-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1.
Reason for the Job
__________________
Refer to the MPD TASK: 274100-02
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific tensiometer No specific warning notice No specific access platform 2.06 m (6 ft. 9 in.)
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B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 24-41-00-862-002 25-54-12-000-002 25-54-12-400-002 25-55-11-000-002 25-55-11-400-002 27-41-00-820-002 27-41-42-000-001 27-41-42-400-001 29-23-00-863-001
29-23-00-864-001 29-24-00-863-001 52-30-00-860-001 52-30-00-860-002
3. Job Set-up
__________ Subtask 27-41-00-860-060
Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerRemoval of the Ceiling Panels in the FWD Cargo CompartmentInstallation of the Ceiling Panels in the FWD Cargo CompartmentRemoval of the Ceiling Panels in the AFT Cargo Compartment - FR47/FR59Installation of the Ceiling Panels in the AFT Cargo Compartment -FR47/FR59Adjustment of the THS Control-Cables LengthRemoval of the Cable Tension RegulatorInstallation of the Cable Tension RegulatorPressurize 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 PumpOpen the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpClose the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Pressurize the Green and Yellow hydraulic systems with the electric pump (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-23-00-863-001).
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(3) Safety Precautions
(a)
On the center pedestal, make sure that the pitch-trim control-wheels are set to zero.
(b)
Put a warning notice on the pitch-trim control wheels to tell persons not to use the pitch trim.
(c)
Put a warning notice on the rudder pedals (CAPT and F/O) to tell persons not to operate them.
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 27-41-00-010-052
B. Get Access
(1)
Open the FWD and AFT cargo compartment doors (Ref. TASK 52-30-00-860-001).
(2)
Put the access platform in position.
(3)
Remove the ceiling panel 131BC in the cargo compartment (Ref. TASK 25-54-12-000-002).
(4)
Remove the ceiling panel 151BC in the cargo compartment (Ref. TASK 25-55-11-000-002).
R **ON A/C 151-199, 401-499,
Subtask 27-41-00-010-052-A
B. Get Access
(1)
Open the FWD and AFT cargo compartment doors (Ref. TASK 52-30-00-860-001).
(2)
Put the access platform in position.
(3)
Remove the ceiling panel 131MC in the cargo compartment (Ref. TASK 25-54-12-000-002).
(4)
Remove the ceiling panel 151FC in the cargo compartment (Ref. TASK 25-55-11-000-002).
**ON A/C ALL
4. Procedure
_________ Subtask 27-41-00-220-051
A. Check of the Correct Tension of the THS Mechanical Control Cables
(1)
Operate the THS fully five times and put it in the zero position.
(2)
In the cargo compartment, you can see four cables:
-
the two cables at right are the THS control cables
-
the two cables at left are the rudder control cables.
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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(99)
