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 October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 17, 2018 · about 2:55 pm local time
- Place
- Aberdeen, Idaho · Aberdeen Muni · 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
- cause Aircraft › Aircraft systems › Fuel system › Fuel selector/shutoff valve › Incorrect use/operation
- 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 |
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 | View Download |
| 2 | NTSB Accident Site, Airframe and Engine Examination Summary | PDF, 8 pages | View Download |
| 3 | Magneto Examination | PDF, 2 pages | View Download |
| 4 | Brittain Airplane Flight Manual Supplement Revision A 0-9-1968 | PDF, 2 pages | View Download |
| 5 | Statement of Party Representatives to NTSB Investigation - Lycoming | PDF, 1 page | View Download |
| 6 | Statement of Party Representatives to NTSB Investigation - Piper | PDF, 1 page | View Download |
| 7 | Toxicological Report | PDF, 1 page | View Download |
| 8 | Photo Array | PDF, 7 pages | View Download |
| 9 | Airport Security Video | video | View Download |
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.
