Cessna 182 accident near Imnaha, Oregon, June 24, 2020
On June 24, 2020 at about 2:41 am local time, a 1971 Cessna 182, registered N9169G, was substantially damaged in an accident during initial climb near Imnaha, Oregon (Memaloose Usfs airport). It was a personal flight under general aviation rules (Part 91). 2 people were seriously injured; 2 others were unhurt. The weather was visual conditions (good weather).
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The NTSB's probable cause their words, unchanged
The pilot’s excessively high pitch attitude and failure to maintain adequate airspeed during takeoff, which resulted in an exceedance of the airplane’s critical angle of attack and impact with terrain. Contributing to the accident was the pilot’s fatigue and his incomplete actions to abort the takeoff.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 24, 2020 · about 2:41 am local time
- Place
- Imnaha, Oregon · Memaloose Usfs · map
- Type
- Accident
- Injuries
- 2 people were seriously injured; 2 others were unhurt.
- Weather
- visual conditions (good weather)
- Aircraft
- Cessna 182 N, built 1971 · all 182s on the register
- Registration
- N9169G · registry record · serial 182
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot and three passengers were making an intermediate stopover at a mountain airstrip to camp with his family. They overflew the destination airport, and the pilot did not observe any concerns, but after they landed at the airport, the airplane became lodged in soft dirt. After several hours, they freed the airplane and decided to return to the airport they had departed from that morning. The pilot stated he felt the airplane begin to lift off the ground early during takeoff, so he maintained a nose low attitude to build up airspeed before starting a climb. When the airplane reached midfield, the pilot suddenly felt the airplane slow down and assumed the landing gear had contacted the runway. He wanted to abort the takeoff, but instead decided to fly the airplane as it had suddenly started to climb. Nearing the end of the runway he shoved the yoke forward after he heard the stall warning horn, but the airplane rolled to the right and impacted the ground. The pilot reported no preimpact mechanical malfunctions or failures with the airplane or engine that could have precluded normal operation. Contrary to the pilot’s recollection of events, flight data showed the airplane pitch increased excessively during the takeoff and the initial climb, and engine power decreased to about idle power as the airplane rotated, continued to climb, and airspeed decreased below stall speed. The stall warning horn likely engaged about the time the airplane’s critical angle of attack was exceeded, resulting in an aerodynamic stall and subsequent impact with terrain. Performance computations for the accident flight were consistent with the pilot’s, which suggested the airplane had sufficient takeoff distance to depart the runway, despite a high-density altitude. Weight and balance computations showed that the airplane was not over gross weight or outside of center of gravity limitations but that it was in a state of forward center of gravity at the time of the accident. The forward center of gravity would have resulted in a nose-heavy condition that required additional back pressure to maintain control during takeoff. The investigation did not find any evidence to suggest the airplane “slowed” during takeoff as the pilot suggested, but a wet patch on the runway or natural obstacles such as small rocks could have been present and adversely affected the takeoff roll. The accident pilot was likely fatigued after working for several hours to free the airplane from being lodged in soft dirt. This factor, coupled with stress and the pilot’s reported self-induced pressure to depart the airport, may have impaired the pilot’s judgment and decision making, causing him to overlook some of the risks associated with this departure. The fatigue likely also affected his ability to properly respond during the takeoff attempt.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Loss of control in flight during initial climb defining event
- Aerodynamic stall/spin during initial climb
- Collision with terrain or object (not controlled flight into terrain) during initial climb
The NTSB's findings
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- Personnel issues › Psychological › Personality/attitude › Motivation/respond to pressure › Pilot
- Environmental issues › Physical environment › Terrain › Rough terrain › Effect on operation
- Environmental issues › Task environment › Pressures/demands › Personal pressure › Awareness of condition
- Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Pitch control › Not attained/maintained
Pilot
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Flight time: 771.9 hours in all; 163.6 in this make and model; 43.4 in the last 90 days; 32.5 in the last 30 days; 716.7 as pilot in command; 0 on instruments
- Last flight review: December 16, 2019
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 5,268.7 hours
- Last inspection: annual inspection, April 20, 2020; 36.7 hours since
- Maximum gross weight: 2,950 lb
- Seats: 4
- Landing gear: fixed
- Engine: Continental O-470 UTS (piston); 5,268 hours total
The flight
- Departed from: 25U Imnaha OR at 2:41 am
- Destination: KLWS Lewiston ID
- Flight plan: none
- Runway 17/3, 3,300 ft by 120 ft
Weather at the time
- Light: dusk
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 79°F (26°C), dew point 45°F (7°C)
- Altimeter: 30.05 inHg
- Observation at 2:51 am from KMYL, 41 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flig | 1 | |||
| Passengers | 1 | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
About this page
Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number WPR20LA194.
