NTSB CAROL · Event
Event CHI00LA255
Registry · N10QB
FAA Aircraft Registry record.
Make / Model
PIPER PA-31-325
Year of manufacture
1978 · 22 years old at event
Engine
LYCOMING TI0-540 SER (310 hp)
Seats / Engines
8 seats · 2 engines
ADS-B equipped
Yes — Mode-S A003BB
Registrant of record
ASC AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the landing gear not deployed, the checklist not followed, the lack of familiarity with the airplane, the landing gear warning system not understood, and the landing gear warning disregarded by the pilot.
Factual narrative
On August 10, 2000, at 1820 central daylight time, a Piper PA-31-325, N10QB, piloted by a commercial pilot, sustained substantial damage during a gear-up landing at the Millard Airport (MLE), Omaha, Nebraska. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 business flight was operating on an instrument flight rules (IFR) flight plan. The pilot and three passengers reported no injuries. The flight departed from the Creighton Municipal Airport, Creighton, Nebraska, at 1715 en route to MLE. The pilot reported, "...I did have visual contact with the landing aircraft and judged that it would clear the runway at the time of my landing. At this time I thought I reached down to push the landing gear lever down. I also dropped a checklist from my lap and reached down to retrieve it. Moving my head back up, I thought I saw the red gear-in-transit light go out and the three gear lights illuminate. I did not look at the gear lights again as I immediately heard the traffic from the West announce they had me in sight. I resumed trying to make visual contact with the traffic downwind to ensure they would not turn base in front of me. I also noted I was still slightly fast at about 130 KIAS. I reduced my power to 20 inches, threw in full flaps, because I was slightly high and fast, and went back to my checklist laying on my lap. I double checked that the emergency pumps were on and that we were on the inboard tanks. I noted traffic still on the runway and, while on short final, thought about going around, but then the Cherokee cleared the runway and I deemed it safe to land. As we cleared the fence, the speed was about 90, slightly high, and I brought power all the way back. A warning horn sounded which I deemed to be the stall warning and I proceeded to flare. The warning horn continued and I saw the speed to be about 82 KIAS. I knew that on N932LA, the Navajo Chieftain on which I had most of my Navajo time, the stall warning went off prematurely, and I thought the same case was true here..." Postaccident testing of the landing gear, under the supervision of the Federal Aviation Administration, revealed no anomalies. The airplane received substantial damage during a gear-up landing. The pilot stated that during landing a warning horn sounded which he thought was the stall warning; the pilot continued the landing. Postaccident testing of the landing gear revealed no anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_CHI00LA255.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…
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