What was found
FUSELAGE EXTERIOR SURFACE FROM BS 654+88 TO 654+ 110, STRINGER 30 - 31L FOUND DENTED AND CRACKED. REPAIRED IAW SRM 53-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR SURFACE FROM BS 654+88 TO 654+ 110, STRINGER 30 - 31L FOUND DENTED AND CRACKED. REPAIRED IAW SRM 53-00-01.