What was found
FRAME 12A, RT FUSELAGE FITTING IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5310-23539-G, APPENDIX E.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME 12A, RT FUSELAGE FITTING IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5310-23539-G, APPENDIX E.