NTSB CAROL · Event
Event ANC97LA048
Registry · N218CS
FAA Aircraft Registry record.
Make / Model
CESSNA T240
Year of manufacture
2013
Engine
CONT MOTOR TSIO-550-C (310 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20130912
ADS-B equipped
Yes — Mode-S A1D77D
Registrant of record
TEXTRON AVIATION INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's decision to continue VFR into IMC. Factors associated with the accident are fog/obscuration, and the pilot's failure to initiate a go-around earlier in the approach.
Factual narrative
On April 7, 1997, about 1506 Alaska daylight time, a wheel equipped Piper PA-31 airplane, N218CS, owned and operated by Cape Smythe Air Service, received substantial damage while landing at the Stebbins Airport, Stebbins, Alaska. None of the six passengers aboard, or the airline transport certificated pilot, reported any injuries. The 14 CFR Part 135 scheduled commuter flight, Flight 365, departed Nome, Alaska, about 1419, en route to Stebbins. A visual flight rules flight plan was in effect. The reported weather at Stebbins was characterized as instrument meteorological conditions at the time of the accident. According to witness reports, fog obscured the gravel and snow covered airstrip. The airplane was observed at a low altitude, close to the threshold of runway 05. It banked hard to the left, and right, and then collided with terrain near the runway threshold. The airplane continued down the runway a short distance, then veered off the left side of the runway and struck a snow berm. At the time of the accident, a weather observer at Stebbins estimated the visibility to be 3/8 of a mile. During a telephone conversation with the NTSB investigator-in-charge on April 17, the pilot related as he approached Stebbins, he was given a weather observation from a weather observer at Stebbins that indicated the prevailing visibility was about 1/4 mile in fog and mist. He said that was later amended to 3/8 of a mile. About seven miles from Stebbins, he said he was able to see a portion of the runway, the approach end of runway 05. The reminder of the runway and village was shrouded in fog. As he continued his approach to Stebbins, and entered a left base for runway 05, he said he realized he was in too close to the runway, performed a tight "S" turn to gain a little distance from the runway, reduced power on the turbine engines to idle, and turned final approach. During final approach, he said he was too low and too slow. He heard the stall warning horn, and quickly added full power to go-around. The airplane rolled hard to the right at the application of power, and the right wing hit the ground. In his written report to the NTSB, under the section titled: "Recommendation (how could this accident been prevented)", the pilot wrote: "Should have made a decision sooner, to go-around and get lined up with the runway." The pilot also estimated the visibility in the vicinity of the airport as 1.5 miles. The pilot was landing at a remote village site. Reported weather was approximately 3/8 of a mile at the time of the accident. The pilot estimated the in-flight visibility as 1.5 miles, and said although much of the runway was shrouded in fog and mist, he could see the approach end of runway 05. While on a base leg to runway 05, he said he was in too close to the runway, and elected to do a tight 'S' turn to gain additional spacing. As he turned to final, he reduced engine power to idle. He subsequently realized he was too low and too slow, heard the stall warning horn, and quickly added full power. The airplane rolled to the right, and struck the runway with the right wing. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_ANC97LA048.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, go-around, vfr into imc, imc). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
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