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时间:2011-03-21 13:44来源:蓝天飞行翻译 作者:admin
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 4. Procedure_________
 Subtask 27-14-00-220-054
 A. Check of the Oscillation of the Servo Control of Each Aileron
 (1) Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
 (2) On the dial indicator, measure the amplitude of the oscillations. If the amplitude is more than 1 mm (0.0393 in.), replace the servovalve of the servo control (33CE3, 33CE4).
 (3) Pressurize the Green hydraulic system (Ref. TASK 29-23-00-863-001).
 (4) Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).
 (5) On the dial indicator, measure the amplitude of the oscillations. If the amplitude is more than 1 mm (0.0393 in.), replace the servovalve of the servo control (33CE1, 33CE2) (Ref. TASK 27-14-51-000-003) (Ref. TASK 27-14-51-400-003).
 5. Close-up________
 Subtask 27-14-00-080-051
 A. Removal of the Tools 
R R  (1) Remove the CHECK TOOL - AILERON, ELEVATOR, RUDDER (98D27303003001) or CHECK TOOL (ORAP) - AILERON, ELEVATOR, RUDDER (98D27303022000).
 (2) Remove the PIN-SIDE STICK LOCKING (98D27903500000).

 

 Subtask 27-14-00-860-055
 B. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the Green hydraulic system (Ref. TASK 29-23-00-864-001).

 (2)
 On the panel 23VU, push the FLT CTL/SEC 1 pushbutton switch (on this pushbutton switch, the OFF legend goes off).

 (3)
 On the panel 24VU, push the FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches (on these pushbutton switches the OFF legend goes off).

 (4)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).


 Subtask 27-14-00-942-062
 C. Remove the maintenance equipement.
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).


 1EFF : ALL 1 27-14-00Page 615 1 1 May 01/05R 1 1 1CES 1


 AILERON - REMOVAL/INSTALLATION
______________________________
 TASK 27-14-41-000-001
 Removal of the Aileron
 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.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 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
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific crane
 No specific safety barriers
 No specific trestle
 No specific warning notice
 No specific access platform 3.8 m (12 ft. 6 in.)


R  SL90-314-5625 1 TOOL - EXTRACTION, TAB WASHERS STA-LOK NSA5454 SL90-314-7500 1 TOOL - EXTRACTION, TAB WASHERS STA-LOK NSA5454
R  SL90-315-5625 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 SL90-315-7500 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 98D27104001000 1 LIFTING FRAME ASSEMBLY (AILERON) 98D27104002001 1 SUPPORT-AILERON ACTUATOR B. Referenced Information


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-22-00-000-001 Removal of STA-LOK Nuts and Lockwashers
 23-61-41-000-001 Removal of the Static Discharger
 27-50-00-866-009 Retraction of the Flaps on the Ground
 29-10-00-864-001 Depressurize the Green Hydraulic System
 29-10-00-864-003 Depressurize the Blue Hydraulic System
 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
 57-51-37-000-005 Removal of the Access Panels 575KB(675KB),

 575LB(675LB), 575MB(675MB)
 57-51-37-000-007 Removal of the Access Panel 575AT(675AT)
 
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