NTSB CAROL · Event
Event LAX02LA046
Registry · N7844W
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-180
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19640925
ADS-B equipped
Yes — Mode-S AAA25B
Registrant of record
SADDY ROCK
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control following his misjudged landing flare and hard touchdown.
Factual narrative
On December 11, 2001, about 1240 hours Pacific standard time, a Piper PA-28-180, N7844W, collided with a runway light and impacted a sign during landing rollout at the Brackett Field, La Verne, California. The airplane was substantially damaged, and the private pilot, who owned the airplane, was not injured. Visual meteorological conditions prevailed at the time, and no flight plan was filed. The airplane was being operated on a personal flight under 14 CFR Part 91. The flight originated from Chino, California, about 1212. The pilot reported that he entered the traffic pattern for landing on runway 26L and everything was normal. The airplane's airspeed was 85 miles per hour, and 25 degrees of flaps were extended. On short final approach he was lined up with the runway. During the landing flare, about 2 feet above ground level, the airplane veered left of centerline. The pilot further indicated that as he started to correct the airplane's left yaw, the airplane "slammed to the ground." Then, the airplane veered off the left side of the runway and collided with runway lights. The pilot also reported that no mechanical malfunction or failure precipitated the accident. The airport manager reported that, based upon his observations of the marks on the runway, the airplane touched down while yawed to the left, about 1/3 of the way down the runway. Skid marks, corresponding to the airplane's three tires, were noted leading off the left side of the runway. The airplane came to rest about 100 feet left of the runway's edge. At 1247 the airport reported its weather was, in part, 20 miles visibility, and few clouds at 9,000 feet. The wind was from 230 degrees at 7 knots. No gusts were reported. The pilot entered the traffic pattern for landing on runway 26L and everything was normal. On short final approach the airplane was initially aligned with the runway centerline, the airspeed was 85 miles per hour, and the wing flaps were at the 25-degree extended position. During the landing flare, about 2 feet above ground level, the airplane yawed left. As the pilot attempted to regain directional control, the airplane stalled and touched down hard. Thereafter, it veered off the left side of the runway and collided with lights before coming to a stop about 100 feet left of the runway's edge. About the time of the mishap, a 30-degree, 7-knot crosswind existed. No gusts were reported. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_LAX02LA046.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). 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 …
- 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…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗