• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 08:50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

Material No. 11-004  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
 Material No. 15-005  AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 15-005A  AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 15-006  AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 EFF : ALL
53-41-00Page 701
Feb 01/04
R
 CES


 C. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
53-35-11-000-001 Removal of the Wing-to-Fuselage Fairings 53-35-11-400-001 Installation of the Wing-to-Fuselage Fairings 53-35-12-000-002 Removal of the Belly Fairing Blowout Panel 53-35-12-400-002 Installation of the Belly Fairing Blowout Panel 53-35-13-000-001 Removal of the Belly Fairing Access Panels 53-35-13-400-002 Installation of the Quick-Release Access Panels on
 the Belly Fairing Structure
 53-41-00-991-034 Fig. 701

 3. Job Set-up
__________
 Subtask 53-41-00-010-117
 A. Get Access
 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.
 (1)
 Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever when working near the flaps/slats.

 (2)
 Put the warning notice on the slat/flap control lever to tell persons not to operate the slats/flaps.

 (3)
 Put the adjustable access platform in the required position.

 (4)
 Remove all the following panels (Ref. TASK 53-35-11-000-001), (Ref. TASK 53-35-12-000-002) and (Ref. TASK 53-35-13-000-001) from the belly fairing support structure.


 Subtask 53-41-00-110-079
 B. Cleaning Procedure
R WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ R MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
 EFF : ALL
53-41-00Page 702


 WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
 (1) Remove the old temporary protection compound from the area to be treated with a non metallic scraper, and clean with CLEANING AGENTS (Material No. 11-004) and a lint free cloth. Make sure that the area is dry before you continue.
 4. Procedure
_________
 CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS.
_______ MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET: -ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS,TEFLON BEARINGS. -ON LUBRICATED SURFACES. -IN DRAIN VALVES OR OTHER ORIFICES. TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE.
R **ON A/C 001-049, 051-099, 101-149, 201-299,
 Subtask 53-41-00-916-069
 A. Temporary Protection Procedure
 (Ref. Fig. 701/TASK 53-41-00-991-034)

 (1) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-005A) or STORAGE PRESERVATION (Material No. 15-006) or equivalent to the fuselage external skin and the belly fairing support structure, contained in the belly fairing, between FR30 and FR53.
 EFF : ALL
53-41-00Page 703


 Fuselage External Surface, contained in the Belly Fairing, and Belly Fairing

 Support Structure zone 190
 Figure 701/TASK 53-41-00-991-034
 EFF :  ALL  53-41-00 Page 704 
Feb 01/98
 CES 

 

R **ON A/C 151-199, 401-499,
 Subtask 53-41-00-916-069-A
 A. Temporary Protection Procedure
 (Ref. Fig. 701/TASK 53-41-00-991-034)

 (1) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-005A) or STORAGE PRESERVATION (Material No. 15-006) or equivalent to the fuselage external skin and the belly fairing support structure, contained in the belly fairing, between FR27 and FR57.
 
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 FUSELAGE 机身3(71)