NTSB CAROL · Event
Event SEA02LA018
Registry · N1577K
FAA Aircraft Registry record.
Make / Model
LUSCOMBE 8C
Engine
CONT MOTOR A&C75 SERIES (75 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19750411
ADS-B equipped
Yes — Mode-S A0E787
Registrant of record
DAWSON DAN P
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Directional control not maintained during the landing roll. Factors include main gear overload and standing water on the runway.
Factual narrative
On November 26, 2001, about 1355 Pacific standard time, a Luscombe 8C, N1577K, sustained substantial damage during the landing roll on runway 26 at Olympia, Washington. The airplane is owned by the pilot, and was being operated as a visual flight rules (VFR) personal flight under the provisions of Title 14, CFR Part 91. The commercial pilot, the sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local flight. The pilot reported that this was his second touch-and-go landing of the flight. He reported that shortly after touchdown, during the landing roll, he felt a "…hard jolt" and his foot inadvertently slipped off the right rudder pedal. He stated that before he could regain control of the airplane, it departed the left side of the runway and encountered soft, wet terrain. After encountering the soft terrain, the airplane's right main gear collapsed and the right wing impacted the ground. In a subsequent written report, the pilot reported that the hard jolt was a result of the airplane encountering standing water on the runway. The pilot reported that this was his second touch-and-go landing of the flight. He reported that shortly after touchdown, during the landing roll, he felt a "…hard jolt" and his foot inadvertently slipped off the right rudder pedal. He stated that before he could regain control of the airplane, it departed the left side of the runway and encountered soft, wet terrain. After encountering the soft terrain, the airplane's right main gear collapsed and the right wing impacted the ground. In a subsequent written report, the pilot reported that the hard jolt was a result of the airplane encountering standing water on the runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_SEA02LA018.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 2020 · arXiv preprint
A Lean and Highly-automated Model-Based Software Development Process Based on DO-178C/DO-331
The emergence of a global market for urban air mobility and unmanned aerial systems has attracted many startups across the world.
- NASA NTRS 2019 · Conference Paper
A digital fly-by-wire technology development program using an F-8C test aircraft
A digital fly-by-wire flight control system has been installed in an F-8C test airplane and has undergone extensive ground and flight testing as part of an overall program to develop digital fly-by-wi…
- NASA NTRS 2016 · Conference Paper
Design and development experience with a digital fly-by-wire control system in an F-8C airplane
To assess the feasibility of a digital fly-by-wire system, the mechanical flight control system of an F-8C airplane was replaced with a digital system and an analog backup system.
- NASA NTRS 2019 · Conference Proceedings
Description and Flight Test Results of the NASA F-8 Digital Fly-by-Wire Control System
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discussed. Phase I of the program demonstrated the feasibility of using a digital fly-by-wire system for ai…
- NASA NTRS 2019 · Presentation
Failure Analysis of T-38 Aircraft Burst Hydraulic Aileron Return Line
During maintenance troubleshooting for fluctuating hydraulic pressures, a technician found that a right hand aileron return line, on the flight hydraulic side, was ruptured (Fig. 1, 2).
- Embry-Riddle Scholarly Commons 2016 · Journal article (IJAAA)
A Comparison of Cervical and Trunk Musculoskeletal Characteristics between Female and Male Army Helicopter Pilots
Introduction: Neck pain (NP) and low back pain (LBP) are prevalent among military helicopter pilots. Although there have been few studies on sex differences in the NP/LBP prevalence in this population…
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