Colorado Aviation Accidents & Incidents

Learn from Colorado's accident history to fly safer in the Rockies

2310 Total Accidents 425 Fatal 816 Fatalities 1982-2026
← Back to all accidents

PEYTON, Colorado

July 3, 2000 · NTSB DEN00LA122 · Rowley P-40F (N42915)
1 Fatal
Note: This analysis may be based on NTSB preliminary reports, which represent an initial, incomplete investigation. Facts can change as the investigation progresses, and preliminary findings should not be assumed to be accurate or final. For older events, a final NTSB report may have been issued β€” always consult the NTSB Aviation Query for the authoritative record.

NTSB Narrative

On July 2, 2000, approximately 1935 mountain daylight time, a Rowley P-40F experimental amateur-built (one of a kind) airplane, N42915, was destroyed following impact with terrain during a forced landing at Meadow Lake Airport, Peyton, Colorado. The private pilot, the sole occupant aboard the airplane, was fatally injured. He died on July 4, 2000. The pilot designed, built, and operated the airplane. Visual meteorological conditions prevailed for the Title 14 CFR Part 91 local flight that originated from Meadow Lake Airport at an unknown time. No flight plan had been filed.

Witnesses said that the pilot was performing a low fly-by over runway 33, and as the airplane reached the departure end, the engine became quiet. They said that the pilot made a left turn back towards runway 15. Subsequently the airplane hit wires, impacted terrain, cart wheeled, and came to rest against a transmission pole.

The pilot designed and built the airplane in 1986. The pilot modified the airframe and replaced the engine at some unknown time. Friends and mechanics at the airport said that the pilot worked on the airplane regularly. The airplane was powered by an AMW Cuyuna 808L-100, three cylinder, reed valve, fuel injected, water-cooled, two cycle engine which had a maximum takeoff rating of 100 horsepower at sea level. During maximum power output, it produced 8,000 to 9,000 RPM, this required a gear reduction system for normal propeller operation.

Postaccident examination of the engine and its reduction gear assembly by a mechanic revealed that the gear reduction system had failed. the pilot's inadequate decision to turn back (low altitude) towards the runway for a forced landing. A contributing factor was the total loss of engine power due to a reduction gear failure.

Case Study & Lessons Learned

Generating educational case study...

Details

NTSB ReportDEN00LA122
AircraftRowley P-40F
RegistrationN42915
DamageDEST
FAR Part091
Location39.0296, -104.4797
Corporate Sponsor
Wings Over the Rockies Air & Space Museum
Wings Over the Rockies Air & Space Museum
All Classifieds Post an Ad