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时间:2011-03-22 06:40来源:蓝天飞行翻译 作者:admin
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 deactivated SEC(s).

 

R NOTE : The spoilers associated
____ R to the SEC deactivated R will be inoperative.
 5. Close-up
________
 Subtask 27-94-00-860-057
 A. Aircraft Maintenance Configuration
 (1)
 On the overhead panel, on the FLT CTL panel 23VU or 24VU, put a warning notice on the pushbutton switch related to the SEC that you deactivated.

 (2)
 Make an entry in the log book.

 (3)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 

 

 TASK 27-94-00-440-002
 Reactivation of the Spoiler Elevator Computer (SEC)

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002  Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
 3. Job Set-up
__________ Subtask 27-94-00-860-058
 A. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 4. Procedure
_________ Subtask 27-94-00-440-050
 A. Reactivation of the Spoiler Elevator Computer (SEC)
 (1)
 Remove the warning notice(s).

 (2)
 Close the circuit breaker(s) 21CE1 and 22CE (SEC1) or 21CE2 (SEC2) or 21CE3 (SEC3) related to the SEC that you must activate.

 (3)
 Do a trouble shooting of the reactivated SEC. Make the necessary corrections.


 1EFF : ALL 1 27-94-00Page 406 1 1 Feb 01/00R 1 1 1CES 1


 5. Close-up
________ Subtask 27-94-00-410-052
 A. Close Access
 (1)
 Install the protective cover on the battery power center 105VU.

 (2)
 Tighten the two screws.

 (3)
 Close the access door 822.

 (4)
 Remove the access platform(s).

 (5)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 

 

 SEC SYSTEM (SPOILER AND ELEVATOR COMPUTER) - ADJUSTMENT/TEST
____________________________________________________________
 TASK 27-94-00-710-002
 Operational Test of the Spoiler Elevator Computer 1 (SEC 1)
 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. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
R 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
R Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure


 3. Job Set-up
__________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 27-94-00-860-052
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).

 (3)
 
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