Piper PA 14 accident near Susanville, California, August 15, 2020
On August 15, 2020 at about 8:40 pm local time, a Piper PA 14, registered N91449, was substantially damaged in an accident during takeoff near Susanville, California (Susanville Muni airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s decision to conduct a steep departure at a high-density altitude and the exceedance of the airplane’s critical angle of attack during a climb, which resulted in an accelerated stall and subsequent loss of control. Contributing to the accident was the installation of a high pitch angle propeller that was not designed for the installed engine which likely degraded the airplane’s performance.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 15, 2020 · about 8:40 pm local time
- Place
- Susanville, California · Susanville Muni · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA 14 No Series · all PA 14s on the register
- Registration
- N91449 · no longer on the register · serial 14-499
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The accident airplane’s takeoff run from a dirt runway was not observed. However, while taxiing his airplane toward the airport’s only asphalt runway, a friend of the accident pilot and pilot-rated passenger observed the accident airplane in a steep left turn about 350 ft above the runway. The airplane then transitioned into a nose-down dive, consistent with a loss of control following an accelerated stall, which resulted in impact with terrain. Examination of the wreckage revealed no preimpact mechanical anomalies with the engine or airframe that could have precluded normal operation. An experimental propeller that was designed for a more powerful engine was attached to the engine at the time of the accident. The propeller’s blade angle was excessive for the engine-propeller configuration, which would have slowed the propeller. This, in turn, would have led to an overall decrease in performance, further degrading the airplane’s ability to climb as the density altitude was nearly double the field elevation of the departure airport when the accident occurred. Additionally, the airplane may have been over its gross weight; however, this could not be determined as the fuel quantities at the time of departure were unknown. The airplane had vortex generators installed, which may have slightly reduced the airplane’s stall speed, but this performance improvement was not guaranteed as stated by the manufacturer. The investigation was unable to determine whether the pilot performed any preflight performance computations, which would have showed that the airplane required 3,750 ft of runway surface to clear a 50 ft obstacle given the temperature and density altitude. Although there was no need to clear a 50 ft obstacle that day, and this performance information was for a lower performance engine than the one he had installed, a conscientious pilot would have exercised caution during the takeoff attempt after reviewing this performance data. However, the witness observation of the airplane altitude is consistent with the pilot performing a high rate of climb departure after takeoff. The pilot’s toxicology testing demonstrated previous use of cocaine, but no active cocaine in his system at the time of the event. The investigation was unable to determine if he had any impairment from cocaine withdrawal at or near the time of the accident and whether his cocaine use contributed to the accident circumstances due to a lack of available evidence.
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 takeoff defining event
The NTSB's findings
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Pitch control › Not attained/maintained
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
- Aircraft › Aircraft propeller/rotor › Propeller system › (general) › Capability exceeded
- Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High density altitude › Effect on operation
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 200 in this make and model
- Medical certificate: BasicMed
- Seat: left
- Injury: fatal
Pilot-Rated Passenger
- Certificate: flight instructor, commercial pilot
- Ratings: single-engine land; instructor: airplane single-engine; instructor: helicopter; instrument: airplane; rotorcraft: helicopter
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 5,057.9 hours
- Last inspection: annual inspection, March 12, 2020; 44.8 hours since
- Maximum gross weight: 2,200 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming Engines O-320-A2B (piston); 0 hours total
The flight
- Departed from: RDD Redding CA at 4:30 pm
- Destination: 1Q2 Susanville CA
- Runway 07, 2,180 ft by 60 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 050° at 4 knots
- Visibility: 10 statute miles
- Sky: a few clouds at 12,000 ft
- Temperature: 91°F (33°C), dew point 43°F (6°C)
- Altimeter: 30.14 inHg
- Observation at 8:35 pm from SVE
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
19 documents, released by the NTSB on August 10, 2022. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
