de Havilland DHC-6-100 near Sullivan, Missouri — 2006-07-29
- Date
- 2006-07-29
- Location
- Sullivan, Missouri, USA
- Aircraft
- de Havilland DHC-6-100
- Registration
- N203E
- Category
- Airplane
Probable cause
the pilot's failure to maintain airspeed following a loss of power in the right engine due to the fracturing of compressor turbine blades for undetermined reasons. Contributing to some parachutists' injuries was the lack of a more effective restraint system on the airplane.
Contributing factors
Contributing to some parachutists' injuries was the lack of a more effective restraint system on the airplane.
NTSB narrative
On a July day in 2006, a 1967 de Havilland DHC-6-100 Twin Otter departed Sullivan Regional Airport in Sullivan, Missouri, carrying a pilot and seven skydivers. The pilot performed an intersection takeoff from Runway 24, using only about 1,700 feet of available runway. Approximately three seconds after becoming airborne, a compressor blade failure in the right Pratt & Whitney PT6A engine produced a loud bang, with smoke and flame erupting from the nacelle. The pilot feathered the failed engine but lost aircraft control, allowing the Twin Otter to drift right and the airspeed to decay until the aircraft stalled and crashed just beyond the departure end of the runway. Five of the skydivers and the pilot were killed. Two skydivers survived, one with serious injuries. Conditions were day VFR and the aircraft was operating under Part 91 rules for parachute operations.
Evidence available
- Video
- Photos
- 50 docket documents
Docket documents50
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Mechanic's Statementinterview
- Record of Interviewinterview
- Record of Interviewinterview
- Record of Interviewinterview
- Record of Interviewinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Airplane Flight Manual Excerptsother
- Airplane Logbook Excerptsother
- Fuel Analysisother
- Letter From Pilot's Brotherother
- Letter Regarding Restraintsother
- Transportation Safety Board of Canada Submissionother
- Photo 1. Picture of Intersection Taxi for Takeoffphotos
- Photo 10. Bottom of Fuselagephotos
- Photo 11. Right Enginephotos
- Photo 12. Right Propeller and Reduction Gear Boxphotos
- Photo 13. Left Engine and Propellerphotos
- Photo 14. Instrument Panelphotos
- Photo 15. Light Bulb From Stall Warning Lightphotos
- Photo 16. Compressor Turbine From Right Enginephotos
- Photo 17. Right Propellerphotos
- Photo 18. Seat Belts for Skydiversphotos
- Photo 19. Accident Site (FAA Photo)photos
- Photo 2. Takeoffphotos
- Photo 20. Operator Supplied View of Cabin Interiorphotos
- Photo 21. View of Engine Controlsphotos
- Photo 22. View of Engine Controlsphotos
- Photo 3. Takeoffphotos
- Photo 4. Visible Flames Emitted From Right Enginephotos
- Photo 5. Climb Outphotos
- Photo 6. Accident Sitephotos
- Photo 7. Right Wingphotos
- Photo 8. Left Wingphotos
- Photo 9. Top of Fuselagephotos
- Video/Image Studyphotos
- Aircraft Manufacturer's Reportreport
- Errata 1 to Operations/Airworthiness Factual Reportreport
- Errata 2 to Operations/Airworthiness Factual Reportreport
- NTSB Report #NTSB-AAR-79-10report
- Operations/Airworthiness Factual Report with Erratareport
- Propeller Manufacturer's Reportreport
- Survival Factors Specialist's Factual Report - Attachment 1report
- Survival Factors Specialist's Factual Report - Attachment 3report
- Survival Factors Specialist's Factual Report - Errata 1report
- Survival Factors Specialist's Factual Report with Erratareport
- Toxicological Reportreport
- Transportation Safety Board of Canada Engineering Report on Compressor Turbine Bladesreport
- Plotted Wreckage Diagramwreckage