NTSB CAROL · Event
Event GAA19CA026
Registry · N76154
FAA Aircraft Registry record.
Make / Model
CESSNA 140
Year of manufacture
1946 · 72 years old at event
Engine
CONT MOTOR C85 SERIES (85 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19560222
ADS-B equipped
Yes — Mode-S AA4863
Registrant of record
BAYOU FLIGHT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s inadvertent brake application, which resulted in a loss of directional control and a subsequent nose-over.
Factual narrative
The pilot of the tailwheel-equipped airplane reported that, during the preflight for a demonstration flight with a second pilot, they discussed the nose-over tendencies of the airplane and the necessity to "stay off the brakes." He added that, during the fourth touch and go landing, the second pilot was flying and performed a wheel landing. During the landing roll, the airplane drifted to the right and the pilot "came on the rudders to help." Suddenly, the airplane nosed over. The pilot reported that he believed he was responsible for the accident and that one of them must have inadvertently applied the brakes. He also believed he misjudged the second pilot's tailwheel experience. The second pilot reported that, at the time of the accident, he had a tailwheel endorsement and met the recency of experience requirements. He added that, during the landing roll, the airplane was tracking the centerline when "suddenly and unexpectedly", it nosed over. The airplane sustained substantial damage to the right wing lift strut and empennage. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot of the tailwheel-equipped airplane reported that, during the preflight for a demonstration flight with another pilot, they discussed the nose-over tendencies of the airplane and the need to "stay off the brakes." He added that, during the fourth touch-and-go landing, the second pilot was flying and performed a wheel landing. During the landing roll, the airplane drifted right, and the pilot "came on the rudders to help." Suddenly, the airplane nosed over. The pilot reported that he believed he was responsible for the accident and that either he or the other pilot must have inadvertently applied the brakes. He also believed that he misjudged the second pilot's tailwheel experience. The second pilot reported that, at the time of the accident, he had a tailwheel endorsement and met the recency of experience requirements. He added that, during the landing roll, the airplane was tracking the centerline when "suddenly and unexpectedly" it nosed over. The airplane sustained substantial damage to the right wing lift strut and empennage. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft systems-Landing gear system-Brake-Incorrect use/operation - C
- C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA19CA026.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 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
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- 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.
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- 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.
- Embry-Riddle Scholarly Commons 2003 · Journal article (JAAER)
A Safer Sky: An Examination of Factors Affecting Flight Safety in Taiwan
On April 26, 1994, China Airlines (CAL) Flight 140, service from Taipei, Taiwan to Nagoya, Japan, crashed near Nagoya International Airport while attempting an Instrument Landing System (ILS) approach…
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