-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
No specific adjustable access platform 8.0 m (26 ft. 3 in.)
No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
98D27207545000 3 PIN - RIGGING
98D27207546000 1 PIN - RIGGING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-005 Material No. 07-001
Material No. 08-029 Material No. 08-061A Material No. 09-005 Material No. 09-018
Material No. 11-004
Material No. 16-003 R Material No. 16-021 R Material No. 19-010
Material No. 19-018
C. Expendable Parts
USA MIL-C-16173 GRADE II
CORROSION PREVENTIVE (Ref. 20-31-00)
ELECTRICAL BONDING COATING (BLUE COLOR)
(Ref. 20-31-00)
USA MIL-R-46082 TYPE I
ADHESIVE (Ref. 20-31-00)
D DAN 220
ALUMINIUM FOIL ADHESIVE TAPE (Ref. 20-31-00)
USA MIL-S-81733 CLASS C
CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
F ASNB70720
COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
F ASNB70720
FLEXIBLE POLYURETHANE (Ref. 20-31-00)
USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
USA AMS 5687
LOCKWIRE 0.6 MM (Ref. 20-31-00)
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R 13 cotter pins
R 13 cotter pins
R 22 tabwashers
27 cotter pins
27-21-47 01 -210 27-21-47 01A-210 27-23-04 01A-08027-23-04 01 -050
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
22-61-00-710-001 Operational Test of the Rudder Travel Limiting Function 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
**ON A/C 001-003, 051-054,
27-23-51-991-001 Fig. 401
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
27-23-51-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 27-23-51-860-054
A. Aircraft Maintenance Configuration
(1)
Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(2)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
(3)
Make sure that the warning notices are in position.
(4)
Make sure that the rudder pedals are in the neutral position.
(5)
Make sure that the RUD TRIM indicator on the panel 110VU of the center pedestal shows zero.
(6)
Make sure that the FLT CTL/FAC 1 pushbutton switch on the overhead panel 23VU is released.
(7)
Make sure that the FLT CTL/FAC 2 pushbutton switch on the overhead panel 24VU is released.
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