Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
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10 in. (254 mm) minimum separation from other craks, holes and disbonds
Regard as hole if more than 0.01 in. (0.25 mm) wide
Maximum five cracks each barrel half
R B. Scratch or Gouge 0.01 in. (0.25 mm) maximum depth over 6 in. (152.4 mm) maximum length Seal with aerodynamic tape(Material No. CP2517).
R Monitor at "A" check.
R R R Permanent repair at "C" check recommended (Ref. SRM 541000).
0.10 in. (2.54 mm) maximum width
Six maximum each barrel half
8 in. (203.2 mm) minimum separation from other damage
R C. Hole 3 in. (76.2 mm) maximum diameter Seal with aerodynamic tape(Material No. CP2517).
R Monitor at "A" check.
R R R Permanent repair at "C" check recommended (Ref. SRM 541000).
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1 in. (25.4 mm) minimum from edge of panel
10 in. (254 mm) minimum separation from other damage
Maximum of three holes each panel
Subtask 71-11-00-210-052
B. Do a Visual Inspection of the Intake Cowl Inner Barrel
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INSPECT/CHECK MAXIMUM SERVICEABLE LIMITS REMARKS
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1. Examine the intake cowl inner barrel for:
R A. Delamination 1.5 in. (38.1 mm) maximum width Monitor at "A" check.
R R R Permanent repair at "C" check recommended (Ref. SRM 541000).
10 in. (254 mm) minimum separation from other voids or delamination Opposite void or delamination on other face sheet not permitted Maximum delamination length for bonded joints is 15 percent of joint lenght and not more than 0.2 in. (5.08 mm) to edge of joint strip
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R B. Dent 0.12 in. (3.05 mm) maximum depth Monitor at "A" check.
R R R Permanent repair at "C" check recommended (Ref. SRM 541000).
1.5 in. (38.1 mm) maximum diameter 10 in.
(254 mm) minimum separation between dents Crushed core is
permitted. Regard as a dent
1.5 in. (38.1 mm) minimum from honeycomb core edge
R C. Gouge 0.01 in. (0.25 mm) maximum depth Monitor at "A" check.
R R R Permanent repair at "C" check recommended (Ref. SRM 541000).
0.1 in. (2.24 mm) maximum width
1 in. (25.4 mm) maximum length 10 in. (254 mm) minimum separation between
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