Cub Crafters CC18-180 accident near Raton, New Mexico, June 5, 2015
On June 5, 2015 at about 12:28 pm local time, a 2008 Cub Crafters CC18-180, registered N162WR, was substantially damaged in an accident during maneuvering (low-alt flying) near Raton, New Mexico. It was a public-use flight (federal) under public-use (government) rules. 2 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to maintain adequate airspeed while maneuvering at a low altitude, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 5, 2015 · about 12:28 pm local time
- Place
- Raton, New Mexico · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Cub Crafters CC18-180, built 2008 · all CC18-180s on the register
- Registration
- N162WR · no longer on the register · serial CC18-0035
- Damage
- Substantial damage
- Flight
- Public-use flight (federal) · public-use (government) rules
The NTSB's narrative final · quoted from the NTSB record
The airplane, which was being operated as a public aircraft, departed with the pilot and a gunner on board for the local flight. The purpose of the flight was to locate and kill coyotes in a geographical area with a history of livestock damage. According to the ground-based spotter, the pilot established radio contact with him after the airplane passed over the mesa that bordered the western edge of the target area. The pilot transmitted that he had observed a coyote behind the spotter's position and that they were going to perform a low-altitude pass for the gunner to kill the coyote. The spotter turned around and located the coyote using his binoculars. He reported that he heard 2 to 3 shotgun blasts as the airplane passed through his field of view on a northeast heading. He remained focused on the coyote as the airplane exited his field of view, and, shortly thereafter, he heard it impact the ground. A review of recovered GPS data indicated that the airplane descended to about 41 ft above the ground and then entered a climbing left turn. The airplane's calculated groundspeed decreased from 77 mph to 55 mph during the climbing left turn. According to the airplane flight manual, the wings-level aerodynamic stall speed was 52 mph with the flaps retracted; however, the stall speed increased to 56 mph when the airplane was in a coordinated 30° banked turn and 74 mph when the airplane was in a coordinated 60° banked turn. A postaccident examination established that the airplane had crashed in a nose-low, near-vertical attitude. Based on the GPS data and the near-vertical impact angle, the pilot likely did not maintain adequate airspeed during the climbing left turn, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall at a low altitude. The postaccident wreckage examination did not reveal any anomalies that would have precluded normal operation of the airplane during the flight. Although postaccident toxicological testing of the pilot identified three over-the-counter sedating antihistamines, the lack of available blood for testing prevented a determination as to whether they affected the pilot's psychomotor or cognitive functioning during the accident flight.
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 control in flight during maneuvering (low-alt flying) defining event
- Collision with terrain or object (not controlled flight into terrain) during maneuvering (low-alt flying)
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Personnel issues › Physical › Health/Fitness › Use of medication/drugs › Pilot
Pilot
- Certificate: commercial pilot
- Ratings: single-engine land; instrument: airplane
- Flight time: 13,484 hours in all; 142.3 in the last 90 days; 62.4 in the last 30 days; 13,034 as pilot in command
- Last flight review: November 20, 2014
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: frt
- Injury: fatal
The aircraft
- Airframe total time: 3,125.7 hours
- Last inspection: annual inspection, May 19, 2015; 33 hours since
- Maximum gross weight: 2,300 lb
- Seats: 2
- Landing gear: fixed
- Engine: Lycoming O-360-C4P (piston); 1,133 hours total
The flight
- Departed from: RTN Raton NM at 12:15 pm
- Destination: RTN Raton NM
Weather at the time
- Light: daylight
- Wind: from 050° at 7 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 54°F (12°C), dew point 45°F (7°C)
- Altimeter: 30.19 inHg
- Observation at 12:53 pm from RTN, 21 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
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.
