F EEFF : ALL E E ECES No carbon fiber damage permitted, treat as a scratch if fibers are damaged
No crack permitted in outer edge
No delamination permitted in outer edge
0.01 in. (0.25 mm) maximum depth over 6 in.
(152.4 mm) maximum length 『E EEESeal with aerodynamic tape(Material No. CP2517).
Monitor at "A" check.
Replace tape if peeled or damaged.
Permanent repair at "C"
check recommended (Ref.
SRM 541000).

Repair crack before flight(Ref. SRM 541000).
Repair crack before flight(Ref. SRM 541000).
Seal with aerodynamic tape(Material No. CP2517).
Monitor at "A" check.
71-11-00Page 603
May 01/05 F 『 E C F M E E E E 56-5B E

 Intake Cowl Outer Barrel
 Figure 601/TASK 71-11-00-991-302

 F 『 EEFF : ALL E Page 60471-11-00
 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E

 Intake Cowl Inner Barrel
 Figure 602/TASK 71-11-00-991-303

 F 『 EEFF : ALL E Page 60571-11-00
 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E

 Intake Cowl Lip
 Figure 603/TASK 71-11-00-991-304

 F 『 EEFF : ALL E Page 60671-11-00
 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E

 Intake Cowl Forward and Aft Bulkeads
 Figure 604/TASK 71-11-00-991-305

 F 『 EEFF : ALL E Page 60771-11-00
 E E Feb 01/98 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E

 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
R
R
R

E. Hole
2. Examine outer barrel skin for:
 A. Abrasion
R
R R
R R R
R B. Crack
R
R R R
F
EEFF : ALL
E
E
ECES

0.10 in. (2.54 mm) maximum width
 Six maximum each barrel half
 8 in. (203.2 mm) minimum separation from other damage
No hole permitted
No carbon fiber damage permitted, treat as a scratch if fibers are damaged
3 in. (76.2 mm) maximum length
『E EEE
Permanent repair at "C"
check recommended (Ref.
SRM 541000).

For permanent repair (Ref. SRM 541000).
Seal surface aerodynamictape (Material No.CP2517).
Monitor at "A" check.
Replace tape if peeled or damaged.
Permanent repair at "C"
check recommended (Ref.
SRM 541000).

Seal with aerodynamic tape(Material No. CP2517).
Monitor at "A" check.
Permanent repair at "C"
check recommended (Ref.
SRM 541000).

71-11-00Page 608
May 01/05

 F 『
 E C F M E
 E E
 E 56-5B E
 E E

 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
10 in. (254 mm) minimum
 separation from other
 cracks, holes, and
 disbonds
 Maximum five cracks per
 barrel half
 Regard as hole if more
 than 0.01 in. (0.25 mm)
 wide 
R  C. Delamination  3 in. (76.2 mm) maximum 
diameter 
R 
R 
R 
10 in. (254 mm) minimum
 separation from other
 damager
 0.25 in. (6.35 mm)
 minimum from edge of
 panel
 Maximum five
 delaminations per panel
 1 in. (25.4 mm) maximum
 length parallel to edge
 of panel 
R  D. Scratch or Gouge  0.01 in. (0.25 mm) 
maximum depth over 6 in. 
(152.4 mm) maximum
 length 
R 
R 
R 
R 
F  『
 EEFF :  ALL  E 
E  E
 E  E
 ECES  E

Monitor at "A" check.
Permanent repair at "C"
check recommended (Ref.
SRM 541000).

Seal with aerodynamic tape(Material No. CP2517).
Monitor at "A" check.
Permanent repair at "C"
check recommended (Ref.
SRM 541000).

71-11-00Page 609
May 01/05

 F 『
 E C F M E
 E E
 E 56-5B E
 E E

 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
　
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