NTSB CAROL · Event
Event SEA99LA088
Registry · N870DR
FAA Aircraft Registry record.
Make / Model
RYAN NAVION B
Engine
LYCOMING GO-435C&D SER (260 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
19551216
ADS-B equipped
Yes — Mode-S ABF6B1
Registrant of record
RAICHL JOHN P
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to reinstall the engine oil filler cap during preflight, resulting in engine oil loss and the necessity for an immediate landing.
Factual narrative
On June 17, 1999, approximately 1534 Pacific daylight time, a Ryan Navion B, N870DR, was substantially damaged in an off-runway landing at Klamath Falls International Airport, Klamath Falls, Oregon, after the pilot noted oil coming from the engine area after takeoff and turned back to the airport. The private pilot-in-command of the aircraft, who was its sole occupant, was not injured in the accident. Visual meteorological conditions were reported at Klamath Falls at 1553, and no flight plan had been filed for the 14 CFR 91 personal flight to Vacaville, California. The pilot reported that he put 1 quart of oil into the engine during his preflight, but that he forgot to replace the oil filler cap. He stated he then accomplished a normal engine start, taxi to runway 14, and preflight engine runup, then took off from runway 14. He reported that at about 600 feet above ground level, he observed oil on top of the engine cowling and on the windshield. He stated he requested an immediate return and lowered the landing gear, and was cleared by the tower to land on any runway. He stated he immediately made a "60 [degree] left turn to runway 25", and that the engine was running roughly at that point. He reported that "due to altitude", he was unable to make it back to the runway, and that the aircraft landed hard at about a 45-degree angle to the runway, just to the north side of the runway in the dirt area. During the landing, the aircraft's right main gear punched through the top of the right wing, and the bottom of the left wing was also wrinkled. The pilot reported that no mechanical failure or malfunction was involved in the accident, stating on his NTSB accident report: "Cause of accident was pilot's incomplete preflight, leaving oil filler cap off. This action precipitated the hard emergency landing [and] damage to [the aircraft]." The pilot added 1 quart of oil to the engine during preflight, but forgot to replace the oil filler cap. Immediately after takeoff from runway 14, the pilot noted oil on the top of the engine cowling and the windscreen. The pilot then requested an immediate return and was cleared to land on any runway. The pilot made a '60 [degree] left turn to runway 25' and attempted a landing with the 'engine...running roughly', but he stated that 'due to altitude' he was unable to make it back to the runway. The aircraft landed at about a 45-degree angle just to the north side of the runway in the dirt area. The landing was sufficiently hard to punch the right main landing gear through the top of the right wing. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_SEA99LA088.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 (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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