NTSB CAROL · Event
Event CHI07TA241
Aircraft involved
Probable cause & findings
The pilot not maintaining clearance from the rising terrain. A factor contributing to the accident was the rising terrain.
Factual narrative
On July 30, 2007, about 0700 mountain daylight time, N661FB, registered as a Christen Industries Inc. A-1 airplane, operated by the State of South Dakota, sustained substantial damage when it impacted rising terrain while maneuvering near Elm Springs, South Dakota. Visual meteorological conditions prevailed at the time of the accident. The public use animal control flight was being conducted under 14 Code of Federal Regulations Part 91. No flight plan was on file. The pilot and passenger sustained minor injuries and went to a hospital. The local flight originated from the Wall Municipal Airport, near Wall, South Dakota, at 0615. The pilot stated in his accident report that he had turned and was heading south. He said that he had begun a shallow descent to maintain a constant altitude above the terrain, which was lowering toward a river bottom. The pilot's accident report, in part, further stated: As we continued to descend I noticed a slight rise in the terrain and determined that we had plenty of altitude to clear that rise and continued on with my southerly flight path and shallow descent. As we approached the slight rise in the terrain the pressure in the stick changed very quickly with a movement in the pitch axis only. The pressure came back immediately and then there was another pressure change in the stick that was a little more pronounced. This movement was identical to the other in that it was a pitch change only; there was no movement in the roll direction. After the second time the pitch change changed I made a remark to the gunner and the crash took place. At 0652, the recorded weather at the Rapid City Regional Airport, near Rapid City, South Dakota, was: Wind 150 degrees at 7 knots; visibility 10 statute miles; sky condition clear; temperature 21 degrees C; dew point 17 degrees C; altimeter 29.97 inches of mercury. The airplane impacted rising terrain while maneuvering on a public use animal control flight. The pilot said that he had turned and was heading south and had begun a shallow descent to maintain a constant altitude above down-sloping terrain. The pilot said, "As we continued to descend I noticed a slight rise in the terrain and determined that we had plenty of altitude to clear that rise and continued on with my southerly flight path and shallow descent. As we approached the slight rise in the terrain the pressure in the stick changed very quickly with a movement in the pitch axis only. The pressure came back immediately and then there was another pressure change in the stick that was a little more pronounced. This movement was identical to the other in that it was a pitch change only; there was no movement in the roll direction. After the second time the pitch change changed I made a remark to the gunner and the crash took place." Flight control continuity was confirmed. An examination of the airplane's systems revealed no anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_CHI07TA241.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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Flight simulation has made progressively significant inroads into pilot training at all levels of a pilot’s career – typically starting with training for the Instrument rating in light aircraft and co…
- Embry-Riddle Scholarly Commons 2020 · Conference paper
Backwards Chaining – Accelerating Solo Flight Training
Flight simulation has made progressively significant inroads into pilot training at all levels of a pilot’s career – typically starting with training for the Instrument rating in light aircraft and co…
- NASA NTRS 2019 · Conference Paper
Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- Embry-Riddle Scholarly Commons 2018 · Conference paper
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The ubiquity of computing technology has revolutionized the workplace and has also had a significant impact on education. The use of interactive simulations based on virtual reality (VR), augmented re…
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