NTSB CAROL · Event
Event LAX00LA305
Aircraft involved
Probable cause & findings
The pilot's improper go-around procedure and his failure to maintain directional control on landing.
Factual narrative
On August 18, 2000, about 0913 hours mountain standard time, a Cessna 172, N2078E, was substantially damaged during landing at Flagstaff, Arizona. The private pilot was not injured. The airplane was operated under the provisions of 14 CFR Part 91 by Glendale Aviation, Glendale, Arizona, and rented by the pilot for a local area personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight originated at Glendale on the morning of the accident about 0700. According to the Flagstaff Control Tower, the pilot was landing on runway 21 when directional control was lost and the airplane veered off the left side of the runway colliding with a 5,000-foot remaining marker sign. The winds were reported as 220 degrees at 6 knots and the density altitude was 9,083 feet. The 80-hour private pilot reported that during the landing touchdown on runway 21, the airplane bounced and ballooned. He added power to soften the landing, but the airplane ballooned further. At that point, the pilot decided to perform a go-around. He applied full power and started climbing. The stall warning was going off, so he reduced the angle of attack. He removed the first notch of flaps, as directed by the balked landing procedure, and the airplane started settling back down quickly. He put the flaps back down, but the descent was not stopped. About the same time, the airplane was hit by a wind gust from the right, pushing the plane left. The pilot attempted to correct but was blown off the runway, colliding with a runway length remaining sign and subsequently, a ditch. He reported that he was number three to land on a long final with full flaps. He stated that there were no mechanical issues with the airplane. According to the Cessna Pilot Operating Handbook: NORMAL PROCEDURES-BALKED LANDING. 1) Throttle-FULL OPEN. 2) Carburetor Heat-COLD. 3) Wing Flaps-20 degrees (immediately). 4) Climb Speed-55 KIAS. 5) Wing Flaps-10 degrees (until obstacles are cleared) RETRACT (after reaching a safe altitude and 60 KIAS. The 80-hour private pilot was on a personal cross-country flight in a Cessna 172N. He was landing at a 7,000 feet msl airport with a density altitude of 9,083 feet. During the landing touchdown, the airplane bounced and ballooned. The pilot added power to soften the landing, but the airplane ballooned further. At that point he decided to perform a go-around. He applied full power and started climbing. The stall warning was going off, so he reduced the angle of attack. He removed the first notch of flaps 'as directed by the balked landing procedure,' and the airplane started settling back down quickly. He put the flaps back down, but the descent was not stopped. About the same time, the airplane was hit by a wind gust from the right, pushing the plane left. He attempted to correct but was blown off the runway colliding with a runway length remaining sign and subsequently, a ditch. The wind was 220 degrees at 6 knots. The pilot reported he was number three to land and was on a long final with full flaps. He stated that there were no mechanical issues with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_LAX00LA305.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 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
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.
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