(5)
 Install the torque shaft (1) (Ref. TASK 27-54-45-400-009).

 (6)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the remaining washers (3) and the bolts (4).

 Subtask 27-54-48-080-050
 C. Preparation for Test
 (1)
 Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from the outboard flap drive-shaft (Ref. TASK 27-50-00-000-003).

 (2)
 Make sure that the work area is clean and clear of tool(s) and other items.

 Subtask 27-54-48-865-053
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 10CV, 12CV.
 1EFF : ALL 1 27-54-48Page 410 1 1 Aug 01/02R 1 1 1CES 1

 Subtask 27-54-48-710-050
 E. Operational Test of the Flap System
 (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
 (2) Do an operational test of the flap system (Ref. TASK 27-54-00-710-001).
 5. Close-up________
 (Ref. Fig. 401/TASK 27-54-48-991-001)
 Subtask 27-54-48-410-050
 A. Close Access 
R R R R R R (1) Install the applicable access panels: FOR 6217CM install 573CB (Ref. TASK 57-51-37-400-002) install 575AB (Ref. TASK 57-51-37-400-004). FOR 6267CM install 573CB (Ref. TASK 57-51-37-400-002) install 575AB (Ref. TASK 57-51-37-400-004). 
Subtask 27-54-48-860-051
 B. Aircraft Maintenance Configuration
 (1) Make sure the flaps are fully retracted (Ref. TASK 27-50-00-866-009).
 (2) Remove the COLLAR-SAFETY, SPOILER from the piston rod of the servo-control.
 (3) Put the applicable spoiler to the 'O' (Operation) position (Ref. TASK 27-60-00-866-002).
 (4) On the servo-control, make sure that the pointer on the hex. head is opposite the letter 'O' (Operation) on the housing.

 Subtask 27-54-48-942-051
 C. Removal of Equipment
 (1)
 Remove the warning notice(s).

 (2)
 Remove the access platform(s).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 ACTUATOR ASSY (6205CM,6211CM,6221CM,6233CM,6255CM,6261CM,6271CM,6283CM)_______________________________________________________________________ REMOVAL/INSTALLATION____________________
 TASK 27-54-49-000-008
 Removal of the Flap Track 1 to 4 Actuators 6205CM(6255CM)/6211CM(6261CM)/ 6221CM(6271CM)/6233CM(6283CM)
 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.
 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:_______ - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1. Reason for the Job__________________ 
R R  Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R  No specific No specific No specific No specific No specific No specific  circuit breaker(s) safety clip(s) clampssafety barrierswarning noticewarning notice(s) access platforms 2.8 m (9 ft. 2 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 24-41-00-862-002 27-50-00-866-008
27-51-18-000-001 27-54-49-000-001 27-54-49-000-002 27-54-49-000-003 27-54-49-000-004
27-60-00-866-002 31-32-00-860-006 32-00-00-481-001 32-12-00-010-001
27-54-49-400-001 27-54-49-400-002 27-54-49-400-003 27-54-49-400-004
3. Job Set-up
__________ Subtask 27-54-49-941-076
 A. Safety Precautions
Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerExtension of the Flaps on the GroundRemoval of the Asymmetry-Position Pick-Off Unit 29CV (30CV)Removal of the Flap Track 1 Actuator 6205CM(6255CM)Removal of the Flap Track 2 Actuator 6211CM(6261CM)Removal of the Flap Track 3 Actuator 6221CM(6271CM)Removal of the Flap Track 4 Actuator 6233CM(6283CM)Extension-Retraction of the Spoilers for MaintenanceProcedure to Get Access to the SYSTEM REPORT/TEST F/CTL PageInstallation of the Safety Devices on the Landing GearsOpen the Main Gear Doors for AccessInstallation of the Flap Track 1 Actuator 6205CM(6255CM) (for corrective action)Installation of the Flap Track 2 Actuator 6211CM(6261CM) (for corrective action)Installation of the Flap Track 3 Actuator 6221CM(6271CM) (for corrective action)Installation of the Flap Track 4 Actuator 6233CM(6283CM) (for corrective action)
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FLIGHT CONTROLS 飛行操縱5(96)