(2)
Make sure that the PIN-SIDE STICK LOCKING is in the CAPT and F/O side stick controllers.
(3)
Make sure that the warning notices are in the flight compartment to tell persons not to operate the flight controls.
(4)
Make sure that the warning notices are in position to tell persons not to operate the hydraulic systems.
(5)
Make sure that the access platforms are in position at zone 334 and/or zone 344.
(6)
Make sure that the horizontal stabilizer trailing edge panels have been removed as necessary (Ref. TASK 55-13-11-000-001).
(7)
Make sure that the elevator leading edge panels have been removed as necessary (Ref. TASK 55-22-11-000-001).
Subtask 55-16-42-865-052
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 R 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 R 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 R
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 55-16-42-140-050
C. Cleaning
(1) Remove the old sealant from the hinge arm fittings and the hinge arms. Use a nonmetallic scraper.
Subtask 55-16-42-110-050
D. Cleaning
(1) Clean the mating surfaces of the hinge arm fittings and the hinge arms and the adjacent areas with CLEANING AGENTS (Material No. 11-008).
R 4. Procedure_________
R (Ref. Fig. 401/TASK 55-16-42-991-001-A)
R Subtask 55-16-42-420-050
R A. Installation of the Hinge Arm End Fittings
R R (1) Apply SEALANTS (Material No. 09-005) to the mating surfaces of the hinge arm fitting (1) and the hinge support No. 1.
R (2) Put the hinge arm end fitting (1) in position on the hinge arm (6).
R (3) Install the bolts (5)and wet with SEALANTS (Material No. 09-001).,
R (4) Install the washers (4) and the nuts (3).
R (5) Safety the nuts (3) with new cotter pins (2)
R R (6) Connect the hinge arm end fitting (1) to its corresponding attach fitting (7) (Ref. TASK 27-34-41-400-001).
R Subtask 55-16-42-420-054-A
R B. Installation of the Hinge Arm End Fitting No 4
R R (1) Apply SEALANTS (Material No. 09-005) to the mating surfaces of the hinge arm fitting (42) and the hinge support No. 4.
R (2) Put the hinge arm end fitting (9) in position on the hinge arm (14).
R (3) Install the bolts (9) and wet with SEALANTS (Material No. 09-001).
R (4) Install the washers (12) and the nuts (11).
R (5) Safety the nuts (11) with new cotter pins (10).
R R (6) Connect the hinge arm end fitting (9) to the attach fitting (15) (Ref. TASK 27-34-41-400-001).
R (7) Install the elevator support strut (8) (Ref. TASK 55-16-48-400-001).
R 5. Close-up________
Subtask 55-16-42-410-051
A. Visual Inspection
(1) Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 55-16-42-410-050
B. Close Access
(1) Install the horizontal stabilizer trailing edge panels (Ref. TASK 55-13-11-400-001).
(2) Install the elevator leading edge panels (Ref. TASK 55-13-11-400-001)
Subtask 55-16-42-942-051
C. Remove Ground Equipment
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Remove the warning notice(s).
(3) Remove the access platform(s).
Subtask 55-16-42-081-050
D. Remove Locking Devices
(1) Remove the PIN-SIDE STICK LOCKING (98D27903500000) from the CAPT and F/O side stick controllers.
Subtask 55-16-42-865-050
E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 19CE1, 19CE2, 19CE3, 15CE1, 16CE1, 15CE2, 16CE2 SUPPORT STRUTS - ELEVATOR - REMOVAL/INSTALLATION
________________________________________________
TASK 55-16-48-000-001
Removal of the Elevator Support Struts
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
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 STABILIZERS 安定面(50)
