What was found
NOSE WHEEL WELL STRUCTURE ON INTERIOR OF FUSELAGE CHORD CRACKED AT BS 340, WL 200, LBL 10. REPAIRED IAW MFG MM. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NOSE WHEEL WELL STRUCTURE ON INTERIOR OF FUSELAGE CHORD CRACKED AT BS 340, WL 200, LBL 10. REPAIRED IAW MFG MM. (K)