B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Material No. 02-003 lockwire, corrosion-resistant steel dia 0.8 mm (0.032 in.)F NSA 307110 TYPE 4
Material No. 05-002 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)USA MIL-P-8116
Material No. 05-005 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)USA MIL-C-16173 GRADE II
CORROSION PREVENTIVE (Ref. 20-31-00)
1EFF : ALL 1 27-44-51Page 418 1 1 May 01/05R 1 1 1CES 1
R R R R
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
37 cotter pins 27-41-04 04 -340 61 cotter pins 27-44-04 01 -270 61 cotter pins 27-44-04 01B-270 65 cotter pins 27-44-04 01 -310 65 cotter pins 27-44-04 01B-310 71 retainer washers 27-44-04 01 -360 71 retainer washers 27-44-04 01B-360 73 retainer washers 27-44-04 01 -340 73 retainer washers 27-44-04 01B-340
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)-
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-41-00-730-001 System Test of the THS Actuator Electrical Control 27-41-00-820-001 Adjustment of the THS Zero Position 27-44-51-210-004 Check the Oil Level of the Gearbox of the
THS-Actuator 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 29-00-00-910-002 Safety Procedures of the Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 27-44-51-991-001 Fig. 401 27-44-51-991-002 Fig. 402 27-44-51-991-003 Fig. 403 27-44-51-991-014 Fig. 404 27-44-51-991-004 Fig. 405 27-44-51-991-005 Fig. 406
3. Job Set-up__________
(Ref. Fig. 401/TASK 27-44-51-991-001, 402/TASK 27-44-51-991-002, 403/TASK 27-44-51-991-003)
Subtask 27-44-51-860-055
A. Aircraft Maintenance Configuration
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
(1)
Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
(2)
Make sure that the access platform is in position below the access door 312AR.
(3)
Make sure that the access door 312AR is open.
(4)
Make sure that the pitch-trim control wheel in the flight compartment is in the zero position.
(5)
Make sure that the PITCH TRIM CONTROL LOCKING (98D27403500000) is installed on the pitch-trim control wheel.
(6)
Make sure that the warning notices are in position in the cockpit to tell persons not to operate the pitch controls.
(7)
Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(8)
Make sure that the reservoirs of the Green and Yellow hydraulic systems are depressurized. (Ref. TASK 29-14-00-614-001).
(9)
Make sure that the warning notices are in position to tell persons not to pressurize the Green, the Yellow and the Blue hydraulic systems:
-in the cockpit on the hydraulic section 40VU of the overhead panel,
- on the ground service panels of the Green, the Yellow and the Blue hydraulic systems.
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