What was found
RT FWD MAIN GEAR DOOR WILL NOT CLOSED AFTER GEAR RETRACTION. R & R FAIL-SAFE PLATE, BELL CRANK LEVER TUBE HINGE PIN IAW MM 32-10-21 AND PERFORMED ALTERNATE EXTENSION IAW MM 32-35-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT FWD MAIN GEAR DOOR WILL NOT CLOSED AFTER GEAR RETRACTION. R & R FAIL-SAFE PLATE, BELL CRANK LEVER TUBE HINGE PIN IAW MM 32-10-21 AND PERFORMED ALTERNATE EXTENSION IAW MM 32-35-00.