R 1EFF : 051-052, 1 52-31-21Page 412 1 1 May 01/05 1 1 1CES 1
R Handle Flap Mechanism
R Figure 402/TASK 52-31-21-991-002
R 1EFF : 051-052, 1 52-31-21 Page 413
1 1 May 01/05
1 1
1CES 1
R TASK 52-31-21-400-002 R Installation of the Handle Flap Mechanism R 1. Reason for the Job
__________________ R Self Explanatory R 2. Job Set-up Information
______________________ R A. Fixtures, Tools, Test and Support Equipment R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION R -------------------------------------------------------------------------------R No specific access platform 3.5 m (11 ft. 6 in.)
R B. Consumable Materials R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R No specific R R Material No. 09-013 R R R Material No. 15-005 R R R Material No. 15-006 R R lockwire, corrosion-resistant steel dia 0.8 mm
(0.032 in.) USA MIL-PRF-81733 TYPE I CLASS A CORROSION INHIBITING BRUSH CONSISTENCY (Ref. 20-31-00) AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00) AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
R 1EFF : 051-052, 1 52-31-21Page 414 1 1 May 01/05 1 1 1CES 1R C. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 12-22-52-640-002 R R 52-30-00-860-001 R R 52-30-00-860-002 R R 52-31-11-820-002
R 3. Job Set-up
__________
R Subtask 52-31-21-860-056 Lubrication of the FWD and AFT Cargo-Compartment Doors Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump Adjustment of the Door Mechanism
R A. Aircraft Maintenance Configuration
R (1) Make sure that the FWD cargo-compartment door (referred to as cargo R door)is opened and safetied with the actuator safety locks (Ref. TASK R 52-30-00-860-001).
R (2) Make sure that the access platform in position below the opened cargo R door.
R (3) Make sure that the access panel 825AR is removed.
R Subtask 52-31-21-865-054
R B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and R tagged
R -------------------------------------------------------------------------------R PANEL DESIGNATION IDENT. LOCATION R -------------------------------------------------------------------------------R 121VU HYDRAULIC/HYD POWER/Y 3803GX N30 R 122VU DOORS/CARGO 1MJ T12 R 123VU Y HYD/ELEC/PUMP 3802GX AB06 R 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
R 1EFF : 051-052, 1 52-31-21Page 415 1 1 May 01/05 1 1 1CES 1
R 4. Procedure_________
R Subtask 52-31-21-560-051
R A. Preparation of the Replacement Components
R (1) Install the handle flap mechanism (9) temporarily and adjust the
R handle flap linkage (1) correctly (Ref. TASK 52-31-11-820-002).
R (2) Remove the handle flap mechanism (9) to safety the handle flap
R linkage (1).
R (3) Safety the lock nuts (2),(4) and the adjustment screw (3) with
R lockwire, corrosion-resistant steel dia 0.8 mm (0.032 in.).
R Subtask 52-31-21-420-051
R B. Final Installation of the Handle Flap Mechanism
R (1) Clean the component interface and/or the adjacent area.
R (2) Do an inspection of the component interface and/or the adjacent area.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM DOORS 舱门4(89)
