98D27903500000 2 PIN-SIDE STICK LOCKING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
C. 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
27-50-00-866-008 Extension of the Flaps on the Ground
27-50-00-866-009 Retraction of the Flaps on the Ground
27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance
27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation
29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply
29-10-00-864-003 Depressurize the Blue Hydraulic System
29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric
Pump
29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
after Operation of the PTU
29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
29-24-00-864-001 Depressurize the Yellow Hydraulic System
27-64-00-991-001-A Fig. 501A
27-64-00-991-006 Fig. 502
27-64-00-991-002 Fig. 503
R 1EFF : 151-199, 401-499, 1 27-64-00Page 534 1 1 Aug 01/05 1 1 1CES 1
3. Job Set-up
__________ Subtask 27-64-00-860-064
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Make sure that the flaps are in the fully retracted position (Ref. TASK 27-50-00-866-009).
(3)
On the center pedestal, make sure that the SPEED BRAKE control lever is set to RET.
(4)
Install the PIN-SIDE STICK LOCKING (98D27903500000) on each side stick controller.
(5)
Put the warning notices on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
(6)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap and slat control lever.
(7)
Put a warning notice on the center pedestal to tell persons not to operate the SPEED BRAKE control lever.
Subtask 27-64-00-010-059
B. Get Access
(1)
Put the access platform in position at the access door 822.
(a)
Open the access door 822.
(b)
On the battery power center 105VU:
-loosen the two screws and remove the protective cover.
(2)
Put the access platform in position at:
(a)
the zone 580 for the left spoilers.
(b)
the zone 680 for the right spoilers.
R 1EFF : 151-199, 401-499, 1 27-64-00Page 535 1 1 Aug 01/05 1 1 1CES 1
(3) Open these access doors:
(a)
573BB for the left spoiler 1.
(b)
575BB for the left spoiler 2.
(c)
575DB for the left spoiler 3.
(d)
575EB for the left spoiler 4.
(e)
575GB for the left spoiler 5.
(f)
673BB for the right spoiler 1.
(g)
675BB for the right spoiler 2.
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6(115)
