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时间:2011-03-27 16:58来源:蓝天飞行翻译 作者:航空
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 (1) Remove the borescope plugs from the approximate 3 and 10 o'clock positions on the combustion case.
 Subtask 72-42-00-290-054
 B. Do a borescope inspection.
 (1) Use the MONITOR, RESOLUTION BORESCOPE (856A1323G01) to make sure the borescope and the lightsource are serviceable. See the Non-Destructive Test Manual for this procedure (Ref. NTM 720000).
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 Combustion Chamber (Inner and Outer Liner Inspection)
 Figure 601/TASK 72-42-00-991-301

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 Combustion Chamber (Sectional View)
 Figure 602/TASK 72-42-00-991-302

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R  Cracks and Missing Material in Dome Area Figure 603/TASK 72-42-00-991-303
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 Outer Liner (Inner)
 Figure 604/TASK 72-42-00-991-305

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R  Inner Liner (Inner) Figure 605/TASK 72-42-00-991-306
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 (2) Connect the fiber light cable to the BORESCOPE KIT (856A1320P04/P05) and to the port on BORESCOPE - LIGHT SOURCE SET (856A1322P03/P04/P07).

 (3) Put the rigid borescope, (856A1320P04/P05), into the ports and turn on the light source of borescope-lightsource set (856A1322P03 or P04).

 (4) Turn the rigid borescope a full 360 degrees to inspect the dome of the combustion chamber, fuel nozzles, the inner and outer liners, and the aft sections. Adjust the borescope equipment to obtain maximum clarity of view.

 (5) Inspect the following :


 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
1. All surfaces for :
 A. Discoloration Any amount
 B. Carbon  Any amount
 Accumulation

 C. Missing, chipped  Any amount
 or spalled areas
 of thermal barrier
 coating

 2. Dome Assembly (Spectacle Plate, Deflector amd Sleeve) for :
 A. Distortion of  Any amount
 deflector or
 sleeve

 B. Radial crack in Any number up to 1 in. See limit extension
 spectacle plate (25.4 mm) length and not (Ref. TASK 72-00-00-200-connected to each other 025)
 C. Circumferential  Any number up to 3 in. See limit extension crack in spectacle (76.2 mm) length (Ref. TASK 72-00-00-200-plate separated by 6 in. 025)
 (152.4 mm)
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 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS
 -------------------------------------------------------------------------------R D. Connected cracks Not more than (1) radial See limit extension R in spectacle plate crack 1 in. (25.4 mm) (Ref. TASK 72-00-00-200-
long with (1) 025) circumferential crack 3 in. (76.2 mm) long
 E. Missing material  Max. 0.06 in. (1.52 mm) See limit extension from spectacle x 0.06 in. (1.52 mm) at (Ref. TASK 72-00-00-200-plate intersection of 025)
 connected crack
 F. Radial crack in  Any number up to 0.5 in. See limit extension deflector or (12.7 mm) length (Ref. TASK 72-00-00-200-sleeve 025)
 G. Circumferential  Any number up to 0.75 See limit extension cracks in in. (19.05 mm) (Ref. TASK 72-00-00-200-deflector or 025) sleeve
 H. Connected cracks  Connection of any radial See limit extension in deflector or and circumferential (Ref. TASK 72-00-00-200-sleeve cracks within limits of 025)
 paragraphs F. and G. above. Limit is exceeded when third crack connects
 J. Missing material  Any amount up to 0.2 in. See limit extension from overhangs on (5.08 mm) maximum depth. (Ref. TASK 72-00-00-200-deflector or 025) sleeve
 K. Burn through holes  3 per dome 1 in. (25.4 See limit extension mm) x 1 in. (25.4 mm) (Ref. TASK 72-00-00-200-maximum 025)
 
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