What was found
LEFT FORWARD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. REPAIRED IAW EO CR-55MR-038 PART A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FORWARD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. REPAIRED IAW EO CR-55MR-038 PART A.