Subtask 55-20-00-941-053
B. Safety Precautions
(1)
Install the locking devices.
(a)
Put the PIN-SIDE STICK LOCKING in the CAPT and F/O side sticks.
(b)
Install the TOOL-ELEVATOR NEUTRAL SETTING on the elevator.
(2)
Put the WARNING NOTICE in the flight compartment to tell persons not to operate the flight controls.
(3)
Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 334/344.
Subtask 55-20-00-865-056
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 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 55-20-00-010-053
D. Get Access
R (1) Remove the horizontal stabilizer tips 332AB/342AB (Ref. TASK 55-24-R 11-000-001).
Subtask 55-20-00-560-050
E. Preparation of the Inspection Area
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1)
Make sure that the outer surface of the inspection area is clean and smooth.
(2)
If necessary, clean the surface of the inspection area with a MISCELLANEOUS (Material No. 19-003) moist in CLEANING AGENTS (Material No. 11-010) until contamination is removed. Do not let the cleaning agent dry on the surfaces.
4. Procedure
_________
(Ref. Fig. 604/TASK 55-20-00-991-004) Subtask 55-20-00-210-056
A. Detailed Inspection
(1)
Make a detailed inspection of the external surface of the elevator outboard rib for corrosion.
(2)
If there is damage, look for the allowable damage limits and the applicable repair procedure. (Ref. SRM 552100 PB 101)
5. Close-up
________ Subtask 55-20-00-410-056
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the elevator stabilizer tips 332AB/342AB. (Ref. TASK 55-14-11-400-001)
Subtask 55-20-00-865-057
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2, 19CE3
Subtask 55-20-00-942-053
C. Removal of Equipment
(1)
Remove the locking devices.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : ALL 1 55-20-00Page 623 1 1 May 01/05 1 1 1CES 1
Inspection of Outboard Rib, LH/RH Figure 604/TASK 55-20-00-991-004
R 1EFF : 1 1 1CES ALL 1 111 55-20-00 Page 624 May 01/05
ELEVATOR SPAR BOX - DESCRIPTION AND OPERATION
_____________________________________________
R 1. General.________
R A. Elevator Spar Box.
R - The elevator spar box is the primary structural component of the
R elevator. All other components are attached to it.
R 2. Description___________
R (Ref. Fig. 001)
R A. Elevator Components.
R - The structure of the elevator has a front spar, an upper and a lower
R skin panel and four ribs. All components are made of laminations of
R Carbon Fiber Reinforced Plastic (CFRP).
R B. Skin Panels.
R - The skin panels are attached to the front spar and to the ribs. Hi-Lok
R fasteners attach them to the front spar and to the ribs. Honeycomb
R cores make them stronger. Screws connect the aft joint of the skin
R panels. Rivets attach a light-alloy profile to the trailing edge to
R make the trailing edge stronger. The light-alloy profile is sealed.
R C. Elevator Fittings.
R - There are six hinge fittings and two actuator fittings attached to the
R front spar. Six nose ribs make the leading edge stronger. Hi-Lok
R fasteners attach the fittings and the ribs.
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 STABILIZERS 安定面(60)
