What was found
DURING SERVICE CHECK, KEVLAR CABLE INT TAILCONE FRAYED AT CAM ATTACH POINT. R & R KEVLAR CABLE IAW AMM. KEVLAR CABLE TO TAILCONE RELEASE MECHANISM CAM WILL BE ACCOMPLISHED ON AMDS 5350-01077-0101.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SERVICE CHECK, KEVLAR CABLE INT TAILCONE FRAYED AT CAM ATTACH POINT. R & R KEVLAR CABLE IAW AMM. KEVLAR CABLE TO TAILCONE RELEASE MECHANISM CAM WILL BE ACCOMPLISHED ON AMDS 5350-01077-0101.