Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
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If depth is more than limit or wider than 0.1 in. (2.54 mm) regard as a crack 10 in. (254 mm) minimum separation from other damage
R D. Hole 1 in. (25.4 mm) minimum separation from other holes Seal with aerodynamic tape(Material No. CP2517).
R Monitor at "A" check.
R R R Permanent repair at "C" check recommended (Ref. SRM 541000).
0.25 in. (6.35 mm) maximum diameter hole permitted Fill hole with aluminumblind rivet, wet withsealant (Ref. SRM 541000).
Subtask 71-11-00-210-054
D. Do a Visual Inspection of the Intake Cowl Forward and Aft Bulkheads
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INSPECT/CHECK MAXIMUM SERVICEABLE LIMITS REMARKS
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1. Examine the forward and aft bulkhead fasteners, joints, and doublers for:
R A. Crack One fastener space maximum length for crack. Must be stopped between two adjacent fasteners Monitor at "A" check.
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R R R
2. Examine the forward and aft bulkheads for:
A. Crack
R B. Dent or buckle
R R R
R C. Scratch or Gouge
R R R 10 in. (254 mm) minimum separation from other cracks
No cracks permitted in bulkheads
3 in. (76.2 mm) maximum length 0.10 in. (2.54 mm) maximum depth
1 in. (25.4 mm) minimum from edge of stiffeners or webs Dents must be smooth and free from creases, gouges, and cracks
10 in. (254 mm) minimum separation between dents
6 in. (152.4 mm) maximum length around intake cowl circumference Permanent repair at "C" check recommended (Ref. SRM 541000).
Repair cracks beforeflight (Ref. SRM 541000).
Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
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-------------------------------------------------------------------------------2 in. (50.8 mm) maximum length in radial direction
0.01 in. (0.25 mm) maximum depth
0.1 in. (2.54 mm) maximum width 6 in. (152.4 mm) minimum separation from other damage
D. Holes No holes permitted Repair before flight (Ref. SRM 541000).
5. Close-up
________
Subtask 71-11-00-410-052
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-040):
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
(3) Remove the access platform(s).
(4) Remove the warning notice(s).
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