32-11-13 02E-16032-11-13 02G-110 32-11-13 01A-06032-11-13 01E-06032-11-13 01F-06032-11-13 01G-060 32-11-13 01A-05032-11-13 01E-05032-11-13 01F-05032-11-13 01G-050 32-11-13 01A-01532-11-13 01E-01532-11-13 01F-01532-11-13 01G-015 32-11-11 60A-06032-11-11 60E-05032-11-11 60F-05032-11-11 60G-060 32-11-11 60A-04032-11-11 60E-04032-11-11 60F-04032-11-11 60G-04032-11-13 01E-15032-11-13 01F-15032-11-13 01E-14032-11-13 01F-140 32-11-11 60A-07032-11-11 60G-07032-11-11 65C-01032-11-11 65D-01032-11-11 60E-05032-11-11 60F-05032-11-11 65C-14032-11-11 65D-14032-11-11 65C-15032-11-11 65D-15032-11-13 01E-15032-11-13 01F-15032-11-13 01E-14032-11-13 01F-14032-11-11 65C-01032-11-11 65D-01032-11-11 65C-150
 1EFF : ALL 1 32-11-13Page 424 1 1 May 01/05 1 1 1CES 1
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FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
61  backing ring  32-11-11 65D-150 
 62  O-ring  32-11-11 65C-140 
 62  O-ring  32-11-11 65D-140 
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-586-002  Lowering of the Aircraft for Maintenance Operations 
 12-12-32-611-008  Hydraulic Replenishment of the MLG Two-Stage Shock 
 Absorber 
 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)- 
24-41-00-861-002  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 
 29-10-00-863-002  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 
 32-00-00-481-001  Installation of the Safety Devices on the Landing 
 Gears 
 32-00-00-860-001  Flight Configuration Precautions with Electrical 
 Power 
 32-00-00-860-002  Ground Configuration after Flight Configuration with 
 Electrical Power 
 32-11-13-400-003  Installation of the MLG Shock-Absorber Gland-Seals 
 32-11-43-400-003  Installation of the 1M and 2M Harnesses on the MLG 
 Axle 
 32-12-00-010-001  Open the Main Gear Doors for Access 
 32-31-00-720-002  Functional Test of the Normal Extension and 
 Retraction of the Landing Gear 
 32-41-11-400-006  Installation of the MLG Wheel 
 (2649GM,2650GM,2651GM,2652GM) 
 32-42-27-400-001  Installation of the Brake 
 (2641GM,2642GM,2643GM,2644GM)
1EFF : ALL 1 32-11-13Page 425 1 1 May 01/05R 1 1 1CES 1
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REFERENCE DESIGNATION
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