What was found
THE TAIL CONE DROP TEST USING EXTERIOR RELEASE HANDLE WAS BELOW 25 MINIMUM PULL. THE TAIL CONE RELEASE SYSTEM WAS ADJUSTED IAW MM 53-53-00. THE TAIL CONE RELEASE CABLE PIN SHAFT WAS REPLACED DUE TO SHARP INDENTATIONS FOUND.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE TAIL CONE DROP TEST USING EXTERIOR RELEASE HANDLE WAS BELOW 25 MINIMUM PULL. THE TAIL CONE RELEASE SYSTEM WAS ADJUSTED IAW MM 53-53-00. THE TAIL CONE RELEASE CABLE PIN SHAFT WAS REPLACED DUE TO SHARP INDENTATIONS FOUND.