What was found
INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 950, THREE INCHES BELOW LONGERON 14L. THE CRACKED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 950, THREE INCHES BELOW LONGERON 14L. THE CRACKED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38.