Piper PA-24-250 accident near Aberdeen, Idaho, December 17, 2018
On December 17, 2018 at about 2:55 pm local time, a 1959 Piper PA-24-250, registered N6283P, was substantially damaged in an accident during initial climb near Aberdeen, Idaho (Aberdeen Muni airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's diverted attention during the takeoff climb due to a loss of engine power, which resulted in the airplane’s exceedance of the critical angle of attack and subsequent stall/spin.
Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 17, 2018 · about 2:55 pm local time · cases in 2018
- Place
- Aberdeen, Idaho · Aberdeen Muni · cases near this airport · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA-24-250, built 1959 · all PA-24-250s on the register
- Registration
- N6283P · no longer on the register · serial 24-1393
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
Security camera video captured the airplane during the initial climb after takeoff. The video showed that as the airplane entered the view of the camera, it appeared to be in a shallow climb; however, about 14 seconds later, the airplane descended in a near vertical manner, out of view of the camera. The airplane impacted open terrain about 1,850 ft west of the departure end of the runway. Examination of the airframe revealed no mechanical anomalies that would have precluded normal operation; however, the left fuel selector valve was in the left wingtip tank position, and the right selector valve was in in a position between the right main fuel tank and right wingtip tank position. The Airplane Flight Manual Supplement for the wingtip fuel tank installation stated that the wingtip tank fuel was to be used in level flight only. It is likely that because of the placement of the fuel port in the wingtip fuel tanks, when the airplane was in a climb attitude, the fuel may not have reached the fuel port in the tank. As a result, the pilot’s improper positioning of the fuel valves could have led to fuel starvation during the takeoff climb and resulted in a loss of engine power. Additionally, examination of the engine revealed that both magnetos were found in poor condition and showed evidence of little maintenance being performed. The left magneto drive shaft would not rotate. Disassembly of the left magneto revealed excessive wear on the bearing race that is attached to the drive shaft. The excessive wear allowed the magnets to contact the magneto housing, which resulted in the magneto being grounded, thus inoperative. The inoperative magneto would have partially reduced engine power. It is likely that the pilot experienced a loss of engine power to some degree during takeoff initial climb and his attention could have been diverted as part of troubleshooting the loss of engine power. The pilot's diverted attention most likely allowed for the airplane to exceed its critical angle of attack, resulting in a stall and subsequent spin at an altitude too low for recovery.
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 engine power (partial) during initial climb
- Loss of control in flight during initial climb defining event
- Collision with terrain or object (not controlled flight into terrain) during initial climb
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Personnel issues › Psychological › Attention/monitoring › Attention › Pilot
- cause Aircraft › Aircraft power plant › Ignition system › Magneto/distributor › Failure other cases naming the engine
- cause Aircraft › Aircraft systems › Fuel system › Fuel selector/shutoff valve › Incorrect use/operation other cases naming the fuel system
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 292.2 hours in all; 172.6 in this make and model; 48.7 in the last 90 days; 4.6 in the last 30 days; 243.3 as pilot in command
- Last flight review: February 26, 2018
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Last inspection: inspection type not recorded
- Maximum gross weight: 2,899 lb
- Landing gear: retractable
- Engine: Lycoming O-540-A1G5 (piston); 0 hours total
The flight
- Departed from: U36 Aberdeen ID
- Destination: Vernal UT
- Flight plan: none
- Runway 25, 3,690 ft by 50 ft
Weather at the time
- Light: daylight
- Wind: from 050° at 3 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 14°F (-10°C), dew point 10°F (-12°C)
- Altimeter: 30.26 inHg
- Observation at 2:53 pm from KPIH, 14 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Photographs from the investigation 7 pictures from the NTSB's docket, as the NTSB released them
Photo 1 – View of the accident site and main wreckage.
Photo 2 - View of the accident site and main wreckage.
Photo 3 – View of right wing.
Photo 4 – View of the forward portion of the airframe and engine.
Photo 5 – View of the main wreckage and left wing.
Photo 6 – View of the fuel selector valve handles.
Photo 7 – View of the engine.The NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
9 documents, released by the NTSB on November 18, 2020. 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.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Video Review Summary | PDF, 3 pages · our copy | View Download |
| 2 | NTSB Accident Site, Airframe and Engine Examination Summary | PDF, 8 pages · our copy | View Download |
| 3 | Magneto Examination | PDF, 2 pages · our copy | View Download |
| 4 | Brittain Airplane Flight Manual Supplement Revision A 0-9-1968 | PDF, 2 pages · our copy | View Download |
| 5 | Statement of Party Representatives to NTSB Investigation - Lycoming | PDF, 1 page · our copy | View Download |
| 6 | Statement of Party Representatives to NTSB Investigation - Piper | PDF, 1 page · our copy | View Download |
| 7 | Toxicological Report | PDF, 1 page · our copy | View Download |
| 8 | Photo Array | PDF, 7 pages · our copy | View Download |
| 9 | Airport Security Video | video · our copy | View Download |
Connections how this case links to the rest of the register
- N6283P: not on the register today · the record of its deregistration
- Piper PA-24 Comanche 2,428 registered today · the model family and its accident history
- Piper 44,838 aircraft on the register
- Engine: Lycoming O-540-A1G5 5,245 aircraft carry this series today · as the NTSB recorded it
- Aberdeen Municipal · nearest airport
- Accidents and incidents in Idaho 1,535 since 1982 · 288 in the last ten years
- Idaho 4,201 aircraft registered
The whole map of how records connect · these connections as data: /graph/accident/WPR19FA042.json.
The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.
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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
