Aviation Crash Map

Mark O Treidel AMERICAN RANGER AR-1 N529MW

16 December 2025 · Denver, Colorado, United States · No injuries

Summary

On 16 December 2025 at about 17:45 local time, a Mark O Treidel AMERICAN RANGER AR-1 registered N529MW was involved in an accident near Denver, Colorado, United States. One person was on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 17:45
Classification
Accident
Location
Denver, Colorado, United States
Nearest airport
Colorado Air and Space Port Ai (CFO)
Coordinates
39.7842, -104.5376
Aircraft
Mark O Treidel AMERICAN RANGER AR-1
Registration
N529MW
Category
Gyrocraft
Year built
2017
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN26LA067

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

The pilot’s failure to attain rotor RPM and maintain proper rotor disc angle during takeoff which resulted in a rotor strike with the rudder.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot stated that it was a very windy day with winds above 20 mph and gusts to 30 mph when he attempted a takeoff in his gyroplane. He stated that during the takeoff roll with the pre-rotor engaged to 130 to140 RPM, he gently eased back on the cyclic and a gust of wind caught the rotors. He felt the rotor flap and then a bump. He immediately arrested the rotor flap and then continued the takeoff roll. When the gyroplane became airborne, he realized there was less rudder authority and returned to land at the departure airport without further incident. After landing, the pilot noticed that rudder had been damaged due to a rotor strike, which likely occurred when the rotor flapped during takeoff, resulting in substantial damage to the rudder. The pilot stated that he should have had the rotors pre-rotated to 160 RPM or greater prior to pulling back on the cyclic, and there were no preaccident mechanical malfunctions or failures of the gyroplane that would have precluded normal operation.

Quoted verbatim from the NTSB record.

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