(16)
 On the F/CTL page of the lower ECAM display unit:

 -make sure that the PITCH TRIM indicator shows 0. plus or minus 0.3..

 (17)
 On the tail cone, make sure that the THS is opposite the 0 mark.

 5. Close-up
________ Subtask 27-41-00-860-063
 A. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).

 (2)
 On the panel 23VU, push the FLT CTL/SEC 1 and FLT CTL/ELAC 1 pushbutton switches (on these pushbutton switches, the OFF legends go off).

 (3)
 On the panel 24VU, push the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend goes off).

 (4)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (5)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (6)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 Subtask 27-41-00-410-055
 B. Close Access
 (1)
 Install the protective cover on the battery power center 105VU.

 (2)
 Tighten the two screws.

 (3)
 Close the access door 822.

 1EFF : ALL 1 27-41-00Page 630 1 1 May 01/05R 1 1 1CES 1

 (4)
 Close the access door 312AR.

 (5)
 Remove the access platform(s).

 1EFF : ALL 1 27-41-00Page 631 1 1 May 01/05R 1 1 1CES 1

 TASK 27-41-00-210-003
 Visual Inspection and Lubrication of the Rear THS control cable (between FR71 and the THS actuator) 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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth
 No specific access platform 2.8 m (9 ft. 2 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
 1EFF : ALL 1 27-41-00Page 632 1 1 May 01/05R 1 1 1CES 1

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-24-11-100-001 Cleaning and Protection of the Cables 20-24-12-200-001 Check of the Control Cables 27-41-00-991-010 Fig. 601
 3. Job Set-up
__________ Subtask 27-41-00-010-062
 A. Get Access
 (1)
 Put the access platform in position at the zone 312.

 (2)
 Open the access door 312AR.

 4. Procedure
_________
 (Ref. Fig. 601/TASK 27-41-00-991-010) Subtask 27-41-00-020-053
 A. Removal of the Protective Covers
 (1)
 Remove the screws (4) and the washers (3).

 (2)
 Release the fasteners (1) and remove the protective covers (2) and (5).

 Subtask 27-41-00-210-057
 B. Visual Inspection of the Rear THS Control Cable
 (1)
 Do an inspection the THS control cable between the tension regulator and the chain linkage.

 (2)
 Make sure that the chain and the cable move freely.

 (3)
 Make sure that the chain and the cable do not touch the structure (no marks on the fasteners).

 (4)
 Make sure that the chain that controls the THS actuator is in the correct condition.

 (5)
 Make sure that the cables are not damaged (Ref. TASK 20-24-12-200-001).

 (6)
 Make sure that there is no corrosion on the cables (Ref. TASK 20-24-11-100-001).

 (7)
 Clean the control cable in this area with a lint-free cloth.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱3(102)