What was found
RIGHT UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R APPROXIMATELY 3/8 INCH LONG. INSTALLED A REPAIR DOUBLER, FILLER, SHIM, REPAIR ANGLE IAW SRM 53-31-01, FIGURE 219, SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R APPROXIMATELY 3/8 INCH LONG. INSTALLED A REPAIR DOUBLER, FILLER, SHIM, REPAIR ANGLE IAW SRM 53-31-01, FIGURE 219, SHEET 1.