What was found
FUSELAGE TO VERTICAL STABILIZER INNER ATTACH ANGLE CRACKED AT BS 1135, LONGERON 2L. R & R ANGLE IAW SRM & DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE TO VERTICAL STABILIZER INNER ATTACH ANGLE CRACKED AT BS 1135, LONGERON 2L. R & R ANGLE IAW SRM & DWG.