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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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27-00-00-480-002  Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000) 25-62-00-991-013 Fig. 404
 3. Job Set-up
__________ Subtask 25-62-00-860-062
 A. Aircraft Maintenance Configuration
 (Ref. Fig. 404/TASK 25-62-00-991-013)

 NOTE : The lock pin (1) and the pressure blanking-plug (5) are kept in a
____ pocket, which attaches to the inflation reservoir (1).
 EFF : 301-399,  25-62-00Page 418

May 01/05
R
 CES


 INTENTIONALLY BLANK

 

 Installation of the Enclosure Door Figure 404/TASK 25-62-00-991-013- 12 (SHEET 1)
R  EFF : CES  301-399,  25-62-00 Page 420 May 01/05 

 

 Installation of the Enclosure Door Figure 404/TASK 25-62-00-991-013- 22 (SHEET 2)
R  EFF : CES  301-399,  25-62-00 Page 421 May 01/05 

 

 (1)
 If the inflation reservoir (1) is charged, install the lock pin (3) in the regulator valve assembly (2).

 (2)
 If you remove an AFT, emergency-exit escape-slide:


 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
 BEFORE YOU START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 -Safety the flap (Ref. TASK 27-00-00-480-002).
 -Put a WARNING NOTICE on the slat/flap control lever to tell persons not to operate the flaps, during the installation procedure.
 (3)
 Put an ACCESS PLATFORM 2M (6 FT) in position adjacent to the related emergency-exit door.

 (4)
 Install the blanking plug (5) on the enclosure connection (4).


 4. Procedure
_________
 Subtask 25-62-00-040-053
 A. Installation Procedure of the Enclosure Door
 (Ref. Fig. 404/TASK 25-62-00-991-013)

 (1)
 Put the lower edge of the enclosure door (8) in the groove in the bottom of the enclosure (6).

 (2)
 Close the enclosure door (8) on the three ball-lock assemblies (7).

 (3)
 Push the head of the lock pin (12) with a SCREWDRIVER - PHILLIPS HEAD, then:

 -Apply force to the enclosure door (8) adjacent to the lock pin (13).
 -Remove the screwdriver.
 -Continue to push the enclosure door (8) until the lock pin (13) moves quickly back to a flush position with the surface of the enclosure door (8).

 (4)
 Do this procedure with each lock pin (13).


 EFF : 301-399, 25-62-00Page 422

May 01/05
R
 CES


 (5) If an AFT emergency-exit escape-slide is removed, install the fairing

 (10):
 (a)
 Engage the tongue-tabs (9) behind the belly fairing, and close the fairing (10).

 (b)
 Push the latch (11) into the fairing (10) until it engages behind the belly fairing.

 (c)
 Make sure that the latch (11) is flush with the outside surface of the fairing (10).


 (6) Make an entry in the logbook to record the procedure. Subtask 25-62-00-869-055
 B. System Consequences
 (1) On the programming and test panel (PTP), if the cabin assignment model (CAM) is programmed to monitor the inflation reservoirs (1):
 -the message 'SLIDE PRESSURE LOW' will show.
 5. Close-up
________ Subtask 25-62-00-860-063
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) from the slat/flap control lever.

 (3)
 Remove the warning notice(s).

 (4)
 Remove the access platform(s).

 


 TASK 25-62-00-440-004 Reactivation of the Enclosure
 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 25-60-02-C)
 Emergency - Escape Slide/Slide Raft
 Emergency Exit

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-62-47-000-001 Escape-Slide Enclosure - Removal 25-62-47-400-001 Escape-Slide Enclosure - Installation 25-62-49-000-001 Inflation Reservoir, Escape-Slide - Removal 25-62-49-400-001 Inflation Reservoir, Escape-Slide - Installation
 3. Job Set-up
__________ Subtask 25-62-00-010-072
 
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