What was found
AFT PIT FUSELAGE STRINGER 44 CORRODED BETWEEN FR 62 - FR 63. REPAIR ACCOMPLISHED IAW SRM 53-00-13 FIG 201, SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT PIT FUSELAGE STRINGER 44 CORRODED BETWEEN FR 62 - FR 63. REPAIR ACCOMPLISHED IAW SRM 53-00-13 FIG 201, SHEET 3.