NTSB CAROL · Event
Event WPR24FA270
Registry · N2764Q
FAA Aircraft Registry record.
Make / Model
CESSNA 182K
Year of manufacture
1967 · 57 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19670216
ADS-B equipped
Yes — Mode-S A2BFB9
Registrant of record
LONG DONALD G JR
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On August 08, 2024, about 1255 mountain daylight time, a Cessna 182K, N2764Q, was substantially damaged when it was involved in an accident near Augusta, Montana. The pilot and two passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight. A father and son were hiking and as they approached Crown Mountain, they noticed smoke rising over the saddle. Upon reaching the saddle, around 1350, they observed the airplane on a steep slope still smoldering from being on fire. They were able to call the Sheriff from the accident site to report the location. A review of the FAA provided automatic dependent surveillance-broadcast (ADS-B) information disclosed that the airplane departed from Pullman/Moscow Regional Airport, Pullman, Washington about 1120 mdt. Following departure, the airplane continued on a northeast heading and maintained an altitude between 7,500 and 8,000 ft mean sea level (msl). The airplane’s track ended at the start of the mountainous terrain in the Bob Marshall Wilderness. The last return was at 1846:10 and located about 25 nm southwest of the accident site (Figure 1 below). Figure 1: Accident Site in Reference to the ADS-B Flight Track The accident site was located in a canyon 17 nm west of Augusta, Montana. The terrain consisted of loose scree beneath firmer ledges and rocky outcrops, bisected by a gradual central gully with forest vegetation. The south canyon wall reached an elevation of 8,450 feet, while the north wall, known as Crown Mountain, peaked at 8,400 feet. The airplane came to rest on a steep south-facing slope at an elevation of 7,550 feet. The airplane’s nose was oriented upslope on a magnetic bearing of approximately 140°. The wreckage was scattered over a 90-foot area, with the most distant debris, primarily windscreen fragments, located east of the main wreckage. The main wreckage, which included all major control surfaces, was found 800 feet below the cliff's top and 625 feet above the canyon floor (Figure 2 below). Figure 2: The Canyon where the Accident Site was Located The fuselage and inboard sections of the wings had been consumed by fire. Within the debris field, fragments of red and blue/green plastic lens covers were found east and west of the main wreckage, respectively, consistent with the wings impacting the terrain with the airplane in a near wings level, nose-up attitude (Figure 3 below). Investigators established continuity of the flight control systems; the flaps were retracted. There was no evidence of catastrophic engine failure and the propeller blade signatures were consistent with the engine producing power at the time of impact. Figure 3: Accident Site on the South Slope of the Canyon Wall Investigators contacted several pilots who were flying in the accident area near the time of the accident. They reported the cloud bases were between 6,500-8,000 ft msl with the mountains obstructed by clouds. The tops of the cloud layers were reported to be between 9,500 and 11,000 msl. One of the hikers who reported the accident’s location took several pictures and provided his observations of the weather. He stated it was incredibly foggy during their hike, with visibility often reduced to less than 20 yards as the fog moved in and out, sometimes obscuring the horizon completely. When they reached the saddle, the wind picked up dramatically, and they were enveloped in fog (Figure 4 below). Figure 4: Picture Taken by a Hiker at 1351 about 2,600 ft Northeast of the Accident Site The pilot purchased the airplane in March 2022 and received his private pilot certificate in May 2023. A review of the pilot's medical records on file with the FAA indicated that on February 07, 2024, when he applied for his most recent third-class aviation medical certificate, he reported that his total flight time experience was 149 hours. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR24FA270.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 (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
Browse the full corpus — academia portal ↗