NTSB CAROL · Event
Event CHI01LA042
Registry · N713HM
FAA Aircraft Registry record.
Make / Model
SMITH AEROSTAR 601P
Year of manufacture
1977 · 23 years old at event
Engine
LYCOMING TI0-540 SER (310 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19770913
ADS-B equipped
Yes — Mode-S A987ED
Registrant of record
PINTO CARLOS
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
altitude/clearance from the trees not being obtained/maintained by the pilot. Factors to the accident were the trees and the contamination of the pitot/static system.
Factual narrative
On November 26, 2000, at 1000 central standard time, an Aerostar PA-60-601P, N713HM, owned and operated by a commercial pilot sustained substantial damage during an in-flight collision with trees during initial climb from runway 28 (4000 feet by 75 feet, ice-covered/asphalt) at the Fillmore County Airport, Preston, Minnesota. Instrument meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR Part 91 and was on an instrument flight rules (IFR) flight plan. The pilot and his sole passenger reported no injuries. The flight was originating at the time of the accident and the pilot performed a precautionary landing at the Quad City International Airport, Moline, Illinois, subsequent to the in-flight collision with the trees. According to the pilot's written statement, "I initiated the takeoff, on runway 28 accelerated to 100 MPH, rotated & lifted off. The gear and flaps were raised, and the aircraft stopped accelerating at about 112-115 MPH. I lowered the nose to pick up some speed, but it still wouldn't accelerate. I could see the trees approaching west of the airport & knew I didn't have climb speed, but also knew there was no choice but to pull up & hope I didn't stall." The pilot reported, "I pulled up sharply, but clipped the tops of the trees, the airspeed was still at 115 MPH IAS [Indicated Airspeed] with 12+ degrees nose up, and the airplane climbing rapidly. I then looked at the GPS [Global Positioning System] ground speed read out, and realized that it was at 140 KTS [Knots]. After assessing things, it became obvious that airspeed was not reading correctly." The pilot reported that he requested to divert from his IFR flight plan and land at the Quad City International Airport, Moline, Illinois, to determine the extent of damage to the airplane. The pilot stated, "During the trip to Moline, the airspeed indicator stayed at 115 MPH for about 15 minutes then pegged out at the back side of the "0" indication, and stayed there for a few minutes and came back to 160 KTS. My GPS was showing about 170 KTS at 7000 ft during the trip." The pilot reported, "I had a problem six weeks ago with a mud dauber wasp building a nest in the pitot tube, but this had been cleared out, and the aircraft flown several times since." During initial climb after takeoff, the pilot noticed that the airspeed indicator was not increasing past 112-115 mph. The pilot reported that he lowered the nose of the airplane to increase airspeed, but no response was noted on the airspeed indicator. The pilot stated that the airplane made contact with a tree line located at the end of the runway, causing substantial damage to the airplane. The pilot reported, "I pulled up sharply, but clipped the tops of the trees, the airspeed was still at 115 MPH IAS [Indicated Airspeed] with 12+ degrees nose up, and the airplane climbing rapidly. I then looked at the GPS [Global Positioning System] ground speed read out, and realized that it was at 140 KTS [Knots]. After assessing things, it became obvious that airspeed was not reading correctly." The pilot stated, "I had a problem six weeks ago with a mud dauber wasp building a nest in the pitot tube, but this had been cleared out, and the aircraft flown several times since." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_CHI01LA042.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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