Amateur-built ZENITH 701 accident near Trinidad, Colorado, April 30, 2015
On April 30, 2015 at about 6:57 pm local time, a 2009 amateur-built ZENITH 701, registered N95MH, was substantially damaged in an accident during maneuvering (low-alt flying) near Trinidad, Colorado. 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 noncertificated pilot's failure to maintain airspeed following a loss of engine power while maneuvering at a low altitude, which resulted in the airplane's wing exceeding its critical angle-of-attack and a subsequent aerodynamic stall. The reason for the loss of engine power could not be determined because postaccident examination revealed no evidence of mechanical failure or malfunction.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 30, 2015 · about 6:57 pm local time
- Place
- Trinidad, Colorado · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built ZENITH 701, built 2009
- Registration
- N95MH · no longer on the register · serial 001
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The noncertificated pilot was conducting a personal flight in the experimental amateur-built airplane. A witness reported seeing the airplane circling overhead about 200 to 300 ft above ground level. According to the witness, the airplane's engine was running normally. The witness reported that during the third circle, the airspeed was low, the wings were level, and the pilot was turning the airplane using only the rudder. The witness heard the engine noise stop, and the airplane "flipped over to the left" and descended in a nose-down attitude to ground impact. Postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The propeller blades displayed no evidence of rotational damage, indicating that the engine was not producing power at ground impact. An engine run was conducted, and the engine started and ran smoothly. Although it is possible that the uncoordinated (wings level) turns the pilot was making caused fuel to move away from the fuel tank ports resulting in fuel starvation, the reason for the loss of engine power was not determined. The pilot did not hold any type of pilot certificate, a medical certificate, or a valid driver's license and his flight time is unknown. It is likely that as the pilot maneuvered the airplane at a low altitude, he allowed the airspeed to decay to the point of exceeding the wing's critical angle-of-attack, which resulted in an aerodynamic stall. Further, it is likely that the pilot was lacking in flight training and experience, which prevented him from maintaining control of the airplane. Toxicological testing identified diphenhydramine, a sedating antihistamine, in the pilot's blood and urine, but the pilot's decision to perform turns at low altitude was likely not due to the effects of diphenhydramine.
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 maneuvering (low-alt flying)
- Loss of control in flight during maneuvering (low-alt flying) defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Personnel issues › Experience/knowledge › Experience/qualifications › Qualification/certification › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
Pilot
- Medical certificate: None
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 435 hours
- Last inspection: condition inspection
- Maximum gross weight: 1,100 lb
- Seats: 2
- Landing gear: fixed
- Engine: Rotax 912 ULS-2 (piston); 435 hours total
The flight
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: at 3 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 77°F (25°C), dew point 30°F (-1°C)
- Altimeter: 30.01 inHg
- Observation at 7:54 pm from TAD, 10 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
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.
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.