(2)
Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).
(3)
Install the escape slide (Ref. TASK 25-62-44-400-001).
(4)
Install the door lining panels:
(Ref. TASK 25-23-46-400-002)
(a) For the left door: 832AZ.
(b) For the right door: 842AZ. R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-13-00-410-060-A
A. Installation of the Components
(1)
Install the door insulation.
(2)
Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).
(3)
Install the escape-slide raft (Ref. TASK 25-62-44-400-001).
(4)
Install the door lining panels:
(Ref. TASK 25-23-46-400-002)
(a)
For the left door: 832AZ.
(b)
For the right door: 842AZ.
1EFF : ALL 1 52-13-00Page 305 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
Subtask 52-13-00-865-053
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
Subtask 52-13-00-410-061
C. Close Access
(1)
Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).
(2)
Close the aft passenger/crew door 832 (842) (Ref. TASK 52-10-00-410-001).
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
(4)
Remove the access platform(s).
1EFF : ALL 1 52-13-00Page 306 1 1 May 01/04R 1 1 1CES 1
AFT PASSENGER/CREW DOOR - ADJUSTMENT/TEST
_________________________________________
TASK 52-13-00-820-001
Adjustment of the AFT Passenger/Crew Door
1. Reason for the Job
__________________
NOTE : You must only do the adjustment/test procedure after maintenance
____ activities that require door rigging (such as replacement of components or malfunction of the doors).
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 two shims (thickness 0.2 mm (0.0078 in))
No specific dynamometer 15 daN (33.7213 lbf)
No specific access platform 3.5 m (11 ft. 6 in.)
No specific positioning templates 70 mm (2.7559 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98DNSA20206120 1 RIGGING PIN 98D52103501000 1 BALLAST WEIGHT - PASSENGER CREW DOOR
1EFF : ALL 1 52-13-00Page 501 1 1 May 01/05 1 1 1CES 1 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)
Material No. 08-007A SEALANT, HIGH TEMP. (Ref. 20-31-00) 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)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
13 cotter pin 52-13-04 04B-170 13 cotter pin 52-13-04 04D-170 R 13 cotter pin 52-13-04 04E-170 47 cotter pin 53-46-04 80B-060 53 lock plate 52-13-11 21 -040 53 lock plate 52-13-11 21A-040 208 cotter pin 52-13-04 05B-040 208 cotter pin 52-13-04 05H-040
1EFF : ALL 1 52-13-00Page 502 1 1 Aug 01/05 1 1 1CES 1 D. Referenced Information
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM DOORS 舱门2(57)