(2)
Retract the flaps (Ref. TASK 27-50-00-866-009).
(3)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).
(4)
Remove the PIN-SIDE STICK LOCKING (98D27903500000) and the warning notice from each side-stick controller.
(5)
Close access door(s) in zone(s) 580, 680.
(6)
Remove access platform(s).
(7)
Make sure that the work area is clean and clear of tool(s) and other items.
(8)
Put a warning notice in the cockpit to tell the crew that the spoiler servocontrol is deactivated.
(9)
Make an entry in the log-book and record the defective servocontrol.
(10) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 27-64-00Page 408 1 1 Aug 01/05R 1 1 1CES 1
TASK 27-64-00-440-001
Reactivation of the Spoiler Servo Control
1. Reason for the Job
__________________
Refer to the MMEL TASK: 27-64-01
Spoiler Hydraulic Actuation
Spoiler
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific metal rod (tommy bar) dia. 4mm (0.1574 in.).
No specific metal rod (tommy bar) dia. 4mm (01574 in.).
No specific warning notices
No specific access platform 3.5 m (11 ft. 6 in.)
98D27603002001 1 SPOILER MAINTENANCE KEY
98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
98D27903500000 2 PIN-SIDE STICK LOCKING
B. 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 27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
after Operation of the PTU 29-24-00-864-001 Depressurize the Yellow Hydraulic System R TSM CH27 (for corrective action)
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
27-64-00-991-007 Fig. 401
**ON A/C 051-051,
27-64-00-991-007-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 27-64-00-860-058
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Remove the warning notice(s).
(3)
Extend the flaps (Ref. TASK 27-50-00-866-008).
(4)
On the overhead panel 23VU :
-Release the FLT CTL/SEC 1 pushbutton switch (on this pushbutton switch, the OFF legend comes on).
(5)
On the overhead panel 24VU :
-Release the FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches (on these pushbutton switches, the OFF legends come on).
(6)
On the panel 114VU, put the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) in position on the flap and slat control lever.
(7)
Put the PIN-SIDE STICK LOCKING (98D27903500000) in position on each side-stick controller.
(8)
Put the warning notices on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
(9)
Depressurize the hydraulic system related to the spoiler that you must reactivate.
(a)
For the spoiler 1 or 5, depressurize the Green hydraulic system (Ref. TASK 29-23-00-864-001).
(b)
For the spoiler 2 or 4, depressurize the Yellow hydraulic system (Ref. TASK 29-24-00-864-001).
(c)
For the spoiler 3, depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).
(10)
Put the access platform in position in :
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵6(103)
