What was found
ACFT HAS A CRACK ON STIFFENER END, BETWEEN PROJECTION LONGERON 12LT AND 11LT AT PRESSURE BULKHEAD BS 1338. STIFFENER END WAS REPLACED IAW SRM 51-30-1, 51-30-5, SRM 51-10-4, AND 51-10-3 PAR 14, 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ACFT HAS A CRACK ON STIFFENER END, BETWEEN PROJECTION LONGERON 12LT AND 11LT AT PRESSURE BULKHEAD BS 1338. STIFFENER END WAS REPLACED IAW SRM 51-30-1, 51-30-5, SRM 51-10-4, AND 51-10-3 PAR 14, 21.