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时间:2011-03-21 08:20来源:蓝天飞行翻译 作者:admin
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 - Release the control switch S1.  - the seat stays locked in this
 position.
 - Set the control switch S1 to  - the motor stops automatically when
 down until the seat is in its  the seat gets to its maximum down
 maximum down position, then  position.
 release it.

 EFF : ALL

25-11-51Page 408


 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-Set the control switch S2 to  - the motor stops automatically when rearward until the seat is in the seat gets to the stowed position. the stowed position, then release it.
 -On the panel 301VU (500VU):
 -
Put the CONSOLE/FLOOR switch in  - Under the Captain/First Officer seat the BRT position , the four lamps come on.

 -
Put the CONSOLE/FLOOR switch in  - The four lamps go off.
 the OFF position.

 

 5. Close-up
________ Subtask 25-11-51-862-051
 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 Subtask 25-11-51-410-050
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the access door 811.

 (3)
 Remove the access platform(s).


 EFF : ALL

25-11-51Page 409


 SEAT - CAPTAIN/FIRST OFFICER (3MS,4MS) - INSPECTION/CHECK
_________________________________________________________
 TASK 25-11-51-200-001
 Inspection/Check of the Captain/First Officer Seat (3MS,4MS)

 1.
 Reason for the Job

__________________
 Visual inspection of seat structure and attachment.


 2.
 Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-11-00-200-002  Inspection/Check of the Shoulder Harness and Seat Belt
 3. Procedure
_________ Subtask 25-11-51-210-050
 A. Inspection Check of the Captain/First Officer Seat
 (1)
 Make sure that the upholstery of the seat is not worn or damaged.

 (2)
 Make sure that the cushion of the seat is in the correct condition.

 (3)
 Make sure that the structure of the seat has no damage or cracks.

 (4)
 Make sure that the paint is not damaged.

 (5)
 Make sure that you can read the identification plates. Make sure that the identification plates and the position indicator are attached correctly.

 (6)
 Make sure that the welded and riveted sections are in the correct condition.

 (7)
 Make sure that the clearance is correct at the manual mode control-levers.

 (8)
 Make sure that the seat belt and the buckle are in the correct condition (Ref. TASK 25-11-00-200-002).


 EFF : ALL

25-11-51Page 601


 (9) Make sure that the electrical bundle is in the correct condition.
 (10) Make sure that the 8 bolts that attach the seat to the floor have no corrosion and that they are installed correctly.
 EFF : ALL

25-11-51Page 602


 TASK 25-11-51-200-002
1. Reason for the Job
R Check of Adjustment of Seat Control Cables __________________ Refer to the MPD TASK: 251100-02
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
81100ST1-015003 1 ADJUSTMENT GAGE - LEVERS, CAPT/F/O SEATS
 81700ST1-015003 1 ADJUSTMENT GAGE - LEVERS, CAPT/F/O SEATS

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 24-42-00-861-001 Energize the Ground Service Network from the External
 Power 25-11-51-000-001 Removal of the Captain/First Officer Seat (3MS, 4MS) 25-11-51-991-003 Fig. 601
 3. Job Set-up
__________ Subtask 25-11-51-860-051 R A. Aircraft Maintenance Configuration
 (1) Energize the aircraft electrical circuits
 
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