-13-12-865-053
 C. Open, safety and tag 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
 Subtask 52-13-12-020-057
 D. Removal of the Lining Flap
　
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