NTSB CAROL · Event
Event SEA82DA018
Aircraft involved
Factual narrative
AFTER AN ANNUAL INSPECTION, THE PILOT MADE A THOROUGH GROUND CHECK AND TAXIED OUT FOR A TEST FLIGHT. DURING TAKEOFF, THE ENGINE LOST POWER AT ABOUT 50 FT AGL. THE PILOT LANDED ON THE RUNWAY OVERRUN IN ABOUT 9 INCHES OF CRUSTED SNOW AND THE PLANE NOSED OVER. NO PROBLEMS WERE FOUND WITH THE ENGINE, FUEL, OR FUEL SYSTEM. THE ENGINE WAS OPERATED AT TAKEOFF POWER FOR 2 MINUTES USING BOTH THE LEFT AND RIGHT TANKS WITH NO DISCREPANCIES. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1982_SEA82DA018.txt.
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Related research
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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
All hydrocarbon- (HC-) fueled heat engine exhaust (tailpipe) emissions (<10 to 140 nm) contribute as health hazards, including emissions from transportation vehicles (e.g., aircraft) and other HC-fuel…
- 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.
- 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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