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时间:2011-03-27 16:55来源:蓝天飞行翻译 作者:航空
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R R  Fan Rotor Blades - Local Distortions Figure 607/TASK 72-21-00-991-315- 34 (SHEET 3)
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R R  Fan Rotor Blades - Local Distortions Figure 607/TASK 72-21-00-991-315- 44 (SHEET 4)
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B. Nicks, dents and  No limited quantity, if  Replace blade (Ref. TASK
 scratches on  not deeper than 0.003  72-21-00-000-007) and
 contour surfaces  in.(0.08 mm) after  (Ref. TASK 72-21-00-400-
of root area, and  removal of high metal.  007) or blend the defects
 full airfoil out  if damage is within the
 of midspan shroud  blending limit of figure
 (Ref. Fig. 606/TASK 72-21-
00-991-314)
 critical area.  Blended fan blades must be
 repaired following ESM
 72-21-01 Rep 01 at first
 shop visit opportunity.
 C. Nicks, dents and  No limited quantity, if  Do blending procedure
 scratches on  not deeper than 0.006  (Ref. TASK 72-21-00-320-
leading edge of  in.(0.15 mm)  003)
 root area, Area A.
 D. Nicks, dents and  No limited quantity, if  Replace blade (Ref. TASK
 scratches on  not deeper than 0.006  72-21-00-000-007) and
 trailing edge,  in. (0.15 mm).  (Ref. TASK 72-21-00-400-
Area D  007) or blend the defects
 (Ref. TASK 72-21-00-320-
003) if damage is within
 the blending limit of
 figure.
 (Ref. Fig. 606/TASK 72-21-
00-991-314)
 Blended fan blades must be
 repaired following ESM
 72-21-01 Rep 01 at first
 shop visit opportunity.
 E. Nicks, dents and  No limited quantity, if  Replace blade (Ref. TASK
 scratches on  not deeper than 0.03 in.  72-21-00-000-007) and
 leading edge in  (0.76 mm), with 0.40 in.  (Ref. TASK 72-21-00-400-
Area B.  (10.16 mm) max length  007) or blend the defectts
 for scratches after  (Ref. TASK 72-21-00-320-
removal of high metal.  003) if damage is within
 the blending limit of
 figure.
 (Ref. Fig. 606/TASK 72-21-
00-991-314)

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 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS
 -------------------------------------------------------------------------------Blended fan blades must be repaired following ESM 72-21-01 Rep 01 at first shop visit opportunity.
 F. Localized  Not serviceable. Replace blade (Ref. TASK distortion on 72-21-00-000-007) and leading and (Ref. TASK 72-21-00-400-trailing edges of 007). root area, Area A.
 G. Leading and  Two areas may be Do a spot trailing edges distorted up to 0.34 in. fluorescent-penetrant distortion in (8.64 mm) out of contour inspection (Ref. TASK 70-Areas B and D (out provided there are no 51-00-230-002) of root area sharp corners and the trailing edge). minimum length L is six
 times the depth of the distortion.
 H. Blade tip (Area C)  Tip curl must not extend Replace pair of blades if for: more than dimension not in the limits
R (1) Leading edge X1=0.5 in. (13 mm) (Ref. TASK 72-21-00-300-
tip curl  across the blade tip and 028) not more than dimension No continued in-service X=0.5 in. (13 mm), along extension is permitted. the leading edge. Maximum deflection from original contour is dimension Y=0.25 in.
 (6.35 mm). A maximum of 6 blades must not have tip curl up to dimension X1=1.3 in. (33 mm) across the blade tip and dimension X=2 in. (51 mm) along the leading edge with maximum deflection from original contour dimension Y=0.6 in. (15 mm). Not more than 3
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