Weight (98D52103501000) for Escape Slide 52-10-00-480-001 Installation of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide/Raft 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
**ON A/C 001-002,
52-13-00-991-008 Fig. 515
R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
52-13-00-991-008-A Fig. 515A
**ON A/C ALL
3. Job Set-up
__________
Subtask 52-13-00-941-052
A. Get Access
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.
1EFF : ALL 1 52-13-00Page 559 1 1 Aug 01/05 1 1 1CES 1
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)
Put the access platform in position in front of the passenger/crew door 832 or 842.
(2)
Open the applicable passenger/crew door (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 52-13-00-865-056
B. 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
**ON A/C 001-002,
Subtask 52-13-00-010-058
C. Removal of Component
(1)
Remove the escape slide (Ref. TASK 25-62-44-000-002).
(2)
Remove the door lining (Ref. TASK 25-23-46-000-002)
(a)
For the left door:
(b)
For the right door:
(3)
Remove the door insulation.
(4)
Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
R 1EFF : ALL 1 52-13-00Page 560 1 1 May 01/05 1 1 1CES 1R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-13-00-010-058-A
C. Removal of Component
(1)
Remove the escape slide (Ref. TASK 25-62-44-000-002).
(2)
Remove the door lining (Ref. TASK 25-23-46-000-002)
(a)
For the left door:
(b)
For the right door:
(3)
Remove the door insulation.
(4)
Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
**ON A/C ALL
4. Procedure
_________
**ON A/C 001-002,
(Ref. Fig. 515/TASK 52-13-00-991-008) R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 515A/TASK 52-13-00-991-008-A)
**ON A/C ALL
Subtask 52-13-00-820-051
A. Load Adjustment of the Control Handle
**ON A/C 001-002,
(Ref. Fig. 515/TASK 52-13-00-991-008)
1EFF : ALL 1 52-13-00Page 561 1 1 Aug 01/05 1 1 1CES 1
Load Adjustment of the Control Handle of the AFT Passenger/Crew Door
Figure 515/TASK 52-13-00-991-008
R 1EFF : 001-002, 1 52-13-00Page 562 1 1 May 01/05 1 1 1CES 1
Load Adjustment of the Control Handle of the AFT Passenger/Crew Door
Figure 515A/TASK 52-13-00-991-008-A
R 1EFF : 003-049, 051-099, 101-149, 151-199, 1 52-13-00Page 563 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 515A/TASK 52-13-00-991-008-A)
**ON A/C ALL
(1)
Take a dynamometer capacity
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2(70)
