20070406005599A

Accident · Substantial damage

FAA accident report · Beech D50E · Elk Mont, AL · April 6, 2007

Date
April 6, 2007 · 15:40 local
Place
Elk Mont, AL
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N107WB
NTSB investigation
NTSBATL07CA068
Reported as
Beech D50E
Reported engine
Lycoming GO480*
People aboard
4
Fatal injuries
0
Pilot’s flight hours
7,336 total227 in this make and model5 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) The pilot stated that one half hour into the flight from augusta, ga to memphis, TN, he switched the fuel selector valve from the main tanks to the auxiliary tanks on both engines. One hour later the right engine ran out of gas and quit. He switched both fuel selector valves back to the main tanks and turned on the electric boost pumps. He immediately asked ATC for al heading to the nearest airport, then the left engine quit. He attempted to start both engines, but they failed to start. He feathered both props, and with landing gear retracted he landed the airplane in an open field. The airplane was substantially damaged during wheels up landing. There were four passengers on board the airplane and they received no injuries. The on scene investigation revealed that during impact, the right propeller separated from the engine and the right engine and wing flight controls were substantially damaged. The right inboard fuel tank was empty but the other three tanks were full. There was no visible sign or smell of fuel leakage. The landing gears were damaged, the fuselage and belly of the airplane was substantially damaged but there was no damage to left side of the airplane.

As the FAA filed it

(-23) THE PILOT STATED THAT ONE HALF HOUR INTO THE FLIGHT FROM AUGUSTA, GA TO MEMPHIS, TN, HE SWITCHED THE FUEL SELECTOR VALVE FROM THE MAIN TANKS TO THE AUXILIARY TANKS ON BOTH ENGINES. ONE HOUR LATER THE RIGHT ENGINE RAN OUT OF GAS AND QUIT. HE SWITCHED BOTH FUEL SELECTOR VALVES BACK TO THE MAIN TANKS AND TURNED ON THE ELECTRIC BOOST PUMPS. HE IMMEDIATELY ASKED ATC FOR AL HEADING TO THE NEAREST AIRPORT, THEN THE LEFT ENGINE QUIT. HE ATTEMPTED TO START BOTH ENGINES, BUT THEY FAILED TO START. HE FEATHERED BOTH PROPS, AND WITH LANDING GEAR RETRACTED HE LANDED THE AIRPLANE IN AN OPEN FIELD. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED DURING WHEELS UP LANDING. THERE WERE FOUR PASSENGERS ON BOARD THE AIRPLANE AND THEY RECEIVED NO INJURIES. THE ON SCENE INVESTIGATION REVEALED THAT DURING IMPACT, THE RIGHT PROPELLER SEPARATED FROM THE ENGINE AND THE RIGHT ENGINE AND WING FLIGHT CONTROLS WERE SUBSTANTIALLY DAMAGED. THE RIGHT INBOARD FUEL TANK WAS EMPTY BUT THE OTHER THREE TANKS WERE FULL. THERE WAS NO VISIBLE SIGN OR SMELL OF FUEL LEAKAGE. THE LANDING GEARS WERE DAMAGED, THE FUSELAGE AND BELLY OF THE AIRPLANE WAS SUBSTANTIALLY DAMAGED BUT THERE WAS NO DAMAGE TO LEFT SIDE OF THE AIRPLANE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.