R R Elevator Hinge Arm End Fittings Figure 401/TASK 55-16-42-991-001-A12 (SHEET 1)
1EFF : 1 1 1CES ALL 1 111 55-16-42 Page 404 Nov 01/98
R R Elevator Hinge Arm End Fittings Figure 401/TASK 55-16-42-991-001-A22 (SHEET 2)
1EFF : 1 1 1CES ALL 1 111 55-16-42 Page 405 Nov 01/98
R Subtask 55-16-42-020-055-A
R B. Remove the Hinge Arm End Fitting No 4.
R (1) Remove the elevator support strut (8) (Ref. TASK 55-16-48-000-001)
R and disconnect the hinge arm end fitting (9) from the attach end
R fitting (Ref. TASK 27-34-41-000-001).
R (2) Remove and discard the cotter pin (10).
R (3) Remove the nuts (11), the washers (12) and the bolts (13).
R (4) Remove the hinge arm fitting (9) from the hinge arm (14).
R NOTE : Record the position of the bolts (13) because some of them____
R attach a bonding strap and the bolts have different lenght.
TASK 55-16-42-400-001
R Installation 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 : 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
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific nonmetallic scraper
98D27903500000 4 PIN-SIDE STICK LOCKING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) Material No. 11-008 (USE 11-008A) (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R 2 cotter pins 55-16-41 01A-010 R 10 cotter pins 55-16-41 04A-010
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-34-41-400-001 Installation 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 55-13-11-000-001 Removal of the THS Trailing Edge Access Panels 55-13-11-400-001 Installation of the THS Trailing Edge Access Panels 55-16-48-400-001 Installation of the Elevator Support Struts 55-22-11-000-001 Removal of the Elevator Leading Edge Access Panels
335AB (345AB), 335BB (345BB), 335CB (345CB), 335DB (345DB). 55-16-42-991-001-A Fig. 401
3. Job Set-up
__________
Subtask 55-16-42-860-051
A. Aircraft Maintenance Configuration
(1)
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