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时间:2011-03-27 12:52来源:蓝天飞行翻译 作者:航空
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 2. Component Description
_____________________ The spoiler is a wedge-shaped structure. It has carbon fiber top and bottom skins, sides and trailing edge profile, bonded to a honeycomb core. There are four machined aluminum-alloy attachment-fittings. These are the inboard and outboard hinge brackets (with links), the center hinge and the spoiler actuator attachment-fitting. The actuator attachment-fitting is installed within the center hinge. The spoiler is connected by the links and the center hinge to the rear spar.
 A titanium alloy rubbing strip is attached to the trailing edge of the spoiler, to prevent damage to the spoiler when the outboard flap is retracted. Seals are located at the inboard and outboard ends and along the leading edge of the spoiler.


 Spoiler 5
 Figure 001
 1EFF :  ALL  1  57-75-00 Page 2 
1  1  Feb 01/98
 1  1
 1CES  1

 

 SPOILER 5 - INSPECTION/CHECK____________________________
 TASK 57-75-00-200-001
 Detailed Visual Inspection of Spoilers 2, 3, 4 and 5 Upper and Lower Skins in Region of Center Hinge Fittings
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
 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. 
R R R R R  CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:_______ - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1. Reason for the Job__________________
 Refer to the MPD TASK: 577007-01
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific No specific No specific  safety barrierswarning noticesaccess platform 3 m (9 ft. 10 in.)

 

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
 Material No. 19-003  USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance ASRM 577000 (for corrective action) 57-75-00-991-001 Fig. 601
 3. Job Set-up
__________
 Subtask 57-75-00-941-050
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put warning notices in the cockpit to tell persons not to operate the spoilers.

 (3)
 Put warning notices in the cockpit to tell persons not to operate the flaps or slats.

 (4)
 Put the access platform in position below the applicable zone:

 -
for spoiler 2, below zone 583(683)

 -
for spoiler 3, below zone 584(684)

 -
for spoiler 4, below zone 585(685)

 -
for spoiler 5, below zone 586(686).

 


 1EFF : ALL 1 57-75-00Page 602 1 1 Aug 01/99R 1 1 1CES 1


 Subtask 57-75-00-860-050

 B. Aircraft Maintenance Configuration
 (1) Do a manual extension of the spoilers (Ref. TASK 27-60-00-866-002).
 (2) Make sure that the COLLAR-SAFETY, SPOILER (98D27604000000) is installed on the spoiler actuator.
 (3) Make sure the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.
 Subtask 57-75-00-865-051
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 4. Procedure_________
 (Ref. Fig. 601/TASK 57-75-00-991-001) 
R R R R R R  CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING_______ EDGE: - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 
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