A320飞机维护手册 AMM DOORS 舱门8(105)

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

Subtask 52-81-00-220-070
 AE. Dimensional Check of the Door Actuator Fitting
 -------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | G | 15.841 | 15.859 | | | 15.822 | | | | OD 24 |(0.6236) |(0.6243) | | |(0.6229) | | | | | | | 0.003 | 0.034 | | | 0.072 | | | | | (0.0001)| (0.0013)| | |(0.0028)| | G | 15.862 | 15.875 | | | | 15.894 | | | ID 19 |(0.6244) |(0.6250) | | | |(0.6257) | | -------------------------------------------------------------------------------
Subtask 52-81-00-220-071
 AF. Dimensional Check of the Door Actuator Fitting
 1EFF : ALL 1 52-81-00Page 620 1 1 Feb 01/98 1 1 1CES 1 -------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | G | 30.150 | 30.163 | | | 30.139 | | | | OD 19 |(1.1870) |(1.1875) | | |(1.1865) | | | | | | | -0.003 | 0.025 | | | 0.047 | | | | |-(0.0001)| (0.0009)| | |(0.0018)| | G | 30.160 | 30.175 | | | | 30.186 | | | ID 22 |(1.1874) |(1.1879) | | | |(1.1884) | | -------------------------------------------------------------------------------

5. Close-up
________
 Subtask 52-81-00-410-052
 A. Close Access
 (1) Install the MLG door (Ref. TASK 32-12-11-400-001).
 Subtask 52-81-00-865-052
 B. TO BE DELETED
 Subtask 52-81-00-869-051
 C. TO BE DELETED
 Subtask 52-81-00-942-051
 D. Remove the Equipment
 (1)
 Remove the access platform(s).

 (2)
 Remove the warning notice(s).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 52-81-00Page 621 1 1 Feb 01/98 1 1 1CES 1

 DOOR - MAIN LANDING GEAR, COMMON RAMP - REPAIRS
_______________________________________________ TASK 52-81-18-300-001 Main Landing-Gear Door - Replacement of the Central-Ramp Teflon Strip WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______ CARBONFIBER REINFORCED PLASTIC.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific 1 ACCESS PLATFORM 2M (6 FT) No specific 1 SCRAPER - NON METALLIC No specific 1 WARNING NOTICE
 1EFF : ALL 1 52-81-18Page 801 1 1 Aug 01/04 1 1 1CES 1

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-005 USA MIL-S-81733 CLASS C
 CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) Material No. 11-010 USA TT-I-735 GRADE A
 ISOPROPYL ALCOHOL (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
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8(105)