DEN02LA042
2002-05-11 · Monument Valley, Utah, United States · None · 1 aircraft · Status: Completed
Airport UT25
N345M has since been reassigned. It is now registered to a different aircraft (PIPISTREL DOO AJDOVSCINA VIRUS SW, built 2014), which was not involved in this event.
Aircraft involved
Probable cause & findings
the pilot's inadvertent stall/mush to the ground during landing flare. Contributing factors were the earth berm along the side of the runway, and the wind shear weather condition on short final.
Factual narrative
On May 11, 2002, at approximately 1220 mountain daylight time, a Piper PA-28-140B, N345M, was substantially damaged following impact with terrain subsequent to an inadvertent stall/mush at Monument Valley Airport, Monument Valley, Utah. The private pilot and his passenger were not injured. The pilot was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cross-country flight that originated from Chandler Municipal Airport, Chandler, Arizona, at 1013. The pilot had not filed a flight plan. The pilot said that he researched the airport before his flight. He was aware of the normal procedures regarding carrying more airspeed and placing the aircraft "firmly" on the runway. He arrived at the destination 2-3 hours after the planned arrival time. At approximately 50 feet above ground level, the airplane experienced a significant loss in air speed due to a "sudden wind shift/shear." The aircraft was moved approximately 50 feet to the right and impacted an earth berm. The nose wheel landing gear collapsed aft, and the engine mount, engine firewall, cowling and fuselage were bent. The pilot said that he arrived at his destination 2-3 hours after the planned arrival time. At approximately 50 feet above ground level the airplane experienced a significant loss in air speed due to a "sudden wind shift/shear." The aircraft was moved approximately 50 feet to the right and impacted an earth berm. The nose wheel landing gear collapsed aft, and the engine mount, engine firewall, cowling and fuselage were bent. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_DEN02LA042.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 ↗
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Related research
Matched on aircraft type or causal vocabulary (wind shear, stall). All research papers
- NASA NTRS 2019 · Conference Paper Optimal recovery from microburst wind shear
The flight path of a twin-jet transport aircraft is optimized in a microburst encounter during approach to landing. The objective is to execute an escape maneuver that maintains safe ground clearance …
- NASA NTRS 2013 · Conference Paper Optimal nonlinear estimation for aircraft flight control in wind shear
The most recent results in an ongoing research effort at Princeton in the area of flight dynamics in wind shear are described.
- 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 …
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