NTSB CAROL · Event
Event CHI93LA258
Registry · N9810M
FAA Aircraft Registry record.
Make / Model
MAULE M-4-210C
Year of manufacture
1966 · 27 years old at event
Engine
CONT MOTOR IO-360 SER (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19660722
ADS-B equipped
Yes — Mode-S ADB13F
Registrant of record
PAKUER LEVI R
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's improper recovery from a bounced landing.
Factual narrative
On July 15, 1993, about 2045 central daylight time, a Maule M4 airplane, N9810M, sustained substantial damage while landing at Tomahawk Airport, Tomahawk, Wisconsin. The solo private pilot was not injured. The local pleasure flight operated without flight plan in visual meteorological conditions under 14 CFR Part 91. The pilot reported he landed hard and bounced three or four times. He applied power and attempted to go around for another landing. During the attempted go around the airplane struck trees, and the pilot elected to make an emergency landing in an adjacent field. THE PILOT REPORTED HE LANDED THE AIRPLANE HARD AND IT BOUNCED. HE ELECTED TO ABORT THE LANDING AND ATTEMPTED TO TAKEOFF. THE AIRPLANE SUBSEQUENTLY STRUCK TREE TOPS BEYOND THE END OF THE RUNWAY, AND THE PILOT MADE A HARD, EMERGENCY LANDING IN A FIELD. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_CHI93LA258.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2025 · arXiv preprint
NMPC-based Unified Posture Manipulation and Thrust Vectoring for Fault Recovery
Multi-rotors face significant risks, as actuator failures at high altitudes can easily result in a crash and the robot's destruction.
- NASA NTRS 2019 · Technical Memorandum (TM)
Threshold Assessment of Gear Diagnostic Tools on Flight and Test Rig Data
A method for defining thresholds for vibration-based algorithms that provides the minimum number of false alarms while maintaining sensitivity to gear damage was developed.
- NASA NTRS 2019 · Technical Memorandum (TM)
Investigation of Spiral Bevel Gear Condition Indicator Validation via AC-29-2C Combining Test Rig Damage Progression Data with Fielded Rotorcraft Data
This is the final of three reports published on the results of this project. In the first report, results were presented on nineteen tests performed in the NASA Glenn Spiral Bevel Gear Fatigue Test Ri…
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
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