What was found
HEAVY CHECK COE, MAJOR REPAIR. FUSELAGE SKIN PANEL HAS AN OUTWARD DENT AFT OF FRAME 29 BETWEEN LT STRINGER 18 - 19. SINGLE RIVET REPAIR SRM 53-00-00 REPAIR 420 REV 101.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HEAVY CHECK COE, MAJOR REPAIR. FUSELAGE SKIN PANEL HAS AN OUTWARD DENT AFT OF FRAME 29 BETWEEN LT STRINGER 18 - 19. SINGLE RIVET REPAIR SRM 53-00-00 REPAIR 420 REV 101.