(c)
 Remove the nuts (39), the washers (37) and the bolts (36) from the door fitting (35).

 (d)
 Hold the transversal link (40) and remove the bearing bracket

 (38) from the door fitting (35).

 (e)
 Disassemble the transveral link (40) from the door fitting (35).

 (f)
 If required, remove the bush (34) from the door fitting (35).

 1EFF : 301-399, 1 52-22-14Page 414 1 1 May 01/04 1 1 1CES 1

 TASK 52-22-14-400-002
 Installation of the Telescopic Rod 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 access platform 3.2 m (10 ft. 6 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I
 SYNTH.ESTER BASED GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
31 cotter pin 52-22-02 01 -070 41 cotter pin 52-22-02 01 -070 48 cotter pin 52-22-02 03 -090
 1EFF : 301-399, 1 52-22-14Page 415 1 1 May 01/05 1 1 1CES 1

 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-22-00-010-001  Opening of the Emergency Exit Doors from the Passenger Compartment 52-22-00-410-001 Closing of the Emergency Exit Doors from the Passenger Compartment 52-22-00-860-003 Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder 52-22-00-860-004 Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder 52-22-14-991-002 Fig. 403
 3. Job Set-up
__________ Subtask 52-22-14-860-051
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the applicable emergency exit door (referred to as door) is partly opened as required (Ref. TASK 52-22-00-010-001).

 (2)
 Make sure that the access platform is in position below the partly opened door.

 (3)
 Make sure that the special precaution procedure for the door damper and emergency operation cylinder is completed (Ref. TASK 52-22-00-860-003).

 4. Procedure
_________
 (Ref. Fig. 403/TASK 52-22-14-991-002) Subtask 52-22-14-910-051
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (2)
 Clean the component interface and/or the adjacent area.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 1EFF : 301-399, 1 52-22-14Page 416 1 1 May 01/04 1 1 1CES 1

 (4) Apply COMMON GREASE (Material No. 04-004) to all movable parts Subtask 52-22-14-420-052
 B. Installation of the Telescopic Rod Assembly
 (1)
 If removed, install the transversal link (40) in the door (35) as follows:

 (a)
 If remove, install the bush (34) in the door fitting (35).

 (b)
 Assemble the transversal link (40) in the door fitting (35) and install the bearing bracket (38) with the bolts (36), the washers

 (37) and the nuts (39).

 (c)
 Install the washer (33) and the nut (32) on the transerval link (40).

 (d)
 TORQUE the nut (32) to between 0.98 and 1.08 m.daN (86.72 and

 95.57 lbf.in) and safety it with the new cotter pin (31).

 (2)
 Connect the telscopic rod assembly (57) on the door fitting (35) as follows:

 (a)
 Assemble the sliding sleeve (58) to the tranversal link (40) and install the spacer (45).
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門3(104)