What was found
LEFT UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L APPROXIMATELY 3/4 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.
LEFT UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L APPROXIMATELY 3/4 INCH LONG. INSTALLED A REPAIR DOUBLER, FILLER, SHIM, REPAIR ANGLE IAW SRM 53-31-01,FIGURE 219, SHEET 1.