DOUGLAS DC3C near Kidron, OH — 2019-01-21
- Date
- 2019-01-21
- Location
- Kidron, OH, USA
- Airport
- OH22
- Aircraft
- DOUGLAS DC3C
- Registration
- N467KS
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Takeoff roll
Probable cause
The loss of airplane control after an engine flameout and auto-feather system interruption during the takeoff climb, which resulted in an impact with terrain.
NTSB narrative
The two pilots departed in a turbine powered DC-3C at maximum gross weight for a repositioning flight. The airplane was part of a test program for new, higher horsepower engine installation. Soon after liftoff and about 3 seconds after decision speed (V1), the left engine lost total power. The propeller began to auto-feather but stopped feathering about 3 seconds after the power loss. The airplane yawed and banked to the left, descended, and impacted terrain. Recorded engine data indicated the power loss was due to an engine flameout; however, examination of the engine did not determine a reason for the flameout or the auto-feather system interruption. While it is plausible that an air pocket developed in the fuel system during the refueling just before the flight, this scenario was not able to be tested or confirmed. It is possible that the auto-feather system interruption would have occurred if the left power lever was manually retarded during the auto-feather sequence. The power loss and auto-feather system interruption occurred during a critical, time-sensitive phase of flight since the airplane was at low altitude and below minimum controllable airspeed (Vmc). The acutely transitional phase of flight would have challenged the pilots' ability to manually feather the propeller quickly and accurately. The time available for the crew to respond to the unexpected event was likely less than needed to recognize the problem and take this necessary action – even as an immediate action checklist/memory item.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Captain could have performed auto-feather tests before takeoff.
NTSB coding
Evidence available
- CVR
- Photos
- 13 docket documents
Docket documents13
- Cockpit Voice Recorder Factual Report and Transcriptcvr
- Statement of Party Representatives to NTSB Investigationinterview
- Correspondence with FAA Test Pilotother
- Excerpts of Flight Manualother
- Fuel Boost Pumps Examinationother
- Fuel Filters Examinationother
- Photos of Accident Sitephotos
- Photos of Takeoff Sequencephotos
- Engine Data Monitor Factual Reportreport
- Engine Data Monitor Factual Report - Attachment 1 - Tabular Datareport
- Propeller Governor - Examinatinon and Testing Reportreport
- Toxicological Report - Captainreport
- Toxicology Report - First Officerreport
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