B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific mystic tape Material No. 11-026 GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (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 -------------------------------------------------------------------------------
1 cotter pin 32-11-12 17 -010 15 cotter pin 32-11-12 17 -010 41 cotter pin 32-11-12 03D-065 41 cotter pin 32-11-12 03F-065
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 29-00-00-910-002 Safety Procedures of the Hydraulic System 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 29-10-00-864-002 Depressurize the Yellow Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
 Transfer Unit (PTU) 29-23-00-860-002 Connection of the Isolation Coupling of the Power
 Transfer Unit (PTU)
 1EFF : ALL 1 32-11-12Page 425 1 1 May 01/05R 1 1 1CES 1

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-00-00-860-002 Ground Configuration after Flight Configuration with
 Electrical Power 32-11-11-400-001 Installation of the MLG Leg Assembly 32-42-00-710-001 Operational Check of the Normal Braking System 32-42-00-870-001 Bleeding of the Normal Braking at the Brake Units 32-42-27-400-001 Installation of the Brake
 (2641GM,2642GM,2643GM,2644GM) 32-43-00-710-001 Operational Check of Alternate Braking System 32-43-00-870-002 Bleeding of the High Pressure Alternate Braking
 System 32-45-00-710-001 Operational Check of the Parking Brake System Using Individual Motors in Turn 32-46-00-740-001 BITE Test of the BSCU
 **ON A/C 001-003, 051-052,
 32-11-12-991-001 Fig. 401

R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-11-12-991-001-A Fig. 401A
 **ON A/C 001-003, 051-052,
 32-11-12-991-002 Fig. 402
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-11-12-991-002-A Fig. 402A
 **ON A/C 001-003, 051-052,
 32-11-12-991-003 Fig. 403
 1EFF : ALL 1 32-11-12Page 426 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 32-11-12Page 427 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-11-12-991-003-A Fig. 403A **ON A/C 001-003, 051-052,
R  32-11-12-991-004 Fig. 404 **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-11-12-991-004-A Fig. 404A **ON A/C 001-003, 051-052,
R  32-11-12-991-005 Fig. 405 **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-11-12-991-005-A Fig. 405A **ON A/C 001-003, 051-052,
R  32-11-12-991-010 Fig. 406 **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-11-12-991-010-A  Fig. 406A

 3. Job Set-up
__________ Subtask 32-11-12-941-052
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).

 (3)
 Make sure that you obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).

 (4)
 On panel 400VU:

 -
make sure that the landing-gear control-lever 6GA is in the DOWN position
　
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