A FORCED LANDING WAS MADE ON A ROAD AFTER THE PLT SHUT DOWN THE ENG DUE TO A 'RUN-AWAY' PROP. DURING THE LANDING ROLL, THE LEFT WING TIP STRUCK A REFLECTOR POST FOLLOWED BY THE RIGHT WING STRIKING A SIGN POST. AN ENG OVERHAUL & AN ANNUAL INSPECTION HAD BEEN COMPLETED 20 DAYS PRIOR TO THE ACCIDENT.DURING AN EXAM AFTER THE ACCIDENT, NO OIL WAS FOUND IN THE ENG AND THE OIL DRAIN PLUG WAS MISSING.…
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series…
Dec 8, 1998
Airframe (PA-28R-200)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies.