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时间:2011-03-21 14:21来源:蓝天飞行翻译 作者:admin
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57-55-11-000-005
57-55-11-010-001
27-54-61-991-016 27-54-61-991-019 27-54-61-991-017 27-54-61-991-026 27-54-61-991-030 27-54-61-991-021 27-54-61-991-018 27-54-61-991-015 27-54-61-991-020 27-54-61-991-022-A
3. Job Set-up
__________
 Subtask 27-54-61-941-056
 A. Safety PrecautionsRemoval of the Inboard and Outboard Flap Hoisting-SlingInstallation of the Inboard and Outboard Flap Hoisting-SlingExtension of the Flaps on the GroundRetraction of the Flaps on the GroundRemoval of the Interconnecting StrutRemoval of the Right Angle Gearbox 6203CM,(6253CM)Removal of the Flap Kink-SealsExtension-Retraction of the Spoilers for MaintenanceRemoval of the Aft Movable FairingRemoval of the Access Panels 573AB(673AB), 573BB(673BB), 573CB(673CB)Removal of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)Removal of the Inboard and Outboard Flap Tab Hinge-FairingsTo Lower the Flap Track No. 2 Movable Fairing for AccessFig. 416Fig. 417Fig. 418Fig. 419Fig. 420Fig. 421Fig. 422Fig. 423Fig. 424Fig. 425
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice on panel 400VU to tell persons not to operate the landing gear.


 1EFF : 301-399, 1 27-54-61Page 499 1 1 Aug 01/05R 1 1 1CES 1


 (3) Put a warning notice in position to tell persons not to operate the flight controls.
 Subtask 27-54-61-860-053
 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 (1)
 Make sure that the flaps are in the fully retracted position (Ref. TASK 27-50-00-866-009).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the slat/flap control lever.


 Subtask 27-54-61-865-052
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 Subtask 27-54-61-010-052
 D. Get Access
 (Ref. Fig. 416/TASK 27-54-61-991-016)

 (1)
 Put the access platform in position below the applicable inboard flap.

 (2)
 Lower the flap track No. 2 movable fairing for access (Ref. TASK 57-55-11-010-001).

 (3)
 Remove the pylon aft movable fairing (Ref. TASK 54-55-00-000-001).

 (4)
 Move the flaps (Ref. TASK 27-50-00-866-008) to get access to the fasteners of the rubbing strip (2).

 (5)
 Remove the support (1) and the rubbing strip (2).


 1EFF : 301-399, 1 27-54-61Page A400 1 1 Aug 01/05R 1 1 1CES 1


 Details of the Wing to Fuselage Panels
 Figure 416/TASK 27-54-61-991-016
 1EFF :  301-399,  1  27-54-61 Page A401 
1  1  Aug 01/05
 1R 1 
1CES  1

 

 (6) Remove the fairing panels 193AB(194AB) and 193BB(194BB) as follows: NOTE : The attachment screws of the fairing panels are not all the
____ same length. Record the position of the screws as you remove them. This will make sure that they are installed correctly when the fairing panel is installed.
 (a)
 For the fairing panel 193AB(194AB):

 (b)
 For the fairing panel 193BB(194BB): 1 Hold the fairing panel and remove the attachment screws.


 1_ Hold the fairing panel and remove the attachment screws and
 washers.
 2_ Remove the fairing panel from the aircraft.

_ 2 Hold the sliding panel (3) in position so that it does not
_ move as the fairing panel is removed.
 3 Move the fairing panel rearward, away from the sliding panel
_
 (3) and off the aircraft. 4 Remove the sliding panel (3) from the flap trunnion.
_
 (7)
 Remove the applicable wing access panels: (Ref. Fig. 416/TASK 27-54-61-991-016)

 (a) For the LH wing:
 -
remove 573CB (Ref. TASK 57-51-37-000-002)

 -
remove 575AB, 575BB (Ref. TASK 57-51-37-000-004).


 (b) For the RH wing:
 -
remove 673CB (Ref. TASK 57-51-37-000-002)

 -
remove 675AB, 675BB (Ref. TASK 57-51-37-000-004).

 

 (8)
 Remove the hinge 1A fairings (Ref. TASK 57-55-11-000-005).

 (9)
 Disconnect the applicable torque shaft from the right angle gearbox (Ref. TASK 27-54-41-000-001).
 
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