NTSB CAROL · Event
Event LAX96LA235
Registry · N6261D
FAA Aircraft Registry record.
Make / Model
CESSNA 172N
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19790424
ADS-B equipped
Yes — Mode-S A82F06
Registrant of record
N6261D LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to initiate a landing flare, which resulted in a bounced landing and porpoise, and his loss of directional control during an attempt to initiate a go-around with insufficient airspeed, which resulted in an inadvertent stall/mush and collision with parked aircraft. A visual illusion created by the runway gradient was a factor in this accident.
Factual narrative
On June 16, 1996, at 1502 hours Pacific daylight time, a Cessna 172N, N6261D, collided with three parked aircraft after a hard landing at Catalina airport, Avalon, California. The aircraft sustained substantial damage; however, neither the private pilot nor his three passengers were injured. The aircraft was being operated as a personal flight by Pars Air when the accident occurred. The flight originated in Santa Ana, California, about 1430 on the day of the accident. Visual meteorological conditions prevailed at the time and no flight plan had been filed. The airport manager reported that he first observed the aircraft in the traffic pattern on approach to runway 22. During the landing sequence the aircraft failed to flare and touched down on the nose wheel. The aircraft porpoised twice and on the second bounce, the pilot attempted to recover. The aircraft veered off the runway and stalled about 25 to 30 feet in the air, hit the ground, and subsequently struck three other parked aircraft. The pilot reported that he was making a normal approach with 40 degrees of flaps. On touchdown he bounced once and then bounced a second time, when the aircraft struck a hole in the runway. The nosewheel began to shake severely and he applied back pressure on the control wheel but thought at this time he was nearing the end of the runway. He intentionally turned left to avoid running off what he thought was the departure end. A second witness, who was a coworker of the airport manager, reported that he heard the engine accelerate during the accident sequence. He also stated that, although there was some spalling of the runway surface, there were no holes in the runway at the time of the accident. According to the NOAA Airport/Facility Directory, pilots cannot see aircraft on opposite ends of the runway due to the runway gradient. The other aircraft involved were identified as: a Beech G18S, N9375Y; a Grumman AA-5, N5439L; and another Cessna 172N, N6441D. A postaccident inspection of the aircraft revealed that the flaps were still extended to 40 degrees and the aircraft was trimmed nose down. Ground witnesses stated that the pilot did not flare and the aircraft touched down hard on the nose wheel and porpoised twice. On the second bounce the aircraft veered off the runway and toward a line of parked aircraft. The pilot attempted to recover by adding power; however, the aircraft stalled, impacted the ground, and collided with three parked aircraft. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_LAX96LA235.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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