B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
2 lock washer 32-31-03 22 -132
7 lock washer 32-31-03 22 -132
12 cotter pin 32-31-03 22 -120
17 cotter pins 32-31-03 22 -180
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
-------------------------------------------------------------------------------
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 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-12-13-000-001 Removal of the Secondary Hinged Fairing 32-12-13-400-001 Installation of a Replacement Secondary Hinged
Fairing
1EFF : ALL 1 32-31-00Page A518 1 1 May 01/05R 1 1 1CES 1
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-12-14-000-001 Removal of the MLG Fixed Fairing Assembly 32-12-14-400-001 Installation of the MLG Fixed Fairing Assembly (That was Removed For Access Only) 32-31-00-720-002 Functional Test of the Normal Extension and
Retraction of the Landing Gear 32-31-00-820-004 MLG Clearance Check 32-31-44-000-001 Removal of the MLG Uplock Assembly 2509GM (2510GM) 32-31-44-400-001 Installation of the MLG Uplock Assembly 2509GM
(2510GM) R 32-31-00-991-018 Fig. 510 R 32-31-00-991-017 Fig. 511
3. Job Set-up
__________
Subtask 32-31-00-820-061
A. MLG Clearance Check
(1) Make sure that a MLG Clearance Check has been done (Ref. TASK 32-31-00-820-004).
Subtask 32-31-00-941-085
B. Safety Precautions
(1) Make sure that the safety barriers are in position.
Subtask 32-31-00-860-095
C. Aircraft Maintenance Configuration
(1)
Make sure that the Green hydraulic system is pressurized (Ref. TASK 29-10-00-863-001).
(2)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
1EFF : ALL 1 32-31-00Page A519 1 1 May 01/05 1 1 1CES 1 Subtask 32-31-00-867-065
D. Extension of the Landing Gear WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
(1)
Make sure that the rigging pin is removed from the applicable MLG uplock.
(2)
On the panel 400VU:
(a)
Put the landing gear control lever to the DOWN position.
(b)
Make sure that the landing gear locked down lights are Green.
(3) Install the landing gear safety devices (Ref. TASK 32-00-00-481-001). Subtask 32-31-00-010-076
E. Get Access
(1)
Open the applicable MLG door for maintenance (Ref. TASK 32-12-00-010-001).
(2)
Put the adjustable access platform adjacent to the applicable MLG leg, zone 731(741).
4. Procedure
_________ R (Ref. Fig. 510/TASK 32-31-00-991-018, 511/TASK 32-31-00-991-017) Subtask 32-31-00-820-062
A. Prepare for Adjustment
(1)
Remove the applicable hinged fairing (Ref. TASK 32-12-13-000-001).
(2)
Remove the applicable fixed fairing (Ref. TASK 32-12-14-000-001).
(3)
Disconnect the free-fall linkage from the up-lock (Ref. TASK 32-31-44-000-001).
1EFF : ALL 1 32-31-00Page A520 1 1 May 01/05 1 1 1CES 1
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