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时间:2011-03-21 08:32来源:蓝天飞行翻译 作者:admin
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 31.71 lbf.ft).

 (9)
 Push in the release stud (7) and insert the ball end of the manual inflation cable (8) in the regulator valve assembly.


 NOTE : If the length of the manual inflation cable (8) is not
____ correct, you must adjust the position of the manual inflation handle (27).
 EFF : 301-399, 25-62-49Page 412

May 01/05
R
 CES


 (10)
 Let go of the release stud (7).

 (11)
 Carefully pull the manual inflation cable (8) and make sure that the ball end is correctly installed.

 (12)
 Install the nipple (6) of the automatic inflation cable (25) in the release-lever (21).

 (13)
 Close the spring safety clamp (5). NOTE : When you close the spring safety clamp on the release-lever,

____ you must safety the clamp in position with lockwire. Wind the lockwire around the two splayed ends of the spring clamp arms and twist the ends of the lockwire together.

 (14)
 Safety the spring safety clamp (5) with MISCELLANEOUS (Material No. 19-010).

 (15)
 Remove the blanking caps from the electrical connectors.

 (16)
 Make sure that the electrical connectors are clean and in the correct condition.

 (17)
 Connect the electrical connector (12).

 (18)
 Put the bonding strap (11) in position and install and tighten the screw (9) and the washer (10). Make good any damage to the protective coating and/or sealant (Ref. TASK 20-28-00-912-004).

 (19)
 Remove the lockpin assembly (3) from the regulator valve assembly of the inflation reservoir (19).

 (20)
 Put the lockpin assembly (3) in the pocket (4).


 5. Close-up
________ Subtask 25-62-49-410-050
 A. Close Access
 (Ref. Fig. 401/TASK 25-62-49-991-001)

 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 EFF : 301-399, 25-62-49Page 413

May 01/05
R
 CES


 (2)
 Do one of the two applicable steps:

 -Close the access panel (1) and push the quick-release fasteners
 (22) to lock the access panel (1).
 -Install the cover (2) and push the quick-release fasteners (22) to lock the cover (2). Close the door of the overhead stowage compartment.

 (3)
 Put the exit safety barrier strap in the retracted position.

 (4)
 Remove the warning notice(s).

 (5)
 Close the emergency exit-door from the passenger compartmant (Ref. TASK 52-22-00-410-001).

 (6)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


 Subtask 25-62-49-862-050
 B. De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).

 

 EVACUATION SIGNALING EQUIPMENT - DESCRIPTION AND OPERATION__________________________________________________________
 1. General_______ The evacuation signaling equipment is operated by the captain or purser in an emergency (on the ground or on water) if the aircraft has to be evacuated. The system gives a signal to the cabin crew to start the evacuation of the passengers and crew. The essential busbar supplies electrical power to the system.
R  2. Component Location__________________ (Ref. Fig. 001) 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 
R  (Ref. Fig. 002) 
R  **ON A/C 401-499, 
R  (Ref. Fig. 002A) 
R  **ON A/C ALL 
R  (Ref. Fig. 003, 004)
 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF. -------------------------------------------------------------------------------2WP CAPT & PURS 21VU 211 3WP COMMAND 21VU 211 5WP WARNING HORN 48VU 210 7WP HORN SHUT OFF 21VU 211

 EFF : ALL
25-63-00Page 1
Aug 01/05


R  Overhead Panel Evacuation Signaling Components Figure 001
 EFF :  ALL  25-63-00 Page 2 Nov 01/03
 CES 

 

 Location of Evacuation Signaling Components - FWD Cabin Figure 002 
R  EFF : 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,  25-63-00 Page 3 Aug 01/05
 CES 

 

R R  Location of Evacuation Signaling Components - FWD Cabin Figure 002A 
R  EFF :  401-499,  25-63-00 Page 4 Aug 01/05
 CES 

 

 Location of Evacuation Signaling Components - AFT Cabin Figure 003
R  EFF : CES  ALL  25-63-00 Page 5 May 01/04 
 
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