- Date
- October 28, 2008, 11:05 local (17:05 UTC)
- Place
- Cedar Fort, UT
- Injuries
- 2 fatal
- Damage
- Destroyed
- Phase of flight
- Maneuvering
- Aircraft
- N78DSSilfvast Starduster TOO
- Defining event
- Maneuvering-aerobatics: Aerodynamic stall/spin
- Weather
- Visual (VMC) · Day
- Status
- Completed · report May 6, 2009
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- Federal Aviation Administration
- FAA report
- 20081028850789A
- Case key
- 69356
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The NTSB’s determination of the probable cause, and any contributing factors.
The pilot's failure to maintain an adequate airspeed and/or angle of attack to avoid a stall/spin during an aerobatic maneuver.
Findings · 3
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings.
Analysis
Multiple witnesses in the vicinity of the accident site reported observing the accident airplane performing a series of aerobatic maneuvers at a low altitude. The airplane was observed in what the witnesses described as a "flat spin" about 1,000 feet above ground level that continued until ground impact. One witness stated that he heard the engine running until the airplane impacted the ground. The airplane was consumed in a postimpact ground fire and all major components of the airplane were located at the accident site. No anomalies were noted with the airplane flight control system during an examination of the wreckage.
Factual narrative
On October 28, 2008, about 1105 mountain daylight time, an amateur built Silfvast Starduster Too experimental biplane, N78DS, was destroyed when it impacted terrain while performing aerobatic maneuvers near Cedar Fort, Utah. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91. The private pilot and his commercial pilot rated passenger were killed. Visual meteorological conditions prevailed and no flight plan was filed for the local personal flight. The flight originated from Salt Lake City Municipal 2 Airport, West Jordan, Utah at an unknown time. Multiple witnesses in the vicinity of the accident site reported observing the accident airplane performing a series of aerobatic maneuvers at a low altitude. The airplane was observed in a "flat spin" about 1,000 feet above ground level until impacting the ground where a post-impact fire ensued. One witness stated that he heard the engine running until the airplane impacted the ground. Examination of the airplane by a Federal Aviation Administration (FAA) inspector revealed that the airplane came to rest inverted within an open field and was consumed by fire. All major components of the airplane were located at the accident site. The primary flight controls of the airplane remained attached to their respective mounts. Control continuity was established from the cockpit controls to all primary flight controls. The Utah State Medical Examiner's office conducted an autopsy on the pilot on October 29, 2008. The medical examiner determined that the cause of death was "total body blunt force injuries." The FAA's Civil Aeromedical Institute (CAMI) in Oklahoma City, Oklahoma, performed toxicology tests on the pilot. According to CAMI's report, carbon monoxide, cyanide, volatiles, and drugs were tested, and had negative results except for an unspecified amount of Naproxen detected in the liver. The Utah State Medical Examiner's office conducted an autopsy on the pilot-rated passenger on October 29, 2008. The medical examiner determined that the cause of death was "total body blunt force injuries." The FAA's Civil Aeromedical Institute (CAMI) in Oklahoma City, Oklahoma, performed toxicology tests on the pilot-rated passenger. According to CAMI's report, carbon monoxide, cyanide, volatiles, and drugs were tested, and had negative results.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident.
Aircraft
- Registration
- N78DS
- Reported as
- Silfvast Starduster TOO
- Category
- Airplane, amateur-built
- Serial number
- DAS-1
- Airframe hours
- 272.18
- Engine
- Lycoming AEIO-360, 180 horsepower, reciprocating
- Damage
- Destroyed
- Flight
- Personal · Part 91
- Operator
- Silfvast David A
- Registered owner
- Silfvast David A
- Airworthiness certificate
- Special, Experimental (Special)
- Last inspection
- Continuous airworthiness · May 1, 2008
- Departed
- U42 · West Jordan, UT
- Flight plan
- Unknown
- Airport
- UT10 · Cedar Valley Airport
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew · 2
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 62
- Injuries
- Fatal
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 3, With waivers/limitations
- Last flight review
- October 27, 2008
- Toxicology
- Performed
- Flight hours
- 439 total · 3 in the last 90 days · 3 in the last 30 days · 1 in the last 24 hours
- Role
- Pilot
- Age
- 71
- Injuries
- Fatal
- Certificates
- Commercial, Airline transport
- Airplane ratings
- Single-engine land, Multi-engine sea, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, With waivers/limitations
- Toxicology
- Performed
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- Calm
- Visibility
- 15 statute miles
- Lowest ceiling
- None
- Temperature
- 52 °F, dew point 36 °F
- Altimeter
- 30.47 inHg
- Observed at
- PVU, 23 nm away
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.