What was found
INSPECTION FOUND CRACKS IN THE NLG WHEEL WELL TOP LEFT AND TOP RIGHT SKIN PANELS. THE CRACKS WERE .75 TO 1 INCH LONG. THE SKIN WAS REMOVED IAW SRM 51-10-1. WEB SKIN WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND CRACKS IN THE NLG WHEEL WELL TOP LEFT AND TOP RIGHT SKIN PANELS. THE CRACKS WERE .75 TO 1 INCH LONG. THE SKIN WAS REMOVED IAW SRM 51-10-1. WEB SKIN WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.