(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (Ref. TASK 27-00-00-080-002).
(3)
Set the flap/slat control lever to position 0.
(4)
Make sure that on the upper display unit of the ECAM system the flap position bar moves to the set position.
5. Close-up
________ Subtask 27-50-00-860-057
A. Aircraft Configuration
(1)
Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002).
(2)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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Subtask 27-50-00-865-059
R R R B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
R -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-50-00-942-053
C. 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 27-50-00-866-009- 01 Retraction of the Flaps/Slats on the Ground 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 : IF THE THRUST REVERSER COWLS ARE OPEN, MAKE SURE THAT THE HALF DOORS
_______ OF THE THRUST REVERSER ARE RETRACTED BEFORE YOU EXTEND THE SLATS. IF THE DOORS ARE EXTENDED, YOU CAN CAUSE DAMAGE TO THE SLATS AND HALF DOORS WHEN THE SLATS EXTEND.
1.
Reason for the Job
__________________
To retract the flaps and slats at the same time
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice(s) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
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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 27-00-00-080-002 Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000) 27-00-00-480-002 Installation of the Flap/Slat Control-Lever Locking
Tool (98D27803000000) 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply 29-10-00-864-002 Depressurize the Yellow Hydraulic System 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU) 29-23-00-860-002 Connection of the Isolation Coupling of the Power
Transfer Unit (PTU) 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
3. Job Set-up
__________
Subtask 27-50-00-941-064
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put the warning notice(s) in position to tell persons that the flap and slat systems are in operation.
(3)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is in position on the flap/slat control lever (Ref. TASK 27-00-00-480-002).
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Subtask 27-50-00-860-067
B. Aircraft Maintenance Configuration
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱3(194)
