NTSB CAROL · Event
Event WPR14LA235
Aircraft involved
Probable cause & findings
The pilot’s improper landing flare in gusting wind conditions, his inadequate recovery from the subsequent bounced landing, and his decision to perform a go-around with insufficient airspeed to climb.
Factual narrative
On June 7, 2014, about 1731 mountain standard time, a Cessna 172N airplane, N5589E, was substantially damaged when it impacted a tree and terrain during an aborted landing at the Page Municipal Airport (KPGA), Page, Arizona. The airplane was being operated by American Aviation Inc., Page, as a visual flight rules (VFR), local area scenic flight, under the provisions of 14 Code of Federal Regulations Part 135. Visual meteorological conditions prevailed, the pilot and the two passengers were not injured. The flight departed Page about 1650. The airport's automated weather reporting station was reporting wind at 190 degrees true, at 13 knots with gusts to 23 knots. Due to the wind conditions, the pilot elected to use runway 25, a short cross runway that is 2,201 feet long and 75 feet wide for landing, as opposed to the main runway that is 5,950 feet long and 150 feet wide. In a written statement to the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) dated June 17, the pilot reported that he entered a 3 mile straight-in approach for runway 25. He approached the runway at 60 knots airspeed in gusting wind conditions, and that when he flared, the airplane started to drift toward the side of the runway. When the main landing gear touched down, a gust of wind lifted the airplane off the runway. He reported that he first touched down near runway 25's intersection with runway 15/33, which is about 700 feet from the threshold of runway 25. When the airplane touched down again, it bounced back into the air, this time too high to continue the landing, and the pilot initiated a go-around. He reported that the airplane engine was at full power, the airplane was in a level attitude, with the wings level, and the airspeed was indicating less than 43 knots. He did not raise the flaps or bank the airplane, for fear of the airplane sinking. The airplane started a slow descent, and he attempted to dodge houses and trees. With the stall warning horn sounding, the airplane struck a small tree, and then the ground. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. He reported that he thought the failure to climb was due to the local wind conditions. The airplane sustained substantial damage to the fuselage and wings. The pilot reported that, while landing the airplane in gusting wind conditions, he approached the runway at 60 knots and that, when he flared the airplane, it started to drift to the side of the runway. When the main landing gear touched down, a gust of wind lifted the airplane off the runway. The airplane touched down again and then bounced too high to continue the landing. The pilot subsequently initiated a go-around; the airplane was at full power with an airspeed of less than 43 knots. He did not raise the flaps because he was afraid the airplane would descend. The airplane started a slow descent, and the stall warning horn sounded. The airplane subsequently struck a small tree and then the ground, which resulted in substantial damage to the fuselage and wings. The wind at the airport was from 190 degrees at 13 knots gusting to 23 knots at the time of the accident. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Physical environment-Object/animal/substance-Tree(s)-Contributed to outcome
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- C Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Contributed to outcome - C
Verbatim from NTSB's published report. Source file
NTSB_2014_WPR14LA235.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
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