What was found
DURING PERFORMANCE OF AMDS WC 2562-7267, TAILCONE DID NOT JETTISON. FOUND THE AFT FUSELAGE CONTROL ARM ASSY BINDING. PERFORMED ADJUSTMENT OF ARM ASSY IAW AMM 53-53-02-201. TAILCONE JETTISONED PROPERLY IAW AMDS WC 2562-7267.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING PERFORMANCE OF AMDS WC 2562-7267, TAILCONE DID NOT JETTISON. FOUND THE AFT FUSELAGE CONTROL ARM ASSY BINDING. PERFORMED ADJUSTMENT OF ARM ASSY IAW AMM 53-53-02-201. TAILCONE JETTISONED PROPERLY IAW AMDS WC 2562-7267.