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-11.24.25

AirborneNextGen-
11.18.25

Airborne-Unlimited-11.19.25

Airborne-AffordableFlyers-11.20.25

AirborneUnlimited-11.21.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

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

Aero-News: Quote of the Day (11.27.25)

“Achieving PMA for the S-1200 Series magnetos is another step in expanding our commitment to providing the aviation community with the most trusted and durable ‘firewal>[...]

Airborne 11.26.25: Bonanza-Baron Fini, Archer v LA NIMBYs, Gogo Loses$$$

Also: Bell 505 on SAF, NYPA Gets Flak For BizAv 'Abuse', FAA Venezuela Caution, Horizon Update Textron Aviation has confirmed it will be ending production of the Beechcraft Bonanza>[...]

FAA Seeks Info For New Brand-New ATC Platform

State-Of-The-Art Common Automation Platform To Replace Legacy Systems The FAA has issued a Request for Information (RFI) regarding the initiative of the Trump Administration and U.>[...]

USAF Reaper Drone Crashes Off the South Korean Coast

Kunsan Air Base Reported the Accident During Routine Operations The US Air Force has confirmed that it lost an MQ-9 Reaper drone to the South Korean waters on November 24. The airc>[...]

Hartzell Engine Tech Magneto Gains FAA-PMA

PowerUp S-1200 Series Approved, Available for 4- And 6-Cylinder Engines Hartzell Engine Tech announced it received FAA Parts Manufacturer Approval for its PowerUp S-1200 Series air>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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