ERA26LA021
2025-10-11 · Plymouth, Connecticut, United States · None · 1 aircraft · Status: Completed
Airport N41
Current FAA registration · N2812N
- Make / Model
- CESSNA 140
- Year of manufacture
- 1947 · 78 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19550725
- ADS-B equipped
- Yes — Mode-S A2D45D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The plot’s failure to account sufficiently for the decrease in the airplane’s takeoff performance due to the wet turf runway, which resulted in a collision with a log barrier and subsequent nose over after aborting the takeoff.
Factual narrative
The pilot was attempting a short field takeoff on a wet turf runway that was 2,005-ft-long. The pilot reported that during the takeoff roll, the tailwheel-equipped airplane would not climb into ground effect and felt as if the one of the wheels was on the ground. Recognizing that the airplane would not be able to accelerate in ground effect, the pilot attempted to abort the takeoff. As the airplane approached a log barrier at the departure end of the runway, the pilot attempted to ground loop the airplane, but the left main landing gear wheel slid on the wet grass. The airplane subsequently impacted the log barrier at low speed, nosed over and came to rest inverted. The airplane sustained substantial damage to the right wing strut, vertical stabilizer, and horizontal stabilizer. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. Based on the pilot’s description of the takeoff, it is likely that the wet runway condition reduced the airplane’s acceleration and resulted in the airplane not climbing into ground affect as otherwise expected during the takeoff from the relatively constrained turf runway. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
- — Environmental issues-Physical environment-Runway/land/takeoff/taxi surface-Wet surface-Decision related to condition
Verbatim from NTSB's published report. Source file
NTSB_2025_ERA26LA021.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type. All research papers
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- arXiv 2024 · arXiv preprint On the shape of ice stalagmites
The growth of ice stalagmites obtained by the solidification of impacting droplets on a cooled substrate ($-50^{\circ}$C to $-140^{\circ}$C) is investigated experimentally.
- NASA NTRS 2019 · Conference Paper Particulate Emissions Hazards Associated with Fueling Heat Engines
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- NASA NTRS 2016 · Conference Paper United Airlines LOFT training
Line oriented training is used in a broader, more generic sense that as a specific program under FAR 12.1409 and AC 120-35.
- Embry-Riddle Scholarly Commons 2016 · Conference paper Late Morning Concurrent Sessions: Innovations in Aviation Technologies: Presentation: Wingsuit Materials Research – The Effect of Currently Used Materials on Wingsuit Aerodynamics.
While wingsuit flight is exhilarating and one of the fastest growing facets of sport skydiving, current wingsuit performance is poor at best.
- NASA NTRS 2013 · Conference Paper Thermodynamic and fluid mechanic analysis of rapid pressurization in a dead-end tube
Three models have been applied to very rapid compression of oxygen in a dead-ended tube. Pressures as high as 41 MPa (6000 psi) leading to peak temperatures of 1400 K are predicted.