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
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