NTSB CAROL · Event
Event ANC02LA096
Registry · N2558D
FAA Aircraft Registry record.
Make / Model
CESSNA 170B
Year of manufacture
1952 · 50 years old at event
Engine
CONT MOTOR 0-300 SER (145 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560602
ADS-B equipped
Yes — Mode-S A26D85
Registrant of record
CLAYTON ALFRED T JR
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate recovery from a bounced landing, and his failure to maintain directional control of the airplane. A factor contributing to the accident was the pilot's excessive braking which resulted in a nose over.
Factual narrative
On August 14, 2002, about 2000 Alaska daylight time, a wheel-equipped Cessna 170 airplane, N2558D, sustained substantial damage when it nosed over following a loss of control while landing at the Soldotna Airport, Soldotna, Alaska. The airplane was being operated as a visual flight rules (VFR) local area personal flight under Title 14, CFR Part 91, when the accident occurred. The airplane was operated by the pilot. The private certificated pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed. The flight originated at the Soldotna Airport about 1930. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on August 14, the pilot reported that he was conducting touch and go landings on runway 25. He said the airplane touched down hard and bounced, and the propeller contacted the runway surface. The airplane veered off the left side of the runway, and the pilot applied the brakes. The airplane then nosed over, receiving damage to both wings, the vertical stabilizer, and rudder. At 1955, an automated weather observation system (AWOS) at Soldotna was reporting in part: Wind, calm; visibility, 10 statute miles; clouds and sky condition, clear; temperature, 64 degrees F; dew point, 39 degrees F; altimeter, 30.36 inHg. The private certificated pilot was conducting touch and go landings to an asphalt surfaced runway. The pilot said the airplane touched down hard and bounced, and the propeller contacted the runway surface. The airplane veered off the left side of the runway, and the pilot applied the brakes. The airplane then nosed over, receiving damage to both wings, the vertical stabilizer, and rudder. The wind was calm. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_ANC02LA096.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.
Browse the full corpus — academia portal ↗