• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 14:39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

No specific lockwire-corrosion resistant steel 0,8 mm Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 07-001 ELECTRICAL BONDING COATING (BLUE COLOR) (Ref. 20-31-00)
 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1 cotter pin 49-16-04 03 -070 12 bellows 49-16-04 03 -080 17 cotter pin 49-16-04 03 -070


 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-16-00-710-002 Operational Test of the Air Intake Flap and Diverter
 (APS 3200) 49-16-43-400-002 Installation of the Air Intake Flap (APS 3200) 49-16-51-991-002 Fig. 201
 3. Job Set-up
__________ Subtask 49-16-51-865-056
 A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
 Subtask 49-16-51-860-050
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the access platform is in position below the access doors 315AL and 316AR.

 (2)
 Make sure that the access door 314AR.


 4. Procedure
_________ (Ref. Fig. 201/TASK 49-16-51-991-002) Subtask 49-16-51-560-050
 A. Preparation of a Replacement Component
 (1) Make an inspection of the bellows (12) for cracks and damage. If necessary, replace the bellows as follows:
 (a)
 Remove the screws (14), the washers (13), the ring (9) and the bellows (12).

 (b)
 Install the new bellows (12), the ring (9), the washers (13) and the screws (14).

 


 Subtask 49-16-51-210-053
 B. Preparation for Installation
 (1)
 Make an inspection of the air intake flap and the structure fittings for cracks and corrosion. Replace the fittings if necessary.

 (2)
 Close and open the air intake flap manually and examine the adjustment. Adjust the air intake flap if necessary (Ref. TASK 49-16-43-400-002).

 (3)
 Protective Treatment


 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 (a) Apply SPECIAL MATERIALS (Material No. 05-002) to all the mating surfaces. Do not apply the putty to any part of the bonding jumper (21) or it's mating surface.
 Subtask 49-16-51-420-053
 C. Installation of the Air-Intake Flap Actuator
 (1)
 Hold the air intake flap in the top position.

 (2)
 Make sure that the new air-intake flap actuator (6) is in the flap open position (retracted).


 NOTE : Turn the manual override device on the air-intake flap
____ actuator with a torque wrench until the actuator rod is in the retracted position (which agrees with the open position of the air intake flap). For the 43-1-1100 Amendment 1 actuator a torque up to 0.3 m.daN (26.54 lbf.in) is permitted. For the 106-1-1100-02 actuator, a torque up to 0.4 m.daN
 (35.39 lbf.in) is permitted.


 Be careful when you come to the mechanical stop at the end of travel. If you turn the manual override device with a torque more than the limit, damage to the air-intake flap actuator will occur.
 NOTE : For the 43-1-1100 Amendment 1 actuator, approximately 47 turns
____ are necessary on the manual override device for one full travel of the air-intake flap actuator. For the 106-1-1100-02 actuator, approximately 87 turns are necessary on the manual override device for one full travel of the air-intake flap actuator.
 (3)
 Put the air-intake flap actuator (6) in position and install the bolt (5), the washers (3) and (4) and the castle nut (2).

 (4)
 TORQUE the castle nut (2) to between 0.7 and 0.8 m.daN (61.94 and

 70.79 lbf.in) and safety it with a new cotter pin (1).

 (5)
 Seal the connection with the SEALANTS (Material No. 09-016) and apply PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material No. 07-001).
 
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 机载辅助动力 AIRBORNE AUXILIARY POWER3(51)