Operational Test of the Toilet UnitOperational Test of the Waste/Water Drain System Installation of the Auxiliary Power Unit (APU) -4005KM (GTCP 36-300)Installation of the Power Plant (APU) (APS 3200)Installation of the Power Plant (APU) (131-9(A)) Preservation / Storage / De-preservation of the Engine (GTCP 36-300)Preservation/Storage/Return to Service of APU (APS 3200)Preservation/Storage/Return to Service of APU (131-9(A))Repair of Corroded AreasOperational Check of Single Drain Pipe Aft of FR70 from OutsideGeneral Inspection of the Pylon Drain SystemRemoval of the Power PlantEngine Automatic StartEngine Manual StartMinimum Idle CheckEngine ShutdownDepreservation
(1)
Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position near the aircraft.
(2)
Put a WARNING NOTICE in position in the cockpit to tell persons not to operate the systems while you prepare the aircraft for operation again.
4. Procedure
_________
Subtask 10-30-00-210-074
A. Visual Inspection
(1) Do a visual inspection of the aircraft for impacts by foreign R objects, bird nests, fluid leakages (hydraulic fluid, fuel), missing R parts, obstruction and corrosion of:
(a)
the upper and the lower surfaces of the wing
(b)
the nacelles and the pylons
(c)
the external surfaces of the fuselage
(d)
the flight control surfaces
(e)
the leading and the trailing edges of the horizontal and vertical stabilizers
(f)
the external skin of:
-
the passenger/crew doors
-
the cargo doors
-
the frame around the doors.
(g)
the external handle of the passenger/crew doors
(h)
the drains 1 In the lower fuselage (Ref. TASK 53-59-00-210-001)
_
2 On the pylons (Ref. TASK 54-50-00-200-001)
_
3 In all other locations.
_
(i)
the toilet areas
(j)
all steel parts for corrosion.
(2)
If you find corrosion, remove it (Ref. TASK 51-74-11-300-001).
(3)
Make sure that:
-
the communication and navigation antennas are correctly installed
-
the static dischargers are correctly installed and in correct condition (Ref. TASK 23-61-00-200-001).
(4) Do a check of the avionics compartment.
Subtask 10-30-00-615-051
B. Cleaning of the Aircraft
(1) Remove all the STORAGE PRESERVATION (Material No. 15-002) and adhesive tapes.
R (2) We recommend that you clean the aircraft externally (Ref. TASK 12-21-11-615-001).
Subtask 10-30-00-420-067
C. Aircraft Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
On the overhead panel 25 VU, on the CABIN PRESS section:
-release the DITCHING pushbutton switch to open the avionics ventilation skin valves and the outflow valve.
NOTE : Make sure that the avionics ventilation continues to operate
____
correctly.
(3) Install and connect the batteries 2PB1 and 2PB2 and make sure that the charge is correct (Ref. TASK 24-38-51-400-001).
Subtask 10-30-00-554-053
D. Removal of the Protections
(1)
Remove all the protective equipment from the engines, the APU, the probes.
(2)
Remove the protection from the cockpit, the passenger seats and the carpets.
Subtask 10-30-00-710-118
E. Inspection of the Doors
(1) Make sure that the doors open and close correctly.
Subtask 10-30-00-420-068
F. Installation of the Equipment Removed
(1) Install the Digital Flight Data Recorder (Ref. TASK 31-33-55-400-002).
(2) Install the Cockpit Voice Recorder (Ref. TASK 23-71-35-400-001).
(3) Install the debris guard, the impeller and the shroud of the brake fans (Ref. TASK 32-48-51-400-005).
R R (4) Install the fire-extinguisher bottles and cartridges if removed of: - the cargo compartment (Ref. TASK 26-23-41-000-004) - the engines (Ref. TASK 26-21-41-400-004) - the APU (Ref. TASK 26-22-41-400-001).
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM PARKING, MOORING, STORAGE & RETURN TO S(49)
