B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 04-001 F AIR-4205
WHEEL BEARING MINERAL GREASE (Ref. 20-31-00)
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-009 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA
(Ref. 20-31-00)
C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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4 cotter pins 27-41-04 04 -260 14 cotter pin 27-41-04 04 -300 21 cotter pins 27-41-04 04 -150 27 cotter pins 27-41-04 04 -340 34 cotter pin 27-41-04 04 -300
D. Referenced Information
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REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-24-11-100-001 Cleaning and Protection of the Cables
20-24-12-200-001 Check of the Control Cables
27-00-00-080-001 Removal of the Pitch-Trim Control Locking Tool
(98D27403500000) 27-41-00-220-002 Check of the Correct Tension of the THS Mechanical Control Cables 27-41-00-720-001 Functional Test of the THS-Actuator Overtravel Related to the Mechanical Indicator 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
R 53-22-12-000-001 Removal of the Cabin Floor Panels
R 53-22-12-400-001 Installation of the Cabin Floor Panels -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
53-32-12-000-002 Removal of the Cabin Floor Panels
53-32-12-400-002 Installation of the Cabin Floor Panels
27-41-45-991-001 Fig. 401
27-41-45-991-002 Fig. 402
27-41-45-991-003 Fig. 403
3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-41-45-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position.
(2)
Make sure that the access panel 311AL is removed and the access door 312AR is opened.
(3)
Make sure that the floor panels 241FF, 241BF (Ref. TASK 53-32-12-000-002) are removed.
(4)
Make sure that the locking clips are removed and the turnbuckles of the THS cables are released.
NOTE : Make sure that there is no tension on the THS control cables.
____
(5)
Make sure that the Green and the Yellow hydraulic systems are depressurized and in the maintenance configuration (Ref. TASK 29-00-00-864-001).
(6)
Make sure that the warning notices are in position to tell persons not to pressurize the Green and the Yellow hydraulic systems.
(7)
Make sure that the PITCH TRIM CONTROL LOCKING (98D27403500000) is installed in the pitch trim control wheel.
(8)
Make sure that the PIN - RIGGING (0U190360) is installed in the mechanical input of the THS actuator.
(9) Make sure that the RIGGING PIN - THS MECHANICAL CONTROL
(98D27407532000) is installed in the rocker assembly of the
regulator.
(Ref. Fig. 401/TASK 27-41-45-991-001)
R **ON A/C 301-399,
R Subtask 27-41-45-860-052-A
R A. Aircraft Maintenance Configuration
R (1) Make sure that the access platform is in position.
R (2) Make sure that the access panel 311AL is removed and the access door
R 312AR is opened.
R (3) Make sure that the floor panels 231BG, 231JG (Ref. TASK 53-22-12-000-
R 001) are removed.
R (4) Make sure that the locking clips are removed and the turnbuckles of
R the THS cables are released.
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