N8137P is a 1991 Beech A36. It is a fixed-wing single-engine aircraft with 6 seats, powered by a Cont Motor IO-550 series rated at 300 horsepower. The registration is active, with the registrant based in Batavia, OH. Its standard airworthiness certificate was issued in Aug 1991. It has been registered to its current owner since Sep 2023. This page also carries 1 NTSB event.
- 35 years old
2023
1991
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N8137P's record changes.
On December 19, 2022, about 1505 central standard time, a Beech A36 airplane, N8137P, was substantially damaged when it was involved in an accident near Harrison, Arkansas. The pilot and passenger were not injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.
The pilot reported the airplane was topped off with fuel before departure. He reported that the flight was normal, and he switched fuel tanks when he reached the initial approach fix for the RNAV 18 approach at the Boone County Airport (HRO), Harrison, Arkansas. He stated that he canceled his instrument clearance as he had visual contact with the airport and the approach to the airport was normal until he was on short final, when the engine stopped producing power. The pilot stated he made one attempt to restore the engine power, which included switching fuel tanks. Unable to restore engine power, the pilot performed a forced landing to a field about one mile short of the runway. During the forced landing the airplane’s fuselage was substantially damaged and a postimpact fire ensued, consuming a majority of the fuselage.
The airplane was transported to a secure facility for further examination. The engine was examined, and it exhibited signs of exposure to the postimpact fire. All 12 spark plugs were removed, bench tested, and all operated normally. The rocker box covers and engine-driven fuel pump were removed. The propeller was rotated by hand and thumb compression, valvetrain continuity, and crankshaft continuity to the accessories were all established. The cylinders were inspected using a borescope and were unremarkable. Both magnetos were removed and operated using a powered drill. The ignition harness suffered thermal damage and could not be tested. The fuel flow divider was inspected and found unremarkable. All the fuel nozzles were clear of debris. The fuel-air mixture unit was examined. All arms remained connected to the unit and the throttle arm moved freely. The fuel screen was removed and clean of debris. All the metal propeller blades had chordwise scratches observed on the cambered side as well as nicks and gouges on the leading edges.
Due to the postimpact fire, the airplane’s fuel system could not be thoroughly examined.
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