Greenville - Greenville
Flight / Schedule
Greenville - Greenville
Aircraft
Beechcraft 200 Super King AirRegistration
N337MT
MSN
BB-1628
Year of Manufacture
1998
Operator
MDTR HoldingsDate
November 9, 2009 at 10:09 AM
Type
CRASHFlight Type
Test
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Crash Location
Greenville-Spartanburg South Carolina
Region
North America • United States of America
Coordinates
34.8954°, -82.2172°
Crash Cause
Human factor
Narrative Report
On November 9, 2009 at 10:09 AM, Greenville - Greenville experienced a crash involving Beechcraft 200 Super King Air, operated by MDTR Holdings, with the event recorded near Greenville-Spartanburg South Carolina.
The flight was categorized as test and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.
3 people were known to be on board, 0 fatalities were recorded, 3 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.
Crew on board: 1, crew fatalities: 0, passengers on board: 2, passenger fatalities: 0, other fatalities: 0.
The listed crash cause is human factor. The pilot flew the airplane to a maintenance facility and turned it in for a phase inspection. The next morning, he arrived at the airport and planned a local flight to evaluate some avionics issues. He performed a preflight inspection and then went inside the maintenance facility to wait for two avionic technicians to arrive. In the meantime, two employees of the maintenance facility test ran the engines on the accident airplane for about 30 to 35 minutes in preparation for the phase inspection. The pilot reported that he was unaware that the engine run had been performed when he returned to the airplane for the local flight. He referred to the flight management system (FMS) fuel totalizer, and not the aircraft fuel gauges, when he returned to the airplane for the flight. He believed that the mechanics who ran the engines did not power up the FMS, which would have activated the fuel totalizer, thus creating a discrepancy between the totalizer and the airplane fuel gauges. The mechanics who performed the engine run reported that each tank contained 200 pounds of fuel at the conclusion of the engine run. The B200 Pilot’s Operating Handbook directed pilots not take off if the fuel quantity gauges indicate in the yellow arc or indicate less than 265 pounds of fuel in each main tank system. While on final approach, about 23 minutes into the flight, the right engine lost power, followed by the left. The pilot attempted to glide to the runway with the landing gear and flaps retracted, however the airplane crashed short of the runway. Only residual fuel was found in the main and auxiliary fuel tanks during the inspection of the wreckage. The tanks were not breached and there was no evidence of fuel leakage at the accident site.
Aircraft reference details include registration N337MT, MSN BB-1628, year of manufacture 1998.
Geospatial coordinates for this crash are approximately 34.8954°, -82.2172°.
Fatalities
Total
0
Crew
0
Passengers
0
Other
0
Crash Summary
The pilot flew the airplane to a maintenance facility and turned it in for a phase inspection. The next morning, he arrived at the airport and planned a local flight to evaluate some avionics issues. He performed a preflight inspection and then went inside the maintenance facility to wait for two avionic technicians to arrive. In the meantime, two employees of the maintenance facility test ran the engines on the accident airplane for about 30 to 35 minutes in preparation for the phase inspection. The pilot reported that he was unaware that the engine run had been performed when he returned to the airplane for the local flight. He referred to the flight management system (FMS) fuel totalizer, and not the aircraft fuel gauges, when he returned to the airplane for the flight. He believed that the mechanics who ran the engines did not power up the FMS, which would have activated the fuel totalizer, thus creating a discrepancy between the totalizer and the airplane fuel gauges. The mechanics who performed the engine run reported that each tank contained 200 pounds of fuel at the conclusion of the engine run. The B200 Pilot’s Operating Handbook directed pilots not take off if the fuel quantity gauges indicate in the yellow arc or indicate less than 265 pounds of fuel in each main tank system. While on final approach, about 23 minutes into the flight, the right engine lost power, followed by the left. The pilot attempted to glide to the runway with the landing gear and flaps retracted, however the airplane crashed short of the runway. Only residual fuel was found in the main and auxiliary fuel tanks during the inspection of the wreckage. The tanks were not breached and there was no evidence of fuel leakage at the accident site.
Cause: Human factor
Occupants & Outcome
Crew On Board
1
Passengers On Board
2
Estimated Survivors
3
Fatality Rate
0.0%
Known people on board: 3
Operational Details
Schedule / Flight
Greenville - Greenville
Operator
MDTR HoldingsFlight Type
Test
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Region / Country
North America • United States of America
