R B. Consumable Materials

R  -------------------------------------------------------------------------------
R  REFERENCE DESIGNATION 
R  -------------------------------------------------------------------------------
R  Material No. 04-004 USA MIL-PRF-23827 TYPE I 
R  SYNTH.ESTER BASED GREASE HIGH PRESSURE 
R  (Ref. 20-31-00) 
R  C. Referenced Information 
R  -------------------------------------------------------------------------------
R  REFERENCE DESIGNATION 
R  -------------------------------------------------------------------------------
R  20-22-00-000-001 Removal of STA-LOK Nuts and Lockwashers 
R  55-16-00-991-005 Fig. 604 
R  3. Job Set-up__________ 
R  Subtask 55-16-00-941-059 
R  A. Aircraft Configuration 
R  (1) Put the PITCH TRIM CONTROL LOCKING (98D27403500000) in the cabin 
R  pedestal center. 
R  (2) Put the warning notices in the flight compartment to tell persons not 
R  to operate the flight controls. 
R  Subtask 55-16-00-010-056 
R  B. Access 
R  (1) Put the access platform in position at zone 314. 
R  (2) Open the access door 314AR.

R 4. Procedure
_________

R  (Ref. Fig. 604/TASK 55-16-00-991-005) 
R  Subtask 55-16-00-220-050 
R  A. Torque Value Inspection 
R  (1) Use TOOL - EXTRACTION, TAB WASHERS STA-LOK NSA5454 to remove the 
R  STA-LOK washer (1). 
R  (2) Use WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 to remove the 
R  STA-LOK nut (2). (Ref. TASK 20-22-00-000-001) 
R  (3) Apply COMMON GREASE (Material No. 04-004) to the thread of the bolt 
R  (3). 
R  (a) Use WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 to install the 
R  STA-LOK nut (2) on the bolt (3). 
R  (b) Torque the STA-LOK nut (2) to between 1.36 and 1.81 m.daN (10.02 
R  and 13.34 lbf.ft). 
R  (c) Use TOOL- INSTALLATION, TAB WASHERS STA-LOK NSA5454 to install 
R  the washer (31) on the nut (30). 
R  5. Close-up________ 
R  Subtask 55-16-00-410-059 
R  A. Close Access 
R  (1) Close the access panel 314AR. 
R  Subtask 55-16-00-942-055 
R  B. Remove Ground Equipment 
R  (1) Remove the warning notice(s). 
R  (2) Remove the PIN-SIDE STICK LOCKING (98D27903500000) from the CAPT and 
R  F/O side stick controllers. 
R  (3) Remove the access platform(s).

R Upper and Lower THS Support Attach Fittings R Figure 604/TASK 55-16-00-991-005
 1EFF : 051-051, 1 55-16-00Page 622 1 1 May 01/05 1 1 1CES 1

 ATTACH FITTINGS - THS ACTUATOR ARM - REMOVAL/INSTALLATION
_________________________________________________________
 TASK 55-16-34-000-001
 Removal of the THS Actuator Arms Attach Fittings
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
 MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
 DAMAGE.

 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
 CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.

 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 : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
 CARBONFIBER REINFORCED PLASTIC.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.0 m/(9ft. 10in)
 No specific circuit breaker(s) safety clip(s)
 No specific warning notices
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM STABILIZERS 安定面(39)