SEA97LA055
1997-02-01 · BANDON, Oregon, United States · None · 1 aircraft · Status: Completed
Airport S05
Current FAA registration · N11099
- Make / Model
- CHAMPION 7ECA
- Year of manufacture
- 1965 · 32 years old at event
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19650215
- ADS-B equipped
- Yes — Mode-S A02FE8
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the dual student's failure to maintain directional control of the airplane, and the flight instructor's improper remedial action. A factor relating to the accident was: the ravine located near the right side of the runway.
Factual narrative
On February 1, 1997, about 1635 Pacific standard time, a Champion 7ECA, N11099, was substantially damaged in a collision with a ravine following a loss of control during a high-speed taxi at Bandon State Airport, Bandon, Oregon. The accident occurred during an instructional event for a tailwheel aircraft checkout. The commercial pilot-in-command, who was a certificated flight instructor (CFI), and the student, a private pilot, were not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the 14 CFR 91 flight. The instructor reported: I was giving taxi instruction to [the pilot-rated student] and upon slowing from a high speed taxi the aircraft began to depart runway 34 to the left. I took control with full rudder, full power and a lot of [right] aileron[,] enough in fact to drag the [right] wing on the runway. This turned the plane to the right about 45 [degrees;] I didn't have enough rudder authority to get the plane straight or headed down the runway before coming to a ravine on the east side of the runway[.] The aircraft impacted the east slope of the ravine, which runs parallel to the runway to the right of the departure end of runway 34. The instructor reported that no mechanical malfunction or failure was involved in the accident. He reported winds at the time as being from 180 degrees magnetic at 3 knots. The flight was an instructional flight for a checkout in a tailwheel equipped aircraft, with a private pilot-rated student in the front seat and a certificated flight instructor (CFI) in the rear seat. The CFI stated that while he was giving the front-seat student taxi instruction, the airplane departed the runway to the left, as they were slowing from a high-speed taxi. The CFI stated that he took control at this point with enough control input (rudder, power, and aileron) to drag the right wing on the runway. The airplane turned about 45 degrees to the right and departed the right side of the runway. Subsequently, it impacted in a ravine which ran parallel to the right side of the departure end of the runway. No preimpact mechanical malfunction was reported. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_SEA97LA055.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (loss of control). All research papers
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- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
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- Semantic Scholar 2021 · Article (Aviation) ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
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