What was found
HOLE FOUND IN FUSELAGE ALONG STRINGER 28L BETWEEN FRAMES 19 AND 20 ON BOTTOM OF FUSELAGE. C/A-INSTALLED REPAIR DOUBLER, TRIPLER & FILLER IAW SRM 53-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HOLE FOUND IN FUSELAGE ALONG STRINGER 28L BETWEEN FRAMES 19 AND 20 ON BOTTOM OF FUSELAGE. C/A-INSTALLED REPAIR DOUBLER, TRIPLER & FILLER IAW SRM 53-10-01.