ASN Wikibase Occurrence # 297991
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Saturday 23 June 2018 |
Time: | 13:08 LT |
Type: | Schempp-hirth STANDARD CIRRUS |
Owner/operator: | |
Registration: | N7880 |
MSN: | 80 |
Year of manufacture: | 1970 |
Total airframe hrs: | 1520 hours |
Fatalities: | Fatalities: / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Aguila, Arizona -
United States of America
|
Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
Nature: | Private |
Departure airport: | Aguila, AZ (28AZ) |
Destination airport: | Aguila, AZ (28AZ) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The glider pilot departed the airport via a tow winch for a local area flight. The tow winch driver reported that the takeoff and flight in the pattern were normal. When he observed the glider again, about 3 minutes later, it was crossing the approach end of the runway at an altitude of about 400 ft. The glider made a right 360° turn, abruptly pitched 60° nose-down and completed two spins. The glider came to rest inverted on the desert floor.
An examination of the glider revealed no mechanical malfunctions that would have precluded normal operations. Investigators established flight control continuity, and all breaks were attributed to impact forces. Given the glider's circling at low altitude, it is likely that the pilot encountered atmospheric lift (thermal) and was attempting to climb when he inadvertently exceeded the glider's critical angle of attack and entered an aerodynamic stall/spin. The glider's low altitude at the time of the spin entry would have precluded recovery.
Probable Cause: The pilot's exceedance of the glider's critical angle of attack while attempting a thermal climb at low altitude, which resulted in an aerodynamic stall/spin at an altitude that precluded recovery.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | WPR18FA178 |
Status: | Investigation completed |
Duration: | 2 years and 5 months |
Download report: | Final report |
|
Sources:
NTSB WPR18FA178
Location
Revision history:
Date/time | Contributor | Updates |
15-Oct-2022 11:31 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation