What was found
DAMAGE ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT. REWORKED AREA ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT WAS REPAIRED PER PERMANET REPAIR IAW SRM 53-02-01- 2R FIG. 202 (SHEET 13).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAMAGE ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT. REWORKED AREA ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT WAS REPAIRED PER PERMANET REPAIR IAW SRM 53-02-01- 2R FIG. 202 (SHEET 13).