• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 08:55来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (9) Install a new cotter pin (7). 
R  **ON A/C 051-051, 
R  Subtask 55-16-48-420-052 
R  C. Install Support Strut 
R  (1) Apply COMMON GREASE (Material No. 04-001) to all connection 
R  components. 
R  (2) Install the bushes (9), bolt (8) and nut (10). Do not tighten at this 
R  time (Ref. TASK 20-22-00-400-001). 
R  (3) Install the hinge bolt (14), the bush (15) and the washer (19). 
R  (4) Tighten the nuts (3) and safety with the tabwashers (4). 
R  (5) Use WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 to install the nut 
R  (16). Torque tighten the nut (16) to between 0.55 and 0.45 m.daN 
R  (48.67 and 39.82 lbf.in) 
R  (6) Use TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 to install the 
R  internal securing ring (17) (Ref. TASK 20-22-00-400-001). 
R  (7) Install a new cotter pin (12) 
R  (8) TORQUE the nut (10) to between 0.85 and 1.6 m.daN (75.22 and 141.59 
R  lbf.in). 
R  (9) Use TOOL - INSTALLATION, WASHERS SL40871 to install the internal 
R  securing ring (11) (Ref. TASK 20-22-00-400-001).

 

R (10) Install a new cotter pin (7) R **ON A/C ALL
 5. Close-up
________
 Subtask 55-16-48-410-051

 A. Visual Inspection
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 Subtask 55-16-48-410-050
 B. Close Access
 (1) Install/close the trailing edge panels 334FB, 334EB left-hand and/or 344FB, 344EB right-hand (Ref. TASK 55-13-11-400-001).
 Subtask 55-16-48-942-051
 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 55-16-48-081-050


 D. Remove Locking Devices
 (1) Remove the PIN-SIDE STICK LOCKING from the CAPT and F/O side stick controllers.

 (2)
 Remove the TBD from the elevator.
 Subtask 55-16-48-865-051

 

 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 19CE1, 19CE2, 19CE3, 15CE1, 16CE1, 15CE2, 16CE2, 1LY, 2LY


 ELEVATORS - DESCRIPTION AND OPERATION
_____________________________________
 1.
 General

_______ The elevators give pitch control to the aircraft. You can move the elevators to a maximum angle of 30 degrees upwards and 15 degrees downwards. Two servo control units at each elevator control the movement.

 2.
 Component Location


__________________
 -------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I I DOOR I REF.
 -------------------------------------------------------------------------------ELEVATOR STRUCTURE 335/345 55-21-00 ELEVATOR LEADING EDGE 335/345 55-22-00 ELEVATOR TIPS AND 335/345 55-24-00 INBOARD END CAPS ELEVATOR ATTACH FITTINGS 335/345 55-26-00 STATIC DISCHARGERS 335/345 23-60-00
 3. Description
___________ (Ref. Fig. 001) The left-hand and right-hand elevators are the same in design and function but are opposite hand. The structure of each elevator has a front spar, an upper and a lower skin panel and four ribs. All other components are attached to it. Six hinge fittings attach each elevator to the spar box of the trimmable horizontal stabilizer. Two fittings attach the servo control units. You can remove the leading edge access-panels, the tips and the inboard end caps. Each elevator has three hoisting points and four static dischargers.


 Elevators
 Figure 001
 1EFF :  ALL  1  55-20-00 Page 2 
1  1  Feb 01/98
 1  1
 1CES  1

 

 ELEVATORS - INSPECTION/CHECK
____________________________
 TASK 55-20-00-200-001 R Special Detailed Inspection of Elevator Top and Bottom Skin Panels in Area of R Hinge Supports 2, 3 and 4 and Actuator Fittings 1 and 2, LH/RH WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
 MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
 
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(54)