(2)
Remove the leading edge intersection (1).
(a)
Remove the screws (4) from the leading edge intersection (1).
(b)
Remove the leading edge intersection (1).
R R Trimmable Horizontal Stabilizer Leading-Edge Figure 401/TASK 55-12-11-991-001
1EFF : 1 1 1CES ALL 1 111 55-12-11 Page 404 May 01/99
R Trimmable Horizontal Stabilizer Leading Edge Left Hand R Figure 402/TASK 55-12-11-991-006
1EFF : ALL 1 55-12-11Page 405 1 1 May 01/99 1 1 1CES 1
TASK 55-12-11-400-001
Installation of the Horizontal Stabilizer Leading Edge
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 : DO NOT GET THE COMPOUND ON YOUR SKIN._______ IF YOU DO: - RUB IT OFF IMMEDIATELY WITH A CLEAN CLOTH - WASH THE SKIN WITH SOAP AND RINSE WITH CLEAN WATER.
R R R R R WARNING : YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO WORK IN OR NEAR A_______ FUEL TANK. IF YOU DO NOT OBEY THE SAFETY PROCEDURES, THERE IS A RISK OF: - DEATH OR INJURY TO PERSONS - DAMAGE TO THE AIRCRAFT OR OTHER EQUIPMENT.
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 98D27903500000 nonmetallic scraper4 PIN-SIDE STICK LOCKING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-013 D TV-53-3507/73 RELEASE AGENT (OBSOLETE USE 05-013A) (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 11-008 (USE 11-008A) (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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
55-12-11-991-001 Fig. 401
55-12-11-991-006 Fig. 402
3. Job Set-up
__________
Subtask 55-12-11-860-054
A. Aircraft Maintenance Configuration
(1)
Make sure that the hydraulic systems are depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-864-003).
(2)
Make sure that thePIN-SIDE STICK LOCKING is in the CAPT and F/O side sick controllers.
(3)
Make sure that the warning notices are in the flight compartment to tell persons not to operate the flight controls.
(4)
Make sure that the warning notices are in position to tell persons not to operate the hydraulic systems.
(5)
Make sure that the access platforms are in position at zone 330 and/or 340.
Subtask 55-12-11-865-060
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
4. Procedure
_________
R (Ref. Fig. 401/TASK 55-12-11-991-001, 402/TASK 55-12-11-991-006) NOTE : Only the installation of the LH leading edge is shown. The
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