• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 17:17来源:蓝天飞行翻译 作者:航空
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

 (1) Remove the sealant from the lower struts, the lower stop, the pipe bundle box, the lower channel bracket, the upper forward seal fitting, the outer flanges, the upper outer seal fitting, the inner flanges and the splice assembly with a plastic scraper.

 (2) Clean the areas:


 WARNING : BEFORE THE USE OF SOLVENT, PROTECTIVE FILM OR SEALANT
_______ CAREFULLY READ THE APPLICABLE "MATERIAL SAFETY DATA SHEET" AND FOLLOW ALL LISTED SAFETY AND HEALTH PRECAUTIONS. USE THESE PRODUCTS IN AN AREA OPENED TO THE AIR AND WEAR PROTECTION GLOVES. THESE PRODUCTS ARE FLAMMABLE AND VAPOR IS DANGEROUS. THEY MAY CAUSE IRRITATION OF EYES, NOSE, THROAT AND SKIN. HIGH CONCENTRATIONS MAY CAUSE WEAKNESS, HEADACHE, NAUSEA, DIZZINESS AND IMPAIRED JUDGEMENT.
R (a) Clean the areas where you removed the sealant acetone (Material R No. CP1039) or stoddard solvent (Material No. CP2011) or ardrox R 552 (Material No. CP2559) or turco ind 79 (Material No. CP2560) R or mag-chem teksol (Material No. CP2566) or degreasol 99 R R (Material No. CP2584) or mag-chem skysol (Material No. CP2656) or R isopropyl alcohol (Material No. CP1041).
 (3) Dry the areas with a clean cloth.
 F 『 EEFF : ALL E Page 41878-36-42
 E E May 01/05 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E


 TASK 78-36-42-400-001
 Installation of the Adapter Ring Assembly
 CAUTION : DO NOT DROP ANY BOLT OR WASHER IN VARIABLE BLEED VALVE AREA. THIS
_______
 COULD CAUSE DAMAGE TO ENGINE.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 No specific HIX3013-OG
 No specific access platform 1 m (3 ft. 3 in.)
 No specific Torque Wrench : range 36.00 to 220.00 lbf.in

 (0.40 to 2.60 m.daN)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. CP1039 * R acetone (Ref. 70-30-00) Material No. CP2011 USA MIL-D-12491 stoddard solvent (Ref. 70-30-00) Material No. CP2104 * molykote G rapid (Ref. 70-30-00) Material No. CP2245 * finish paint EA4 blue 5991 (Ref. 70-30-00) Material No. CP2267 *
 RTV 106 (Ref. 70-30-00) R Material No. CP2559 * R ardrox 552 (Ref. 70-30-00) R Material No. CP2560 * R turco ind 79 (Ref. 70-30-00) R Material No. CP2566 * R mag-chem teksol (Ref. 70-30-00)
 F 『 EEFF : ALL E Page 41978-36-42
 E E May 01/05 E E ECES E -------------------------------------------------------------------------------

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
R Material No. CP2584 *
R degreasol 99 R (Ref. 70-30-00)
R Material No. CP2656 *
R mag-chem skysol (Ref. 70-30-00) Material No. CP8001 * lockwire 0.032 in. (Ref. 70-30-00) Material No. CP8002 * lockwire 0.032 in. (Ref. 70-30-00)
 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors
 71-13-00-410-040 Closing of the Fan Cowl Doors
 78-30-00-081-041 Make the Thrust Reverser Serviceable after

 Maintenance 78-30-00-481-041 Make the Thrust Reverser Unserviceable for Maintenance 78-32-11-400-002 Installation of the Left or Right Half Door of Thrust
 Reverser
 78-36-42-991-301 Fig. 401
 78-36-42-991-302 Fig. 402
 78-36-42-991-303 Fig. 403
 78-36-42-991-310 Fig. 404
 78-36-42-991-311 Fig. 405
 78-36-42-991-312 Fig. 406
 78-36-42-991-304 Fig. 407
 78-36-42-991-306 Fig. 408

 3. Job Set-up
__________
 Subtask 78-36-42-860-050
 A. Aircraft Maintenance Configuration
 (1) On the center pedestal, on the ENG panel 115VU, make sure that a warning notice is in position to tell persons not to start the engine.
 F 『 EEFF : ALL E Page 42078-36-42
 E E May 01/05 E E ECES E

 F  『
 E  C F M  E
 E  E
 
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 EXHAUST 2(112)