FTW97LA179
1997-05-06 · GRANTS, New Mexico, United States · Serious · 1 aircraft · Status: Completed
Airport GNT
Current FAA registration · N2915V
- Make / Model
- CALLAIR A-2
- Engine
- LYCOMING 0-290 SERIES (140 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19551104
- ADS-B equipped
- Yes — Mode-S A2FC4C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Inadvertent stall. Factors were the ground depression, the high density altitude, and a lack of recent experience in the make and model of aircraft.
Factual narrative
On May 6, 1997, at 1035 mountain daylight time, a Callair A2A, N2915V, owned by a private individual and flown by a private pilot under Title 14 CFR Part 91, impacted the terrain following a loss of lift during takeoff near Grants, New Mexico. The private pilot received serious injuries and the sole passenger received minor injuries, and the airplane substantial damage. Visual meteorological conditions prevailed for the planned cross country flight and a flight plan was not filed. The flight was originating at the time of the accident. Telephone interviews, conducted by the investigator-in-charge (IIC), revealed that the pilot "felt a loss of lift during the climb toward rising terrain and the airplane stalled as he pulled the nose up." The airplane descended uncontrolled into a terrain depression. Local authorities and the airport manager reported that a natural terrain depression (30 feet across and 50 feet deep) located approximately 1/2 mile beyond the end of runway 31 was known by the local pilots as a "loss of lift, sink hole area." With an airport elevation of 6,521 feet and a temperature of 62 degrees Fahrenheit, the IIC calculated the density altitude at 8,200 feet. Structural damage occurred to the fuselage and the wings. The pilot reported 22 hours total time in the make and model of airplane. He reported 30 hours of flight time in the previous 90 days (none in the Callair). During the takeoff initial climb, the pilot 'felt a loss of lift during the climb toward rising terrain and the airplane stalled as he pulled the nose up.' The airplane descended uncontrolled into a terrain depression (30 feet across and 50 feet deep) located approximately 1/2 mile beyond the end of the runway. With an airport elevation of 6,521 feet and a temperature of 62 degrees Fahrenheit, the density altitude was calculated at 8,200 feet. The pilot reported 22 hours total time in the make and model of airplane with no flight time in the previous 90 days in this airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW97LA179.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
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Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
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- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…