• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 00:00来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 Installation of the Vent Door
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  access platform 3.5 m (11 ft. 6 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 15-005  AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1 cotter pins 52-32-22 02A-010 17 cotter pin 52-32-21 07 -040
 1EFF : ALL 1 52-32-22Page 412 1 1 Aug 01/05R 1 1 1CES 1


 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
12-22-52-640-002 Lubrication of the FWD and AFT Cargo-Compartment Doors 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
 52-31-11-820-003 Adjustment of the Vent Door
 52-32-13-400-001 Installation of the Lining and Insulation

 **ON A/C 001-049, 053-099, 101-105, 201-220,
 52-32-22-991-001 Fig. 401
 **ON A/C 051-052,
 52-32-22-991-001-C Fig. 401A
 **ON A/C 106-149, 221-299, 301-399,
 52-32-22-991-001-B Fig. 401B
 **ON A/C 151-199,
 52-32-22-991-001-A Fig. 401C
R **ON A/C 401-499,
R 52-32-22-991-001-D Fig. 401D
R 1EFF : ALL 1 52-32-22Page 413 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL


 3. Job Set-up
__________ Subtask 52-32-22-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the AFT cargo-compartment door (referred to as cargo door) is opened and safetied with the actuator safety locks (Ref. TASK 52-30-00-860-001).

 (2)
 Make sure that the access platform in position below the opened cargo door.

 (3)
 Make sure that the lining and insulation are removed from the inner side of the cargo door.


 Subtask 52-32-22-865-051
 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
 4. Procedure
_________ **ON A/C 001-049, 053-099, 101-105, 201-220,
 (Ref. Fig. 401/TASK 52-32-22-991-001) **ON A/C 051-052,
 (Ref. Fig. 401A/TASK 52-32-22-991-001-C)
 1EFF : ALL 1 52-32-22Page 414 1 1 Aug 01/05R 1 1 1CES 1


 **ON A/C 106-149, 221-299, 301-399,
 (Ref. Fig. 401B/TASK 52-32-22-991-001-B)
 **ON A/C 151-199,

 (Ref. Fig. 401C/TASK 52-32-22-991-001-A) R **ON A/C 401-499,
R (Ref. Fig. 401D/TASK 52-32-22-991-001-D)
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,

 Subtask 52-32-22-420-050
 A. Installation of the Vent Door
 (1)
 Put the vent door (10) in position to the vent door frame.

 (2)
 Install the bolt (8), the washer (3) and the bush (9) to attach the vent door (10) to the upper hinge bracket.

 (3)
 Install the bolt (8) and the nut (2) to attach the vent door temporarily to the lower hinge bracket.

 (4)
 Adjust the upper and lower gaps between the vent door (10) and the vent door frame as follows:

 (a)
 Put the vent door (10) in the middle of the opening so that the gap is between 1.0 mm (0.0393 in.) and 3.0 mm (0.1181 in.).

 (b)
 Measure the clearance between the lower hinge bracket and the lower hinge arm to get the thickness of the shim set.

 (c)
 Remove the nut (2) and the bolt (8) from the lower hinge bracket.

 (d)
 Install the shim set of washers (4) with the correct thickness between the lower hinge brackets and the lower hinge arm.
 
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6(12)