A. Inspection
(1) Do a detailed visual inspection of the rudder attach fittings 6 and
7.
NOTE : If you find damage, refer to (Ref. ASRM 55-46-00-101).
____
5. Close-up
________
Subtask 55-40-00-916-051
A. Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to the inspection area.
R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
Subtask 55-40-00-410-054
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access panel 325DL (Ref. TASK 55-33-13-410-002).
(3)
Install the access panel 325EL (Ref. TASK 55-33-13-410-002).
(4)
Install the vertical stabilizer tip 324AT (Ref. TASK 55-34-11-400-001).
(5)
Remove the access platform(s).
(6)
Remove the warning notice(s).
(7)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Rudder Attach Fittings 6 and 7 Figure 603/TASK 55-40-00-991-003
1EFF : 1 1R 1CES ALL 1 11 1 55-40-00 Page 622 Feb 01/02
R **ON A/C 106-149, 159-199, 211-299, 301-399, 401-499,
Subtask 55-40-00-410-054-A
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access panel 325DL (Ref. TASK 55-33-13-410-002).
(3)
Install the access panel 325EL (Ref. TASK 55-33-13-410-002).
(4)
Install the access panel 326CT at the rudder attach fitting No. 7 (Ref. TASK 55-42-13-400-001).
(5)
Install the vertical stabilizer tip 324AT (Ref. TASK 55-34-11-400-001).
(6)
Remove the access platform(s).
(7)
Remove the warning notice(s).
(8)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
**ON A/C ALL
Subtask 55-40-00-865-061
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2, 14CC1, 14CC2, 15CC, 15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2, 19CE3, 22CE, 21CE1, 21CE2, 21CE3, 22CE, 21CE1, 21CE2, 21CE3
RUDDER MAIN STRUCTURE - DESCRIPTION AND OPERATION
_________________________________________________
1. General
_______
The rudder main structure has a front spar, two side shells and an upper and
a lower rib. The side shells are honeycomb constructions. The seven rudder
attach fittings and the three actuator attach fittings are also part of the
rudder main structure. All other components are attached to it.
2. Component Location
__________________
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
(Ref. Fig. 001)
R **ON A/C 106-149, 159-199, 211-299, 301-399, 401-499,
(Ref. Fig. 001A)
**ON A/C ALL
3. Description
___________
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
All components of the rudder main structure are made of laminations of Carbon Fiber Reinforced Plastic (CFRP). Hi-Lok fasteners connect them, but not the trailing edge. The side shells are installed to the front spar. In the area of the rudder attach fittings the side shells have cut-outs for clearance. Two rows of fasteners connect the side shells at the trailing edge. The inner row has threaded inserts and countersunk screws, the outer row has shear head rivets. Three hoisting points are bonded into each side shell.
Rudder Main Structure.
Figure 001
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 55-41-00Page 2 1201-210, 1May 01/05 1 1 1CES 1
Rudder Main Structure.
Figure 001A
R 1EFF : 106-149, 159-199, 211-299, 301-399, 1 55-41-00Page 3 1401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 159-199, 211-299, 301-399, 401-499,
All components of the rudder main structure are made of laminations of Carbon Fiber Reinforced Plastic (CFRP). Hi-Lok fasteners connect them, but not the trailing edge. The side shells are installed to the front spar. An access panel, installed in the left side shell, gives access to the No. 7 rudder attach fittings. The access panel is attached with countersunk screws. At the other locations, cutouts in the side shells give access to the adjacent attach fittings. Two rows of fasteners connect the side shells at the trailing edge. The inner row has threaded inserts and countersunk screws, the outer row has shear head rivets. Three hoisting points are bonded into each side shell. 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 STABILIZERS 安定面(110)
