What was found
VERTICAL STAB LT AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO C700-55MR-001-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB LT AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO C700-55MR-001-0.