What was found
FUSELAGE SKIN DENTED AT LAP JOINT (APPROX FR 28) BELOW AFT EDGE OF C1 DOOR CUTOUT. EVIDENCE OF PRESSURE LEAK. REPAIRED IAW SRM 53-00-11 PARA 4E FIG 211.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DENTED AT LAP JOINT (APPROX FR 28) BELOW AFT EDGE OF C1 DOOR CUTOUT. EVIDENCE OF PRESSURE LEAK. REPAIRED IAW SRM 53-00-11 PARA 4E FIG 211.