• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 14:35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

 (4)
 Clean and examine the attachment brackets, the APU mount-bracket (14) and the structure for damage and replace if nescessary.


 **ON A/C 001-049, 101-105, 201-203,
 Subtask 49-12-52-420-056
 B. Installation of the Vibration Isolator CAUTION : WHEN YOU REMOVE (INSTALL) THE APU, DISENGAGE (ENGAGE) ALL THE
_______ VIBRATION ISOLATORS AT THE SAME TIME FROM THE APU MOUNT BRACKETS. IF YOU DISENGAGE (ENGAGE) THEM ONE AFTER THE OTHER, THE LOADS WILL NOT BE EQUAL. THIS WILL CAUSE DAMAGE TO THE TIE RODS.
 (1)
 Apply SPECIAL MATERIALS (Material No. 05-002) to all mating surfaces. Do not apply it to the bonding straps.

 (2)
 Install the vibration isolator (16) on the APU mount-bracket (14).

 (3)
 If removed install the tie-rods (4) and (6).


 (a) Install the bolts (18), the washers (19) and the castle nuts (20).
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-52Page 411 201-210, Config-2 Aug 01/05
 CES


 (b)
 TORQUE the castle nuts (20) to between 0.55 and 0.75 m.daN (48.67 and 66.37 lbf.in) and safety them with the new cotter pin (21)

 (c)
 Connect the bonding straps (10).

 (d)
 Install the bolts (7), the washers (8) and the nuts (9).

 (e)
 TORQUE the nuts (9) to between 0.22 and 0.26 m.daN (19.46 and


 23.00 lbf.in)
 (4)
 Install the tie-rods (4) and (6) at the vibration isolator.

 (5)
 Install the bolts (5) and (17), the washers (1) and (12) and the castle nuts (2) and (13).

 (6)
 TORQUE the castle nuts

 -
item (2) to between 0.3 and 0.35 m.daN (26.54 and 30.97 lbf.in),

 -
item (13) to between 0.55 and 0.75 m.daN (48.67 and 66.37 lbf.in) and safety them with the new cotter pin (3) and cotter pin (11).

 

 (7)
 Remove the PROTECTOR - THREADS, APU MOUNTING BOLTS and install the nut (15).

 (8)
 TORQUE the nut (15) to between 2.5 and 3.1 m.daN (18.43 and 22.86 lbf.ft)

 

R  **ON A/C 107-107, 151-199, 204-210,
 Subtask 49-12-52-420-056-A
 B. Installation of the Vibration Isolator
 (1) 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 mating surfaces. Do not apply it to the bonding straps.
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-52Page 412 201-210, Config-2 Aug 01/05
 CES


 (2)
 Install the vibration isolator (16) on the APU mount-bracket (14).

 (3)
 If removed install the tie-rods (4) and (6).

 (a)
 Install the bolts (18), the washers (19) and the castle nuts (20).

 (b)
 Tighten and TORQUE the castle nuts (20) to between to between

 0.55 and 0.75 m.daN (48.67 and 66.37 lbf.in) and safety them with the new cotter pin (21)

 (c)
 Connect the bonding straps (10).

 (d)
 Install the bolts (7), the washers (8) and the nuts (9).

 (e)
 Tighten and TORQUE the nuts (9) to between to between 0.22 and

 0.26 m.daN (19.46 and 23.00 lbf.in)

 (f)
 Install the clamps (26) and (27) with the bolts (22), the washers (23), the bonding strap (24) and the nuts (25) at the tie-rod (4).

 

 (4)
 Install the tie-rods (4) and (6) at the vibration isolator.

 (5)
 Install the bolts (5) and (17), the washers (1) and (12) and the castle nuts (2) and (13).

 (6)
 Tighten and TORQUE the castle nuts

 -
item (2) to between to between 0.3 and 0.35 m.daN (26.54 and 30.97 lbf.in),

 -
item (13) to between to between 0.55 and 0.75 m.daN (48.67 and


 66.37 lbf.in) and safety them with the new cotter pin (3) and cotter pin (11).

 (7)
 Remove the PROTECTOR - THREADS, APU MOUNTING BOLTS and install the nut (15).

 (8)
 Tighten and TORQUE the nut (15) to between 2.5 and 3.1 m.daN (18.43 and 22.86 lbf.ft)

 

R  **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
 Subtask 49-12-52-080-052
 C. Remove the APU hoist (Ref. TASK 49-00-00-080-003)

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-52Page 413 201-210, Config-2 Aug 01/05
 
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 POWER2(96)