No fatalities

18 Oct 2019: Beech N35 NO SERIES (N35) — Madisonville, TN

Madisonville, TN, United States

On 18 Oct 2019, a Beech N35 NO SERIES (registration N35) was involved in an aviation accident near Madisonville, TN. No fatalities were reported. Investigators recorded the probable cause as: The pilot's unstable approach and delayed decision to go-around. Contributing to the accident was the unporting of the fuel supply following a forward slip maneuver during the approach, which resulted in the loss of engine power during the go-around. This summary draws on records from NTSB; 10 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On October 18, 2019, a Beech N35 (N564T) impacted terrain during a go-around at Monroe County Airport, Tennessee. The pilot was uninjured; the wings sustained substantial damage.

Accident

On October 18, 2019, about 1530 eastern daylight time, a Beech N35 airplane, N564T, impacted terrain and trees during a go-around at Monroe County Airport (MNV) in Madisonville, Tennessee. The private pilot, operating the airplane as a Title 14 Code of Federal Regulations Part 91 personal flight, was not injured.

Flight Sequence

The pilot reported that during the approach to MNV he decided to perform a training exercise by simulating an engine failure during landing. He entered the traffic pattern for runway 5 and reduced power to idle. While on final approach, he noted the airplane was "a little fast and a little high" and performed a forward slip to the left (left rudder application) for a "second or two." He continued the approach, and the airplane touched down with about 1,000 feet of the 3,643-foot runway remaining and immediately bounced back into the air.

The pilot decided to perform a go-around and applied power; however, the engine did not respond. The airplane flew beyond the departure end of the runway, touched down in grass, and skidded into shrubs and trees. The left and right wings sustained substantial damage.

Postaccident Examination

Postaccident, the pilot reported that he believed the slip maneuver "unported fuel from the right tank [selected tank for approach] and prevented the plane from throttling up." He stated there were no mechanical malfunctions or failures with the airplane.

Examination of the airplane by a Federal Aviation Administration inspector found no preimpact mechanical malfunctions or failures that would have precluded normal operation. There were no obstructions or debris found in the fuel system, and the engine produced normal power when test-run. Inspection revealed 17 gallons of fuel in the right tank and 22 gallons in the left tank.

Aircraft Information

The airplane flight manual stated in part:

FUEL CELLS Fuel supply is carried in two bladder-type cells with a total capacity of [40 gallons, optional fuel system installed], located in the wings just outboard of the fuselage. Fuel is fed from the cells to a selector valve just forward of the front seat, on the left side, then through a strainer to the fuel pump and the engine. The fuel tank fillers are located in the wing leading edges.

Maximum Slip Duration: 30 seconds for airplanes with baffled main fuel cells in both wings.

Contributing factors

Causes

Descent/approach/glide path — Not attained/maintainedPilotAirspeed — Not attained/maintained

Other contributing factors

Fluid level