• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 17:11来源:蓝天飞行翻译 作者:航空
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

 Subtask 76-11-00-820-059
 B. Hold the adjusting rod (5) then turn the nut (4) to get a load of 0.8 +0.1 -0 daN (1.8 +0.22 -0.0000 lbf) on the related throttle control lever.
 NOTE : Measure this value in the IDLE STOP/MAX CLIMB range. Do not
____ R measure this value at the detent points where the load increases R suddenly.
 (1) Tighten the lock nut (6) to block the adjustment system. Measure the load again to make sure that it is the same.
 Subtask 76-11-00-420-052
 C. Safety the lock nut (6) with lockwire 0.032 in. (0.8mm) dia..
 Subtask 76-11-00-020-053

 D. Cut and remove the lockwire from the lock nut (2). Loosen the lock nut. Subtask 76-11-00-820-060 R E. Turn the adjustment screw (1) to get a load equal to 2.5 +0.1 -0 daN
R (5.62 +0.22 -0 lbf) when you go through the MAX CLIMB detent point (the
R first detent point that you feel when you move the lever forward).
R NOTE : This detent point includes the load measured in paragraph B.

____
 (1) Block the adjustment system. Measure the load again to make sure that it is the same as the value given in the paragraph E.
 F 『 EEFF : ALL E Page 51376-11-00
 E E May 01/99 E E ECES E

 

 Adjustment of the Artificial Feel Unit
 Figure 504/TASK 76-11-00-991-913

 F 『 EEFF : ALL E Page 51476-11-00
 E E Feb 01/98 E E ECES E Subtask 76-11-00-420-053

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


 F. Safety the lock nut (2) with lockwire 0.032 in. (0.8mm) dia.
 (1) Install the guard (7). Tighten the three screws (3).
 5. Close-up
________ Subtask 76-11-00-410-056
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Close the access door 811.

 (3) Remove the access platform(s).


 (4) Remove the warning notice(s). Subtask 76-11-00-865-062
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1JH, 2JH1, 2JH2, 3JH1, 3JH2, 21CE1, 21CE2, 21CE3, 22CE
 Subtask 76-11-00-080-052
 C. Remove the tool from the throttle control levers.
 F 『 EEFF : ALL E Page 51576-11-00
 E E Feb 01/98 E E ECES E ARTIFICIAL FEEL UNIT - THROTTLE CONTROL - REMOVAL/INSTALLATION

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


______________________________________________________________
 TASK 76-11-17-000-042
 Removal of the Throttle Control Artificial Feel Unit
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps No specific circuit breaker(s) safety clip(s) No specific warning notice No specific access platform 1.8 m (5 ft. 11 in.) 98DNSA20206080 1 RIGGING PIN
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-82-12-000-001 Removal of the MCDU (3CA1,3CA2,3CA3) 23-13-13-000-001 Removal of the Radio Management Panel (CRMP) (1RG1, 1RG2, 1RG3) 23-51-12-000-001 Removal of the Audio Control Panel (ACP) (2RN1, 2RN2,
 2RN3, 2RN4, 2RN5) 34-41-12-000-001 Removal of the Weather Radar Control Unit (3SQ) 34-52-12-000-001 Removal of the ATC/TCAS Control Unit (3SH) 76-11-17-991-908 Fig. 401 76-11-17-991-909 Fig. 402 76-11-17-991-910 Fig. 403
 F 『 EEFF : ALL E Page 40176-11-17
 E E Feb 01/98 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E


 3. Job Set-up
__________
 Subtask 76-11-17-865-056
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU LIGHTING/EMER LT/CKPT/DOME 1LE H08
R  105VU FLT CTL/SEC1/STBY SPLY 22CE B01
R 121VU ENGINE/IGN/ENG2/SYS B 3JH2 P42 121VU ENGINE/IGN/ENG1/SYS B 3JH1 P41 121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 P40 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 P39 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
 
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 ENGINE CONTROLS 发动机控制(8)