R Material No. 08-004 USA MIL-A-25457
R ADHESIVE SEALANT (Ref. 20-31-00)
R Material No. 08-026
R ADHESIVE/SEALANT ONE PART,RTV SILICONE RUBBER
R (Ref. 20-31-00)
R Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A
R CORROSION INHIBITING BRUSH CONSISTENCY
R (Ref. 20-31-00)
R Material No. 11-003A
R X (Ref. 20-31-00)
1EFF : ALL 1 52-32-18Page 409 1 1 May 01/05 1 1 1CES 1
C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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17 cotter pin 52-36-04 08C-080 17 cotter pin 52-36-04 08D-080
D. Referenced Information
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REFERENCE DESIGNATION
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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)-
29-00-00-910-002 Safety Procedures of the Hydraulic System 29-10-00-863-002 Pressurize the Yellow 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 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump
52-31-11-820-004 Adjustment of the Door Opening Angle
52-32-11-100-001 Cleaning/Painting of AFT Cargo-Compartment Door
52-32-24-400-001 Installation of the Wiring Harness 4613VB
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
52-32-18-991-001-A Fig. 401
**ON A/C 051-052,
52-32-18-991-001-B Fig. 401A
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
52-32-18-991-002-A Fig. 402
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REFERENCE DESIGNATION
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R **ON A/C 051-052,
R 52-32-18-991-002 Fig. 402A
R **ON A/C ALL
3. Job Set-up
__________
Subtask 52-32-18-860-051
A. Aircraft Maintenance Configuration
(1)
Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
(2)
Make sure that the hydraulic reservoirs are depressurized (Ref. TASK 29-14-00-614-001).
(3)
Make sure that the Yellow hydraulic system is depressurized (Ref. TASK 29-10-00-864-002).
(4)
Make sure that the cargo door is opened (Ref. TASK 52-30-00-860-001) and safetied with the SUPPORT STRUT - CARGO DOORS (98D52307524000).
(5)
Make sure that the access platform in position below the opened cargo door.
Subtask 52-32-18-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU DOORS/CARGO 1MJ T12 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
1EFF : ALL 1 52-32-18Page 411 1 1 May 01/05 1 1 1CES 1
4. Procedure
_________ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401/TASK 52-32-18-991-001-A)
**ON A/C 051-052,
(Ref. Fig. 401A/TASK 52-32-18-991-001-B) R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 402/TASK 52-32-18-991-002-A)
**ON A/C 051-052,
(Ref. Fig. 402A/TASK 52-32-18-991-002)
Subtask 52-32-18-560-050
A. Preparation of Replacement Component WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門5(69)
