What was found
LOWER FUSELAGE ANGLE CRACKED AT BS 663.75, LBL 27. R & R ANGLE IAW SRM & DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE ANGLE CRACKED AT BS 663.75, LBL 27. R & R ANGLE IAW SRM & DWG.