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时间:2011-03-27 16:55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

R R
R R
L. Missing coating on inner faces of platform.
 M. Fretting on dovetail pressure faces.
Flaking of Cu.Ni.In up  See limit extension
to 10 percent is  (Ref. TASK 72-00-00-200-
permitted if coating  025) and examine blades
adherence is correct in  for serviceability. Make
adjacent areas and if  sure that MoS2 dry film
there is no evidence of  lubricant is applied to
wear on base material.  disk slots, the blade
roots (dovetails), the
 blade platforms and
 lateral surfaces of those
 platforms, and the midspan
 shroud mating surfaces
 before blade installation 
(Ref. TASK 72-21-00-210-
004).
 Flaking of Cu.Ni.In over  See limit extension
 10 percent and less than  (Ref. TASK 72-00-00-200-
50 percent is permitted  025) and examine blades
 if coating adherence is  for serviceability. Make
 correct in adjacent  sure that MoS2 dry film
 areas and if there is no  lubricant is applied to
 evidence of wear on base  disk slots, the blade
 material.  roots (dovetails), the
 blade platforms and
 lateral surfaces of those
 platforms, and the midspan
 shroud mating surfaces
 before blade installation 
(Ref. TASK 72-21-00-210-
004) .
Any amount.
Not serviceable.  Replace pair of blades
(Ref. TASK 72-21-00-300-
028).


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N. Nicks, dents and  Not serviceable. Replace pair of blades scratches in (Ref. TASK 72-21-00-300-dovetail fillet 028). radius.
 P. Pits.  No limited quantity if Replace pair of blades not deeper than 0.005 (Ref. TASK 72-21-00-300-in. (0.13 mm). No limits 028). as regards diameter or spacing.
 Q. Nicks, dents and  No limited quantity if Replace blade (Ref. TASK scratches on not deeper than 0.010 72-21-00-000-007) and midspan shroud. in. (0.25 mm). No (Ref. TASK 72-21-00-400-
limited length for 007), or blend the defects scratches, and 0.5 in. (Ref. TASK 72-21-00-320-
(12.7 mm) diameter for 003) if damage is within dents. None permitted in the blending limit of midspan shroud critical figure.
 (Ref. Fig. 606/TASK 72-21-00-991-314)
 area.  Blended fan blades must be repaired following ESM 72-21-01 Rep 01 at first shop visit opportunity.

 R. Missing hard  Flaking of hard coating
 coating from is permitted if coating
 midspan shroud not adherence is correct in
 exceeding 10 adjacent areas.
 percent of the
 midspan shroud
 mating face.

 Missing hard Flaking of hard coating Monitor at every 2 "A" coating from is permitted if coating checks (800 cycles). midspan shroud adherence is correct in Remove and examine blades exceeding 10 adjacent areas. for serviceability percent but less (Ref. TASK 72-21-00-000-than 20 percent of 007). Make sure that MoS2 the midspan shroud dry film lubricant is mating face. applied to disk slots, the
 blade roots (dovetails),

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 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
the blade platforms and
 lateral surfaces of those
 platforms, and the midspan
 shroud mating surfaces
 before blade installation
 (Ref. TASK 72-21-00-400-
007).
 Missing hard coat  Not serviceable.  See limit extensions
 from midspan  (Ref. TASK 72-00-00-200-
shroud exceeding  025).
 20 percent of the
 midspan shroud
 mating face.
 S. Wear due to  Any amount up to 0.005  Replace pair of blades
 shingling on  in. (0.13 mm) deep.  (Ref. TASK 72-21-00-300-
midspan shroud.  028).
 T. High metal caused  Any amount after
 by shingling on  smoothing of high metal.
 
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