NTSB CAROL · Event
Event CHI99LA006
Registry · N151KC
FAA Aircraft Registry record.
Make / Model
SCHWEIZER 269C
Year of manufacture
1997 · 1 years old at event
TCDS
4H12 · SCHWEIZER RSG LLC
Engine
LYCOMING HIO-360 SER (205 hp)
Seats / Engines
3 seats · 1 engine
Last airworthiness date
19971023
ADS-B equipped
Yes — Mode-S A0CECA
Registrant of record
AIR FLITE INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain control of the helicopter. Factors associated with the accident were the high winds, low altitude at which the pilot was maneuvering and the uneven terrain which the helicopter contacted.
Factual narrative
On October 10, 1998, at 1600 mountain daylight time, a Schweizer 269C, N151KC, operated by a private pilot, collided with the terrain following a loss of control while maneuvering over open land 15 miles east of Oshkosh, Nebraska. The private pilot was not injured. The helicopter was substantially damaged. The 14 CFR Part 91 flight was operating in visual meteorological conditions without a flight plan. The flight originated from Oshkosh, Nebraska, at 1445 mdt. The pilot stated that he was checking cattle while flying over "choppy" terrain at an altitude of 150 to 175 feet above the ground. He stated he was flying to the southeast then made a turn to the northeast (downwind) and had just started a turn back to the southeast when the helicopter began to settle. The pilot reported that because the terrain was uneven the helicopter rolled over to the left when it contacted the terrain resulting in extensive damage to the rotor and tail. He reported the winds were from the south southeast at 20 knots with slight gusts at the time of the accident. The pilot was checking cattle while flying over 'choppy' terrain at an altitude of 150 to 175 feet above the ground. He was flying to the southeast then made a turn to the northeast (downwind) and had just started a turn back to the southeast when the helicopter began to settle. The helicopter impacted uneven terrain and rolled over to the left. The pilot reported the winds were from the south southeast at 20 knots with slight gusts at the time of the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_CHI99LA006.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.
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