Agusta Spa A109E accident near Newkirk, New Mexico, July 17, 2014
On July 17, 2014 at about 7:42 am local time, a 2000 Agusta Spa A109E (helicopter), registered N507CF, was destroyed in an accident during enroute (cruise) near Newkirk, New Mexico. It was a positioning flight under general aviation rules (Part 91). 3 people were killed. The weather was conditions the NTSB did not record.
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The NTSB's probable cause their words, unchanged
The pilot's inadvertent visual flight into instrument meteorological conditions, which resulted in a loss of helicopter control.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- July 17, 2014 · about 7:42 am local time
- Place
- Newkirk, New Mexico · map
- Type
- Accident
- Injuries
- 3 people were killed.
- Weather
- conditions the NTSB did not record
- Aircraft
- Agusta Spa A109E E, built 2000 · all A109Es on the register
- Registration
- N507CF · no longer on the register · serial 11067
- Damage
- Destroyed
- Flight
- Positioning flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
After the commercial pilot received an emergency medical services helicopter flight request, he quickly (in about 20 seconds) assessed the weather conditions and accepted the flight. No records were found indicating that the pilot obtained an official weather briefing before departing on the flight, and the investigation could not determine which weather resources the pilot used to assess the weather. About 8 minutes later, the pilot called the company's operations center to report that the flight was departing; this was the last communication received from the pilot. The helicopter was operating in an area that was known by company pilots, including the accident pilot, to have the potential for low visibility, even though there were no airport weather reporting facilities or Doppler radar coverage in the area. A review of GPS data showed that, while en route to pick up the patient, the helicopter performed a slight descending 360° turn before continuing toward the hospital. Weather overlays with the GPS track indicated that the helicopter made the 360° turn about the same time that an outflow boundary wave, which could have increased the potential for windshear and strong updrafts and downdrafts and reduced ceilings and visibility. Following the 360° turn, the helicopter proceeded toward the destination. About 14 minutes later, the helicopter turned right and began flying toward a major highway. It is likely that, due to the reduced visibility in the area, the pilot was flying toward the highway to follow the lights toward the city. The helicopter then turned further right and began to climb. As the helicopter entered another outflow boundary wave, it turned left. The left turn tightened, and the helicopter began to rapidly descend into terrain. The helicopter impacted a mesa in a near-level attitude. A review of a company communication recording showed that, about 17 minutes after the estimated accident time, the operations center attempted to contact the flight crew and was unsuccessful. The company sent three company helicopters to the accident helicopter's last known position; one helicopter pilot flew near the helicopter's site but was unable to see anything, and the two other pilots could not proceed close to the accident site due to clouds and low visibility. The wreckage was subsequently located by local law enforcement. A postaccident examination of the helicopter and engine did not reveal any anomalies that would have prevented normal operation. Due to mid- and low-level cloud cover, it is likely that no lunar or celestial lighting was available for amplification by the pilot's night vision goggles (NVG). Since the helicopter was not equipped with an infrared spotlight, only cultural light would have been available for NVG amplification. However, the helicopter was operating in a remote, sparsely populated area with minimal cultural light. Although the pilot's recurrent training included recovery procedures from inadvertent entry into instrument meteorological conditions (IMC), and his training records showed that he satisfactorily completed this item on his most recent training flight about 8 months before the accident, the circumstances of the accident are consistent with the pilot's inadvertent visual flight into IMC, which resulted in a loss of helicopter control.
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
- VFR encounter with IMC during enroute (cruise)
- Loss of control in flight during enroute (cruise) defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Environmental issues › Conditions/weather/phenomena › Light condition › Dark › Effect on operation
- Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Clouds › Effect on operation
- Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Clouds › Awareness of condition
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: instructor: helicopter; instructor: instrument helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 6,167 hours in all; 208 in this make and model; 28.1 in the last 90 days; 9.8 in the last 30 days; 1,189 on instruments
- Last flight review: November 26, 2013
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 3,703 hours
- Last inspection: approved inspection programme, July 4, 2014; 16 hours since
- Maximum gross weight: 6,283 lb
- Landing gear: fixed
- Engine 1: P&W Canada PW206C (turboshaft); 4,358 hours total
- Engine 2: P&W Canada PW206C (turboshaft); 3,866 hours total
- Fire on the ground
- Operator: Tristate Careflight LLC
The flight
- Departed from: SAF Santa Fe NM at 6:51 am
- Destination: Tucumcari NM
Weather at the time
- Light: night
- Wind: from 050° at 18 knots
- Visibility: 10 statute miles
- Sky: overcast at 1,500 ft; ovct at 1,500 ft
- Temperature: 66°F (19°C), dew point 55°F (13°C)
- Altimeter: 30.03 inHg
- Observation at 7:35 am from KTCC, 32 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flig | 3 |
About this page
Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The docket at the NTSB holds the report as a PDF and the investigation's photographs and documents. This site never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number CEN14FA369.
