• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 14:18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

 (f) TORQUE the union nut of the case drain line (8) to between 1.5 and 1.7 m.daN (11.06 and 12.53 lbf.ft).
 (g) Connect the hydraulic lines (11) to the valve block assembly (23).
 (h) TORQUE the union nuts of the hydraulic lines (11) to between 5.4 and 5.9 m.daN (39.82 and 43.51 lbf.ft).
 (i) Connect the seal drain line (10) to the POB (41). 
R  (16) Connect the electrical connector (22).
 (a) Remove the caps from the electrical connectors (22).
 (b) Connect the electrical connector (22) to the valve block assembly (23).
 Subtask 27-54-54-860-051
 C. Preparation for the Test
 (1) Remove the PIN RIGGING-FLAPS from the left and right flap track positions 1.
 (2) Pressurize the reservoirs of the Green and Yellow hydraulic systems (Ref. TASK 29-14-00-614-002).

 

 Subtask 27-54-54-865-052
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV
 Subtask 27-54-54-710-050
 E. Test
 (1)
 Do the operational test of the flap system (Ref. TASK 27-54-00-710-001).

 (2)
 Make sure that there are no leaks and that no fluid comes out of the seal drain line (10).


 5. Close-up
________ Subtask 27-54-54-860-052
 A. Put the aircraft back to the serviceable condition.
 (1)
 Make sure that the level of fluid in the relevant hydraulic reservoir is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).

 (2)
 Remove the container from below the PCU (1).


 (3) Remove the access platform(s). Subtask 27-54-54-410-050
 B. Close the main doors of the main gear (Ref. TASK 32-12-00-410-001).


R  TASK 27-54-54-000-002 
R  Removal of the Hydraulic Motor of the Flap Power Control-Unit (6201CM) without 
R  the Pressure-Off Brake and the Valve Block Assembly 
R  WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ 
R  GEAR. 
R  WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE_______ 
R  CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. 
R  WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU_______ 
R  START A TASK ON OR NEAR: 
R  - THE FLIGHT CONTROLS 
R  - THE FLIGHT CONTROL SURFACES 
R  - THE LANDING GEAR AND THE RELATED DOORS 
R  - COMPONENTS THAT MOVE. 
R  1. Reason for the Job__________________ 
R  Self Explanatory 
R  2. Job Set-up Information______________________ 
R  A. Fixtures, Tools, Test and Support Equipment 
R  -------------------------------------------------------------------------------
R  REFERENCE  QTY DESIGNATION 
R  -------------------------------------------------------------------------------

R  No specific  circuit breaker(s) safety clip(s) 
R  No specific  1 ACCESS PLATFORM 3M (10 FT) 
R  No specific  1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 
R  No specific  1 CAP - BLANKING 
R  No specific  1 CONTAINER 5 L(1 1/2 USGAL) 
R  No specific  1 WARNING NOTICE 
R  98D27504005000  2 PIN RIGGING-FLAPS (TRACK 1) 
R  98D27504006000  2 PIN RIGGING FLAPS 
R  98D27803000000  1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER

 

R B. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 27-00-00-480-002 R R 27-50-00-866-009 R 29-10-00-864-001 R 29-10-00-864-002 R 29-14-00-614-001 R 32-12-00-010-001 R 27-54-54-991-002
R 3. Job Set-up
__________
R Subtask 27-54-54-866-051 Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000) Retraction of the Flaps on the Ground Depressurize the Green Hydraulic System Depressurize the Yellow Hydraulic System Depressurization of the Hydraulic Reservoirs Open the Main Gear Doors for Access Fig. 402
R A. Retraction of the Flaps

R (1) Retract the flaps to the 0 degree position (Ref. TASK 27-50-00-866-R 009).
R (2) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000)

R (Ref. TASK 27-00-00-480-002) on the slat/flap control lever.
R Subtask 27-54-54-865-053
R B. Open, safety and tag this(these) circuit breaker(s):
R -------------------------------------------------------------------------------
 
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 FLIGHT CONTROLS 飞行操纵5(159)