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时间:2011-03-27 16:58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

 A. Radial cracks extending out of gill holes.  Any number ; no missing material. 
B. Other cracks (not in gill hole rows).  Any number ; no missing material. 
C. Burns and cracks.  Any number ; no missing material or burn through. 
3. Convex surface of vane airfoil for:
 A. Radial cracks.  Any number.
 B. Axial cracks.  Any number.
 C. Burns and bulges.  Any number. 

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See limit extension (Ref. TASK 72-00-00-200-025).
See limit extension(Ref. TASK 72-00-00-200-025).
See limit extension(Ref. TASK 72-00-00-200-025).
See limit extension(Ref. TASK 72-00-00-200-025).
See limit extension (Ref. TASK 72-00-00-200-025).


72-51-00Page 607
May 01/98

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 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
D. Missing panel 
R R R  E. Missing Thermal Barrier Coating (TBC)
 4. Trailing edge of vane airfoil for:
 A. Axial cracks starting from slots adjacent to trailing edge
 B. Burns and cracks. 
C. Buckling or bowing 
D. Missing material (loss of metal). 
5. All areas of airfoil for:
 A. Craze cracking. 

Not serviceable.
Any amount.
Any number.
Any number.
Any amount.
Total area removed from trailing edge not to be more than 0.5 in. (12.7 mm) in axial direction.
Any amount.
See limit extension (Ref. TASK 72-00-00-200-025).
See limit extension(Ref. TASK 72-00-00-200-025).
 NOTE : Craze cracking looks like many surface cracks that have no visual
____ width or depth.
 B. Nicks, scores,  Any number.
 scratches and
 dents.
 C. Metal splatter.  Any amount.
 D. Missing codep  Any amount.
 coating.

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 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
6. Inner and outer
 platform for:
 A. Cracks in parent metal.  Any number.
R R R R  B. Missing metal or burning of parent metal.  No through holes, but any amount of missing material from cracking or burning is permitted.
 C. Nicks, scores, scratches and Any amount.
 dents or platform surface.
 D. Bulging and bowing.  Any amount.
R R R R  E. Cracks in platform braze joint.  Any amount, no separation of braze joint allowed unless caused by burning.

See limit extensions (Ref. TASK 72-00-00-200-025).
(1) When the inspection is complete, turn off the light source and remove the borescope and the guide tube.

 (2) If any defects are found then remove additional borescope plugs and the spark igniters to inspect all of the HPT nozzle assembly.


 Subtask 72-51-00-010-055
 C. Remove parts before borescope inspection.
 (1) Remove the drain tube from the fuel nozzle adjacent to the 6 o'clock borescope plug.
 NOTE : If you remove the drain tube from the fuel nozzle adjacent to
____ the 6 o'clock borescope plug, you will be required to perform a leak check after this inspection. Use the 6 o'clock borescope port only if necessary.
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 (2) Remove the borescope plugs from the approximate 1 and 6 o'clock positions.

 (3) Remove both spark igniters (Ref. TASK 74-21-30-000-002)
 Subtask 72-51-00-290-053
 D. Do a borescope inspection.
 (1) Repeat paragraph 4.B.(1) thru (6) for each borescope and spark igniter location.
 Subtask 72-51-00-410-054
 E. Install parts removed for borescope inspection.
 CAUTION : BE SURE TO INSTALL THE CORRECT BORESCOPE PLUGS. THE COMBUSTOR
_______ BORESCOPE PLUGS DO NOT HAVE A STEM FEATURE. INADVERTENT INSTALLATION OF BORESCOPE PLUGS WITH STEMS FROM OTHER LOCATIONS WILL RESULT IN THE STEM FEATURE BEING BURNED AWAY BY COMBUSTION GASES.
R (1) Apply a small amount of graphite grease (Material No. CP2101) or R Never Seez-Pure Nickel, Special (Material No. CP2619) to the R borescope plug threads and pressure faces.
 
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