LAX05LA286
2005-09-02 · Yuma, Arizona, United States · Fatal · 1 aircraft · Status: Completed
Airport YUM
Aircraft involved
Probable cause & findings
the pilot's failure to maintain an adequate airspeed on short final, which resulted in an inadvertent stall.
Factual narrative
On September 2, 2005, at 0830 mountain standard time, a Cessna 172 airplane, N5070A, was destroyed when it impacted the displaced threshold for runway 8 at the Yuma International Airport, Yuma, Arizona. The private pilot/owner of the airplane sustained serious injuries and the passenger was fatally injured. The pilot operated the airplane under the provisions of 14 CFR Part 91 as a personal flight. Visual meteorological conditions prevailed, and a flight plan was not filed for the local flight that departed Yuma around 0715. During a telephone interview with the pilot, he reported that the purpose of the flight was to photograph some private property of his that was for sale. The passenger was seated in the left seat to photograph the property and the pilot was flying from the right seat. They finished taking photographs of the property and were returning to the airport when the accident occurred. The airplane was on final approach and the pilot was conducting a full-flap landing. He reported that everything was fine, but the airplane began descending too fast. He applied some power to go-around, but the airplane encountered a gust of wind and stalled on short final. Witnesses informed the Federal Aviation Administrator inspector who responded to the accident site that they observed the airplane on short final. The nose pitched up to a level position about 50 feet above the ground and then nosed down until impact with the ground. Photographs taken of the accident site by airport operations personnel displayed tire marks on the displaced threshold followed by parallel gouges in the asphalt that were perpendicular to the airplane's direction of travel. The airplane came to rest upright about 80 yards from the initial impact point and erupted into flames. The center fuselage was burnt in its entirety and the wings were bent down and the tips were touching the ground. The floorboard behind the front seats was bent up and the aft fuselage and empennage were lying on the ground. At 0856, the weather observation facility at the Yuma International Airport reported the wind from 080 degrees at 7 knots. The airplane, which underwent its last annual inspection 22 hours prior to the accident (October 01, 2004), was not equipped with shoulder harnesses. The pilot reported having accumulated a total of 800 flight hours, of which 640 hours were accumulated in the accident airplane. The airplane stalled on short final and impacted the runway's displaced threshold in a nose low pitch attitude and erupted in flames. The pilot was flying the airplane from the right seat, with a passenger occupying the left seat in order to take some aerial photographs of nearby property. The airplane was on final approach and the pilot was conducting a full-flap landing. He reported that everything was fine, but the airplane began descending too fast. He applied some power to go-around, but the airplane encountered a gust of wind and stalled on short final. Witnesses at the airport observed the airplane on short final. The nose pitched up to a level position about 50 feet above the ground and then nosed down until impact with the ground. The weather observation facility at the airport was reporting the wind at 7 knots down the runway. The airplane was not equipped with shoulder harnesses. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_LAX05LA286.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- 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 …
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
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