(2)
 Remove the door linings (Ref. TASK 25-23-46-000-002).

 (3)
 Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).

 (4) Remove the door insulation. R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-13-31-010-058-A
 C. Removal of Components
 (1)
 Remove the escape slide/raft (Ref. TASK 25-62-44-000-002).

 (2)
 Remove the door lining panels (Ref. TASK 25-23-46-000-002).

 (3)
 Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).

 (4)
 Remove the door insulation.

 1EFF : ALL 1 52-13-31Page 436 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 4. Procedure
_________ Subtask 52-13-31-020-053
 A. Removal of the Girt Bar Fittings
 (Ref. Fig. 410/TASK 52-13-31-991-011)

 (1)
 Remove the old sealant around the girt bar fittings and on the heads of the screws (111) and (121) with CLEANING AGENTS (Material No. 11-004), MISCELLANEOUS (Material No. 19-003) and a non metallic scraper.

 (2)
 Loosen the screws (111) (121) and remove them.

 (3)
 Remove the girt bar fittings (110) (120).

 1EFF : ALL 1 52-13-31Page 437 1 1 Feb 01/02R 1 1 1CES 1

 Girt Bar Fittings Figure 410/TASK 52-13-31-991-011
 1EFF : 1 1R 1CES  ALL  1 11 1 52-13-31 Page 438 Feb 01/02

 TASK 52-13-31-400-003
 Installation of the Girt Bar Fittings
 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 3.5 m (11 ft. 6 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 09-005  USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
 Material No. 11-004  USA MIL-T-81533
 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
 (Ref. 20-31-00)

 Material No. 19-003  USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 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
 1EFF : ALL 1 52-13-31Page 439 1 1 Feb 01/04 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

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 52-11-00-820-001 Adjustment of the FWD Passenger/Crew Door 52-13-31-991-011 Fig. 410 52-13-31-991-012 Fig. 411
 3. Job Set-up
__________
 Subtask 52-13-31-869-052
 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 52-13-31-865-056
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------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
　
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(6)