DEN02LA079
2002-07-18 · Grants, New Mexico, United States · None · 1 aircraft · Status: Completed
Airport GNT
Aircraft involved
Probable cause & findings
the pilot's inadequate preflight preparation, and his failure to maintain airspeed which resulted in an inadvertent stall. Contributing factors were the high density altitude conditions, the terrain barrier (berm).
Factual narrative
On July 18, 2002, at approximately 1345 mountain daylight time, a Cessna 150F, N8067S, was substantially damaged when it struck terrain while attempting to return to the airport immediately after takeoff from Grants-Milan Municipal Airport, Grants, New Mexico. The private pilot, the sole occupant on board, was not injured. The pilot was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the personal cross-country flight which was originating at the time of the accident. The pilot had not filed a flight plan; he said his next planned stop was Moriarty, New Mexico. The pilot stated that he climbed approximately 350 feet and made one circle to climb to altitude. The airplane was having difficulty climbing. As he executed a shallow turn back toward the airport, the airplane had difficulty maintaining altitude. He was considering an off-field landing, but realized there was a soil berm in his flight path. The pilot "eased" the control column back to clear the berm, and the airplane stalled. The airplane then struck the ground, bending both wing tips up, and bending both the engine mount and firewall. The density altitude was calculated to be 9,322 feet. The airplane's POH (Pilot's Operating Handbook) states that the service ceiling of this aircraft was 12,650 feet. The pilot stated that he climbed approximately 350 feet and made one circle to climb to altitude. The airplane was having difficulty climbing. As he executed a shallow turn back toward the airport, the pilot had difficulty maintaining altitude. He was considering an off-field landing, but realized there was a soil berm in his flight path. The pilot "eased" the control column back to clear the berm, and the airplane stalled. The airplane then struck the ground, bending both wing tips up, and bending both the engine mount and firewall. The density altitude was calculated to be 9,322 feet. The service ceiling of the airplane was12,650 feet. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_DEN02LA079.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
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
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
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
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…