What was found
LEFT AND RIGHT FUSELAGE TO VERTICAL STABILIZER ATTACHMENT DRAG ANGLES ARE CRACKED AT REAR SPAR DATUM 67.5 PERCENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT AND RIGHT FUSELAGE TO VERTICAL STABILIZER ATTACHMENT DRAG ANGLES ARE CRACKED AT REAR SPAR DATUM 67.5 PERCENT.