-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1. Reason for the Job
__________________
Refer to the MPD TASK: 575900-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notices No specific 5.0 mm (0.2 in.) dia. non-metallic probe No specific adjustable platform 4.0 m (13 ft. 1 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
1EFF : ALL 1 57-59-00Page 601 1 1 May 01/05R 1 1 1CES 1
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-59-00-991-002 Fig. 601
**ON A/C 301-399,
57-59-00-991-002-A Fig. 601A
**ON A/C ALL
3. Job Set-up
__________
Subtask 57-59-00-941-051
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(3)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-59-00-010-051
B. Get Access
(1) Put the adjustable platform in position below the applicable drain holes at zones 533(633), 532(632), 531(631).
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 601/TASK 57-59-00-991-002)
Drains in the T/E Devices
Figure 601/TASK 57-59-00-991-002
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-59-00Page 603 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
**ON A/C 301-399,
(Ref. Fig. 601A/TASK 57-59-00-991-002-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-59-00-210-051
A. Inspection
(1) Examine the drain-holes in the flap track fairing for blockage. If the drain-holes are blocked, push a 5.0 mm (0.2 in.) dia. non-metallic probe through the hole to remove the obstruction.
(2) Find the cause of the blockage.
**ON A/C 301-399,
Subtask 57-59-00-210-051-A
A. Inspection
(1)
Examine the drain-holes in the flap track fairing for blockage. If the drain-holes are blocked, push a 5.0 mm (0.2 in.) dia. non-metallic probe through the hole to remove the obstruction.
(2)
Find the cause of the blockage.
(3)
Examine the drain-holes in the outboard flap trailing edge, between the rear spar, L-Profile and end ribs for blockage. If the drain-holes are blocked, push a 5.0 mm (0.2 in.) dia. non-metallic probe through the hole to remove the obstruction.
(4)
Find the cause of the blockage.
R Drains in the T/E Devices
R Figure 601A/TASK 57-59-00-991-002-A
1EFF : 301-399, 1 57-59-00 Page 605
1 1 May 01/04
1 1
1CES 1
R **ON A/C ALL
5. Close-up
________
Subtask 57-59-00-410-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the access platform(s).
Subtask 57-59-00-942-051
B. Removal of Equipment
(1)
Remove the warning notice(s).
(2)
Remove the safety barriers.
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
AILERONS - DESCRIPTION AND OPERATION
____________________________________
1. General
_______
(Ref. Fig. 001)
The aileron is installed on the fixed structure of the trailing edge. It is
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼5(81)
