What was found
THE AFT FUSELAGE TAIL CONE EXTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE AFT FUSELAGE TAIL CONE EXTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-00.