NTSB Final Report: CSP Leasing LLC MTO Sport | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-06.23.25

Airborne-NextGen-06.24.25

AirborneUnlimited-06.25.25

Airborne-AffordableFlyers-06.26.25

AirborneUnlimited-06.27.25

Mon, Nov 25, 2024

NTSB Final Report: CSP Leasing LLC MTO Sport

Gyroplane Rolled Onto Its Right Side And Off The Runway, Which Substantially Damaged The Rotor Mast

Location: Gardiner, Montana Accident Number: WPR23LA269
Date & Time: June 1, 2023, 10:21 Local Registration: N207AG
Aircraft: CSP Leasing LLC MTO Sport Aircraft Damage: Substantial
Defining Event: Sys/Comp malf/fail (non-power) Injuries: 1 Minor
Flight Conducted Under: Part 91: General aviation - Personal

Analysis: The pilot landed on the runway with about 10 mph forward speed. After touchdown, the gyroplane veered to the right despite the pilot’s full use of opposite rudder and nosewheel steering. The gyroplane rolled onto its right side and off the runway, which substantially damaged the rotor mast. Postaccident examination of the rudder/nosewheel steering system revealed that the mechanical stop was bent. There was overstress damage to three of the four control rods which likely occurred when the nosewheel turned beyond its limit during the accident landing.

The manufacturer’s construction of the rudder/nosewheel steering assembly met British Civil Airworthiness Requirements (BCAR) Section T, “Light Gyroplanes” standards. No preimpact mechanical malfunctions or anomalies were observed that would have precluded normal operation.

The airport’s website described the runway as being in poor condition, with cracks and vegetation growth throughout. However, the pilot was aware of the conditions and had made two successful landings before the accident landing. Wind conditions were reported as variable at 5 knots and likely did not influence the landing.

Although the steering system’s mechanical stop may have become bent during either the accident landing or a previous landing, the investigation was not able to determine the source of the bent stop.

Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this accident to be -- Failure of the rudder/nosewheel steering system for reasons that could not be determined, which resulted in loss of yaw control and a subsequent rollover.

FMI: www.ntsb.gov

Advertisement

More News

TikToker Arrested After Landing His C182 in Antarctica

19-Year-Old Pilot Was Attempting to Fly Solo to All Seven Continents On his journey to become the first pilot to land solo on all seven continents, 19-year-old Ethan Guo has hit a >[...]

Classic Aero-TV: Versatile AND Practical - The All-Seeing Aeroprakt A-22 LSA

From 2017 (YouTube Edition): A Quality LSA For Well Under $100k… Aeroprakt unveiled its new LSA at the Deland Sport Aviation Showcase in November. Dennis Long, U.S. Importer>[...]

ANN's Daily Aero-Term (06.27.25): Hazardous Weather Information

Hazardous Weather Information Summary of significant meteorological information (SIGMET/WS), convective significant meteorological information (convective SIGMET/WST), urgent pilot>[...]

ANN's Daily Aero-Linx (06.27.25)

Aero Linx: Historic Aircraft Association (HAA) The Historic Aircraft Association (HAA) was founded in 1979 with the aim of furthering the safe flying of historic aircraft in the UK>[...]

Aero-News: Quote of the Day (06.27.25)

"We would like to remember Liam not just for the way he left this world, but for how he lived in it... Liam was fearless, not necessarily because he wasn't afraid but because he re>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC