Colorado Aviation Accidents & Incidents
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2310 Total Accidents
425 Fatal
816 Fatalities
1982-2026
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1 Fatal
GRAND JUNCTION, Colorado
NTSB Narrative
HISTORY OF FLIGHT
On February 16, 2001, approximately 1500 mountain standard time, a Ross G-202 single-engine experimental homebuilt airplane, N39HR, was destroyed when it impacted terrain in an uncontrolled descent near Grand Junction, Colorado. The private pilot, sole occupant of the airplane, received fatal injuries. The airplane was registered to and operated by the pilot. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight departed Walker Field Airport, Grand Junction, approximately 1430.
The pilot departed the airport for a practice aerobatic flight. When the pilot failed to arrive home, the flight was reported overdue by the pilot's family. A search commenced, and the accident site was located on February 17, 2001, at 1440. The wreckage was found near the edge of a ravine in a hilly open area about 6 miles north of the departure airport.
PERSONNEL INFORMATION
The pilot received a private pilot certificate on February 20, 1972, and an instrument rating on November 8, 2000. The pilot was issued a third-class medical certificate on July 1, 1999, with the limitation "Holder shall wear correcting lenses while exercising the privileges of his/her airman certificate." According to the pilot's logbook, the pilot had logged 1,451.6 total flight hours, with 63 hours in the accident airplane, and 1 hour in the 30 days preceding the accident. In addition, the pilot had logged 2.6 flight hours performing aerobatic maneuvers.
According to emergency rescue personnel, the pilot was flying the airplane from the aft seat and was not wearing a parachute at the time of the accident.
AIRCRAFT INFORMATION
The tandem two-seat, low-wing airplane was issued an experimental airworthiness certificate on May 28, 1998. The airplane was powered by a 180-horsepower Lycoming AEIO-360-B1H engine (s/n: L-27065-51A) and equipped with a constant-speed 2 blade MTV-15-B-C/C193-34 wooden propeller. A review of the aircraft's maintenance logbooks revealed that the airplane underwent its last annual inspection on October 13, 2000, at an airframe and engine total time of 96.7 hours. The total time of the airframe and engine at the time of the accident was 105.7 hours. According to fueling records, the airplane was fueled with 11.3 gallons of 100LL avgas on February 6, 2000.
METEOROLOGICAL INFORMATION
At 1456, the weather reporting facility at Walker Field Airport (located 6 miles south of the accident site) reported the wind from 350 degrees at 3 knots, visibility 10 statute miles, sky conditions clear, temperature 6 degrees Celsius, dew point minus 6 degrees Celsius, and an altimeter setting of 30.25 inches of mercury.
WRECKAGE AND IMPACT INFORMATION
The airplane came to rest upright and remained intact except for the empennage, which was separated from the fuselage. The rudder was separated from the vertical stabilizer and was found between the fusel
On February 16, 2001, approximately 1500 mountain standard time, a Ross G-202 single-engine experimental homebuilt airplane, N39HR, was destroyed when it impacted terrain in an uncontrolled descent near Grand Junction, Colorado. The private pilot, sole occupant of the airplane, received fatal injuries. The airplane was registered to and operated by the pilot. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight departed Walker Field Airport, Grand Junction, approximately 1430.
The pilot departed the airport for a practice aerobatic flight. When the pilot failed to arrive home, the flight was reported overdue by the pilot's family. A search commenced, and the accident site was located on February 17, 2001, at 1440. The wreckage was found near the edge of a ravine in a hilly open area about 6 miles north of the departure airport.
PERSONNEL INFORMATION
The pilot received a private pilot certificate on February 20, 1972, and an instrument rating on November 8, 2000. The pilot was issued a third-class medical certificate on July 1, 1999, with the limitation "Holder shall wear correcting lenses while exercising the privileges of his/her airman certificate." According to the pilot's logbook, the pilot had logged 1,451.6 total flight hours, with 63 hours in the accident airplane, and 1 hour in the 30 days preceding the accident. In addition, the pilot had logged 2.6 flight hours performing aerobatic maneuvers.
According to emergency rescue personnel, the pilot was flying the airplane from the aft seat and was not wearing a parachute at the time of the accident.
AIRCRAFT INFORMATION
The tandem two-seat, low-wing airplane was issued an experimental airworthiness certificate on May 28, 1998. The airplane was powered by a 180-horsepower Lycoming AEIO-360-B1H engine (s/n: L-27065-51A) and equipped with a constant-speed 2 blade MTV-15-B-C/C193-34 wooden propeller. A review of the aircraft's maintenance logbooks revealed that the airplane underwent its last annual inspection on October 13, 2000, at an airframe and engine total time of 96.7 hours. The total time of the airframe and engine at the time of the accident was 105.7 hours. According to fueling records, the airplane was fueled with 11.3 gallons of 100LL avgas on February 6, 2000.
METEOROLOGICAL INFORMATION
At 1456, the weather reporting facility at Walker Field Airport (located 6 miles south of the accident site) reported the wind from 350 degrees at 3 knots, visibility 10 statute miles, sky conditions clear, temperature 6 degrees Celsius, dew point minus 6 degrees Celsius, and an altimeter setting of 30.25 inches of mercury.
WRECKAGE AND IMPACT INFORMATION
The airplane came to rest upright and remained intact except for the empennage, which was separated from the fuselage. The rudder was separated from the vertical stabilizer and was found between the fusel
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Details
| NTSB Report | DEN01FA053 |
| Aircraft | Ross G-202 |
| Registration | N39HR |
| Damage | DEST |
| FAR Part | 091 |
| Location | 39.0798, -108.5495 |
