(2)
Depressurize the applicable hydraulic reservoir (Ref. TASK 29-14-00-614-001).
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-81-00-942-051
C. Removal of Equipment
(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 safety barriers.
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 27-81-00Page 515 1 1 Aug 01/05R 1 1 1CES 1
TASK 27-81-00-710-002
Operational Test of the Wing-Tip Brake and the Pressure-Off Brake with the Ground Power Cart 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 TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______ R
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notices
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-38-00-710-001
24-41-00-861-002
24-41-00-862-002
27-51-00-750-001
27-80-00-869-004
29-10-00-863-001 29-10-00-863-003
R R R R 29-10-00-864-001 29-10-00-864-003 29-14-00-614-001 29-23-00-863-002 29-24-00-864-001 31-32-00-860-006
R 3. Job Set-up__________
Subtask 27-81-00-941-057
A. Safety Precautions
Operational Test of the Battery Charge Limiter (BCL), (without the CFDS)Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerAutomatic Integrity Test of the Slat and Flap Control ComputersReset of the Wing Tip Brake (WTB) of the Slat System on the GroundPressurize the Green Hydraulic SystemPressurize the Blue Hydraulic System with a Ground Power Supply Depressurize the Green Hydraulic SystemDepressurize the Blue Hydraulic SystemDepressurization of the Hydraulic Reservoirs Pressurize the Yellow Hydraulic System from the Green Hydraulic System through the PTU with the Ground Service CartDepressurize the Yellow Hydraulic SystemProcedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page
(1)
Put the safety barriers in position.
(2)
Put the warning notices in postion to tell persons that the slat and flap systems are in operation.
Subtask 27-81-00-860-055
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2) Make sure that the aircraft batteries are fully charged (Ref. TASK 24-38-00-710-001).
(3) Get access to the SYSTEM REPORT/TEST (F/CTL) page on the MCDU (Ref. TASK 31-32-00-860-006).
(4) Do the automatic integrity test of the two SFCC's, which includes Slat and Flap BITE tests of the two computers (Ref. TASK 27-51-00-750-001).
R (5) If the result of the BITE test indicates no faults but the WTB is applied, reset the WTB (Ref. TASK 27-80-00-869-004).
Subtask 27-81-00-865-064
R C. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(63)
