SEA84LA089
1984-04-14 · EVERETT, Washington, United States · None · 1 aircraft · Status: Completed
Airport PAE
Current FAA registration · N7535C
- Make / Model
- FORNEY F-1
- Year of manufacture
- 1958 · 26 years old at event
- Engine
- CONT MOTOR C90 SERIES (95 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19581024
- ADS-B equipped
- Yes — Mode-S AA2838
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACFT MADE A HARD LANDING AND BOUNCED. THE PLT SAID HE THINKS HE HIT A DOWNDRAFT. THE ACFT WENT OFF THE RWY INTO THE GRASS AND DAMAGED THE NOSE GEAR AND THE FUSELAGE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1984_SEA84LA089.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. All research papers
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- arXiv 2022 · arXiv preprint Mach and Reynolds Number Effects on Transonic Buffet on the XRF-1 Transport Aircraft Wing at Flight Reynolds Number
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- NASA NTRS 2019 · Conference Paper Lightning attachment patterns and flight conditions experienced by the NASA F-106B airplane from 1980 to 1983
The direct lightning strike data and associated flight conditions recorded from 1980 to 1983 during 742 thunderstorm penetrations with a NASA F-106B in Oklahoma and Virginia are studied with an emphas…
- NASA NTRS 2011 · Conference Paper Joint thunderstorm operations using the NASA F-106B and FAATC/AFWAL Convair 580 airplanes
During the 1985 thunderstorm season, three joint thunderstorm research flights were conducted within 100 n.mi. of NASA Langley by the NASA Storm Hazards F-106B and the FAA/USAF CV-580 research airplan…
- NASA NTRS 2000 · Technical Memorandum (TM) Spin-Tunnel Investigation of a 1/40-Scale Model of the F-111A Airplane with Store Loadings and with Supplementary Spin-Recovery Devices
An investigation has been made in the Langley spin tunnel to determine the spin and spin-recovery characteristics of the F-111A airplane in the symmetric and asymmetric stores loading conditions.
- arXiv 2025 · arXiv preprint Constrained Control Allocation With Continuous-Time Rate Constraints: Three-Dimensional Case
This paper presents a novel quadratic programming (QP) approach for constrained control allocation that directly incorporates continuous-time actuator rate constraints without requiring slack variable…