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时间:2011-03-21 14:12来源:蓝天飞行翻译 作者:admin
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R  Subtask 27-51-00-865-094 
R  C. Table of the circuit breakers used in this procedure: 
R R R R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20
 4. Procedure_________
 Subtask 27-51-00-865-081
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 8CV. 
R  Subtask 27-51-00-865-095 
R R  B. If necessary, remove the safety clip and tag and close the circuit breaker 12CV.

 

 Subtask 27-51-00-440-051
R C. Reactivation of the Slat and Flap Control Computer (SFCC) No. 2 Flap Channel
 (1)
 Do the trouble-shooting of the SFCC and do the applicable correction(s) (Ref. TSM 27 PB101).

 (2)
 Make an entry in the aircraft technical log to say that the SFCC No. 2 flap channel has been reactivated.


 5. Close-up
________
 Subtask 27-51-00-942-071

 A. Removal of Equipment
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 


 TASK 27-51-00-040-005
 Deactivation of the Slat and Flap Control Computer (SFCC) No. 2 Slat Channel
 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.
 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 27-51-01-B)
 Flaps Electrical Control and Monitoring
 Slat and Flap Control System (SFCS)
 SLAT channel

 NOTE : For the deactivation of the No. 2 flap channel of the SFCC, refer to
____
 TASK 27-51-00-040-001.

 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 safety barriers No specific warning notice
 1EFF : ALL 1 27-51-00Page 411 1 1 Feb 01/01R 1 1 1CES 1


 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002
24-41-00-862-002
27-50-00-869-006
27-51-00-710-003
27-51-00-710-004
R 29-10-00-863-001 R 29-10-00-863-002 R 29-10-00-863-003 R R 29-10-00-864-001 R 29-10-00-864-002 R 29-10-00-864-003
31-32-00-860-001
3. Job Set-up
__________
 Subtask 27-51-00-941-075
R A. Safety Precautions R Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerReset of the Wing Tip Brake (WTB) of the Flap System on the GroundOperational Test of the Wing Tip Brake and the Pressure Off Brake with the Ground Power CartOperational Test of the Wing Tip Brake and the Pressure Off Brake with the Engine Driven Pumps Pressurize the Green Hydraulic System Pressurize the Yellow Hydraulic System Pressurize the Blue Hydraulic System with a Ground Power Supply Depressurize the Green Hydraulic System Depressurize the Yellow Hydraulic System Depressurize the Blue Hydraulic SystemProcedure to Get Access to the SYSTEM REPORT/TEST Menu Page
R (1) Put the safety barriers in position.
 (2) Put a warning notice in position to tell persons not to operate the slats and flaps.
 Subtask 27-51-00-861-057
 B. Energize the Aircraft Electrical Circuits
R (1) Energize the aircraft electrical circuits R (Ref. TASK 24-41-00-861-002). R Subtask 27-51-00-865-096


 C. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19
 
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