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时间:2011-03-27 08:55来源:蓝天飞行翻译 作者:admin
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 E. Remove Locking Devices
 (1) Remove the PIN-SIDE STICK LOCKING (98D27903500000) from the CAPT and F/O side stick controllers.
 Subtask 55-16-38-865-051
 F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 19CE1, 19CE2, 19CE3, 15CE1, 16CE1


 HINGE ARM FITTINGS - ELEVATOR - REMOVAL/INSTALLATION
____________________________________________________ TASK 55-16-42-000-001 R Removal of the Elevator Hinge Arm End 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. WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
 FALL CAN INJURE OR KILL YOU.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

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

 1.
 Reason for the Job

__________________
 To inspect or to replace the hinge arm fittings


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific warning notices
 No specific access platform 3.5 m (11 ft. 6 in.)
 98D27903500000 2 PIN-SIDE STICK LOCKING

 

 B. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-34-41-000-001 Removal of the Elevator
 29-10-00-864-001 Depressurize the Green Hydraulic System
 29-10-00-864-002 Depressurize the Yellow Hydraulic System
 29-10-00-864-003 Depressurize the Blue Hydraulic System
 55-16-48-000-001 Removal of the Elevator Support Struts
 55-16-42-991-001-A Fig. 401

 3. Job Set-up
__________
 Subtask 55-16-42-860-050
 A. Depressurize Hydraulic Systems
 (1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-10-00-864-00100) (Ref. TASK 29-10-00-864-00200) (Ref. TASK 29-10-00-864-00300) (Ref. TASK 29-10-00-864-001) (Ref. TASK 29-10-00-864-002) (Ref. TASK 29-10-00-864-003).
 Subtask 55-16-42-865-051
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09

R 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
R 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
R 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 55-16-42-481-050
 C. Install Locking Devices
 (1) Put the PIN-SIDE STICK LOCKING (98D27903500000) in the CAPT and F/O side stick controllers.


 Subtask 55-16-42-941-050

 D. Safety Precautions
 (1) Put the warning notices in the flight compartment to tell persons not to operate the flight controls.
 (2) Put the warning notices in position to tell persons not to operate the hydraulic systems.
 (3) Put the access platform in position at zone 334 for the left hand elevator hinge arm fittings and/or zone 344 for the right hand elevator hinge arm fittings.
 Subtask 55-16-42-010-050
 E. Access
 (1) Remove the horizontal stabilizer trailing edge panels as necessary (Ref. 55-13-11-000-00100).
 (2) Remove the elevator leading edge panels as necessary (Ref. 55-22-11-000-001 00). 
R  4. Procedure_________ 
R  (Ref. Fig. 401/TASK 55-16-42-991-001-A) 
R  Subtask 55-16-42-020-051 
 
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