Probable cause
An aerodynamic stall/spin and loss of control for reasons that could not be determined based on the available information.
NTSB analysis
The student pilot was departing in the motorglider when the accident occurred. A witness stated that the glider used about 3/4 of the 2,580-ft-long runway to become airborne. As the glider climbed, it entered an aerodynamic stall and spin, and subsequently impacted terrain. Security camera footage showed the glider impact the ground in a near-vertical, nose-low attitude in a counterclockwise spin. The glider sustained substantial damage to the right wing and fuselage.
An examination of the glider did not reveal any anomalies that would have precluded normal operations. The glider’s maintenance history could not be determined. The glider had been deregistered about 8 years before the accident. The student pilot’s logbook was not located, and neither his total flight experience nor experience in the accident glider could be determined.
Although the circumstances of the accident are consistent with an aerodynamic stall/spin and loss of control, the reason for the loss of control could not be determined based on the available information.
Text from the NTSB. Open the NTSB docket for CEN21LA396 for the full record.
Event
- Date
- Sep 6, 2021
- Type
- Accident
- Place
- Tulsa, Oklahoma
- Nearest airport
- Harvey Young (1H6)
- Highest injury
- Fatal
- Fatal injuries
- 1
- Weather
- Visual (VMC)
- Light
- Day
Amateur-built MONI
- N-number
- N983JV
- Category
- Glider
- Year built
- 1986
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.