North American AT-6 accident near Nunica, Michigan, September 17, 2011
On September 17, 2011 at about 10:07 pm local time, a North American AT-6, registered N217RK, was substantially damaged in an accident during takeoff near Nunica, Michigan (Hat Field Airport). It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The loss of engine power due to fuel starvation during climbout for undetermined reasons, because postaccident examination of the fuel system did not reveal any discrepancies that would have precluded normal engine operation. Contributing to the accident was the pilot not visually checking the fuel level prior to departure.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- September 17, 2011 · about 10:07 pm local time
- Place
- Nunica, Michigan · Hat Field Airport · map
- Type
- Accident
- Injuries
- 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- North American AT-6 · all AT-6s on the register
- Registration
- N217RK · no longer on the register · serial 43942
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
According to the pilot, the airplane had been refueled to its full capacity prior to the flight to the accident airport. The pilot indicated that the "flight to the accident airport required 50 minutes, which would have burned, with start-up, taxi, and flight time, 29 gallons.” The pilot then departed the accident airport and stated that he applied full takeoff power. On climbout, the low fuel pressure light illuminated just before gear retraction, the fuel pressure then dropped to zero, and the engine abruptly lost power. A video taken at the airport where the accident occurred revealed that the airplane lost power during takeoff, impacted a tree on the left side of the departure runway, and subsequently impacted terrain. The airplane’s engine monitor data revealed no recorded engine anomalies and fuel flow monitor data indicated 32.5 gallons of fuel used up to the time of the accident, and 77.1 gallons remaining. The pilot stated that he verified the fuel prior to departure at the accident airport by visual reference of fuel gauges and airplane fuel flow meter. Examination of the wreckage revealed that the right fuel tank was full. No anomalies were detected during the examination of the engine-driven fuel pump, gascolator, and the wobble pump. The fuel selector was found selected to the reserve position, which feeds from the reserve fuel retained within the standpipe and any additional left tank fuel above that retained reserve amount. The left main and reserve standpipes and screens were installed correctly and were free of obstructions. The left fuel tank contained about four gallons of fuel when it was defueled. The pilot did not visually check the level of the fuel tank’s contents prior to departure; had he done so, he would have recognized that the left tank’s fuel level was below what was expected. Fuel usage figures provided by both the pilot and the engine monitor data indicated there should have been over 20 gallons of fuel remaining in the left tank at the time of the accident. The reason for the discrepancy between the expected and actual fuel amounts could not be determined.
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 (total) during takeoff defining event
- Fuel starvation during takeoff
- Collision during takeoff/land during takeoff
The NTSB's findings
- cause Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid level
- factor Personnel issues › Task performance › Inspection › Preflight inspection › Pilot
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane
- Flight time: 4,496 hours in all; 1,209 in this make and model; 96 in the last 90 days; 27 in the last 30 days; 4,397 as pilot in command
- Last flight review: August 7, 2010
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: frt
- Injury: serious injuries
The aircraft
- Airframe total time: 10,073 hours
- Last inspection: annual inspection, February 15, 2011
- Seats: 2
- Landing gear: retractable
- Engine: Pratt & Whitney R-1340-AN1 (piston); 0 hours total
The flight
- Departed from: 5N7 Nunica MI at 10:07 pm
- Destination: TEW Mason MI
- Flight plan: none
- Runway 08, 3,600 ft by 100 ft
Weather at the time
- Light: daylight
- Wind: from 130° at 9 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 68°F (20°C), dew point 43°F (6°C)
- Altimeter: 30.29 inHg
- Observation at 9:55 pm from MKG, 8 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on January 7, 2013. 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 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 2 | Miscellaneous - Pilot Statement in Addition to the 6120.1 Form | PDF, 3 pages | View Download |
| 3 | Miscellaneous - Communication Summary -- FAA Inspector | PDF, 1 page | View Download |
| 4 | Miscellaneous - North American Trainer Association Article from April 1988 Sent by the Pilot | PDF, 1 page | View Download |
| 5 | Miscellaneous - Video of the Takeoff | MOV file | Download |
| 6 | Retention / Release of Wreckage Form and Evidence Control Form | PDF, 2 pages | View Download |
| 7 | Evidence Control Form - Shadin Fuel Flow Instrument | PDF, 1 page | View Download |
| 8 | Engine Data Monitor (EDM) - Specialist's Factual Report | PDF, 6 pages | View Download |
| 9 | Engine Data Monitor (EDM) - Attachment 1 - Tabular Data (Csv Format) | data file | Download |
| 10 | Engine Instrument 17 - Specialist's Factual Report (Fuel Flow Indicator) | PDF, 4 pages | 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.
