• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-05-21 10:19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

Radial gear marks on tooth wear pattern, which are produced by metal-to-metal contact.
Probable Cause
Careless handling.
Careless handling.
Excessive stress due to shock, overloading or faulty processing; extension of a nick or scratch; defective material; overheating.
Excessive heat generation in the gear mesh, from marginal lubrication.
Material has gone past it’s endurance limit.
Excessive heat generation in the gear mesh, that causes lubrication breakdown, which produces metal-to-metal contact.
Inspection
Page 334 Apr 1/05 Copying, use or disclosure of information on this page is subject to proprietary restrictions.
20-00-02/70-00-01

G. Visual Inspection
(1)
General Information

(a)
Visual inspection involves viewing the part for general appearance in an effort to locate conditions, which cause or indicate abnormal wear.  Whenever these conditions exist, the inspector shall refer to dimensional inspection requirements in the applicable manual related to damaged part to decide if rework is feasible.

(b)
Where no evidence of damage or wear is present, the inspector shall determine if dimensional inspection is required. After a decision has been reached, the part shall be tagged accordingly in the manner utilized by the particular overhaul facility.  The disposition of the part shall then be noted on the inspection records.

(c)
Parts, which are normally replaced at each overhaul, shall be given cursory inspection, since damage to these parts may sometimes reflect malfunction of other components. This is not only a good assumption to make about parts normally replaced, but shall be considered when any part has been damaged. Certain special visual inspections, required for some parts, are reflected in the following steps.

(d)
Information in this section supplements model-specific visual inspection requirements in the applicable inspection manual and/or workscope planning guide.

 

(2)
Inspect parts in accordance with the following procedures:

.  
Threaded parts
. Check threaded parts for stripped, galled, or crossed threads.


.  
Threaded inserts
. Check thread inserts for security and condition of threads.


.  
Threaded Keensert inserts
. Check thread insert for security and condition of threads.


.  
Threaded Keensert studs . Check threaded portion for stripped, galled or crossed threads. . Check stud for security. Axial movement of stud shall not exceed 0.0076 inch

(0,1930 mm). No rotational movement of stud is allowed. . If axial movement of stud exceeds limits specified in Sub-step (b) above, refer to Repair, Section IV.

.  
Bearing bores and diameters . Check all bearing bores and diameters for corrosion, wear and scoring.

 


Inspection
Page 335
Apr 1/05

20-00-02/70-00-01

.  All bearing bores and diameters shall be free of obvious damage.  Radial scoring lines not exceeding 0.005 inch (0,127 mm) in width or 0.005 inch (0,127 mm) in depth, which do not cover more than 30 percent of bearing surface and do not penetrate protective coating, dry-film lubricant, or other finishes applied to base metal of the bore or diameter, are acceptable.
.  
Plated surfaces

.  Check dry-film lubricated, plated, anodized, and painted parts for wear through to base metal.

.  
Press-fitted parts

.  Visually check press-fitted bearings, bushings, pins, plugs, sleeves, spacers, and restrictors for security and condition.

.  
Sealing surfaces and flanges . Visually check all sealing surfaces and flanges for nicks, dents, and scratches.

.  
Passageways . Visually check all air and oil passageways for corrosion and foreign obstructions.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:标准施工手册 STANDARD PRACTICES MANUAL 20-00-02/70-00-01(50)