What was found
FUSELAGE SKIN AT LWR AFT CORNER OF MAIN DOOR JAMB CRACKED. REPAIRED PER DC9 SRM 53-05 FIG 103 PAGE 407-418 & 420. REPAIR IS CAT-B N5343 ASSIGNED INSP WITHIN 28,000 CYCLES PER SRM 51-10-5C (EDDY CURRENT).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT LWR AFT CORNER OF MAIN DOOR JAMB CRACKED. REPAIRED PER DC9 SRM 53-05 FIG 103 PAGE 407-418 & 420. REPAIR IS CAT-B N5343 ASSIGNED INSP WITHIN 28,000 CYCLES PER SRM 51-10-5C (EDDY CURRENT).