(2)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001).
(3)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(4)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 27-41-00-410-057
B. Close Access
(1)
Install the protective cover on the battery power center 105VU.
(2)
Tighten the two screws.
1EFF : ALL 1 27-41-00Page 525 1 1 May 01/04R 1 1 1CES 1
(3)
Close the access door 822.
(4)
Remove the access platform(s).
1EFF : ALL 1 27-41-00Page 526 1 1 May 01/04R 1 1 1CES 1
TASK 27-41-00-820-002
Adjustment of the THS Control-Cables Length
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 CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
CAUTION : MAKE SURE THAT THE AIRCRAFT IS IN THE TEMPERATURE CONDITIONS (STABLE
_______ AMBIENT TEMPERATURE) SPECIFIED IN THE AIRCRAFT MAINTENANCE CONFIGURATION PARAGRAPH. CHANGES IN THE TEMPERATURE CAN CAUSE INCORRECT MEASUREMENTS.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific tensiometer No specific thermometer No specific warning notice No specific 1 ACCESS PLATFORM 2M (6 FT) No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 0U190360 1 PIN - RIGGING
1EFF : ALL 1 27-41-00Page 527 1 1 May 01/04R 1 1 1CES 1
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R 12-33-21-618-001 21-21-41-000-001 21-21-41-400-001 24-41-00-861-002
24-41-00-862-002
R R R R R R R 25-54-12-000-001 25-54-12-000-002 25-54-12-400-001 25-54-12-400-002 27-41-00-820-003 27-41-44-000-001 27-41-44-400-001 29-23-00-863-001
29-23-00-864-001
29-24-00-863-001
29-24-00-864-001 52-41-00-410-002 53-32-12-000-002 53-32-12-400-002 27-41-00-991-006 27-41-00-991-008
3. Job Set-up__________
Subtask 27-41-00-862-054
Pre-conditioning through the LP Ground Connection Removal of the Recirculation Filter 4012HM (4013HM) Installation of the Recirculation Filter 4012HM (4013HM)Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External Power Removal of the FWD Cargo Compartment Partition FR34 Removal of the Ceiling Panels in the FWD Cargo Compartment Installation of the FWD Cargo Compartment Partition FR34 Installation of the Ceiling Panels in the FWD Cargo CompartmentShortening of the THS Control CableRemoval of the THS Control CablesInstallation of the THS Control CablesPressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTUPressurize the Yellow Hydraulic System with the Electric PumpDepressurize the Yellow Hydraulic SystemClose the Avionics Compartment Doors after AccessRemoval of the Cabin Floor PanelsInstallation of the Cabin Floor PanelsFig. 505Fig. 506
A. Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-41-00-010-057
B. Get Access
(1)
Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 312AR.
(2)
Open the access door 312AR.
(3)
Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 811.
(4)
Open the access door 811.
(5)
Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 812.
(6)
Open the access door 812.
(7)
Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 824.
(8) 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱3(88)
