NTSB CAROL · Event
Event SEA02LA038
Registry · N62658
FAA Aircraft Registry record.
Make / Model
BOEING A75N1(PT17)
Year of manufacture
1942 · 60 years old at event
Engine
CONT MOTOR W670 SERIES (250 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20011023
ADS-B equipped
Yes — Mode-S A82FAF
Registrant of record
INTERNATIONAL AIR SERVICES INC TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control on landing resulting in the aircraft leaving the runway environment, crossing a ditch and nosing over. Contributing factors were variable winds reported by the pilot and the ditch.
Factual narrative
On February 10, 2002, approximately 1321 Pacific standard time, a Boeing Stearman A75N1, N62658, registered to, and operated/being flown by a private pilot, incurred substantial damage during a loss of control and nose over on landing at the Creswell airport, Creswell, Oregon. The pilot and passenger were uninjured. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was personal, was operated under 14CFR91, and originated from Creswell, stopping at Eugene, Oregon, and then departing about 1305 back to Creswell. The pilot reported to law enforcement authorities immediately after the accident that during the landing roll on runway 33 "…he lost control of the plane…" and that "…he tried to correct the plane's path but couldn't…" (refer to ATTACHMENT LE-I-1). The pilot also told the FAA inspector on site that the aircraft began to veer left on runway 33. He applied rudder to correct back toward the centerline, but the aircraft veered right departing the right side of the runway. The aircraft impacted a culvert perpendicular to the east side of the runway during which the main landing gear sheared off. The culvert began approximately 81 feet east of the runway centerline (refer to ATTACHMENT LE-I-2). The aircraft then nosed over. The pilot reported that there was no mechanical malfunction with the aircraft. The pilot also reported that the winds upon landing were light and variable but that upon touchdown the wind changed to a quartering tailwind and that although he had 978 hours of total flight experience he had only 12 hours in the A75N1. Winds reported at Eugene airport 15 nautical miles northwest of the accident site were from 170 degrees magnetic at nine knots at 1254, and from 200 degrees at twelve knots at 1354. Runway 33 measures 3,100 feet in length by 60 feet in width. The minimum safety area width for a design group I, visual airport supporting small airplanes (i.e., aircraft less than 12,500 pounds in weight) is defined as 120 feet, or 60 feet left and right of the centerline (refer to ATTACHMENT AD-I [page 24 of FAA Advisory Circular 150/5300-13]). The pilot of the tail wheel equipped Boeing Stearman A75N1 landed on the 3,100 foot long runway (RWY 33) at the Creswell airport. During the landing roll the aircraft began to veer left and the pilot over corrected with right rudder. The aircraft veered right off the right side of the runway impacting a culvert perpendicular to the runway and then nosed over. The pilot reported variable light winds which changed to a quartering tailwind upon touchdown. He also reported 978 hours of total flight experience and 12 hours in the A75N1. Winds approximately 30 minutes before and after the accident at Eugene, Oregon, 15 nautical miles northwest, were from the south to southwest at nine to twelve knots. The culvert began approximately 81 feet east of the runway centerline or about 21 feet outside of the lateral standard dimensions for a runway safety area established for a Design Group I (small airplane) airport. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_SEA02LA038.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 or causal vocabulary (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- 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
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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