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-11.17.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-FltTraining-11.13.25

AirborneUnlimited-11.14.25

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

Classic Aero-TV: Extra Aircraft Announces the Extra 330SX

From 2023 (YouTube Edition): An Even Faster Rolling Extra! Jim Campbell joined General Manager of Extra Aircraft Duncan Koerbel at AirVenture 2023 to talk about what’s up and>[...]

Aero-News: Quote of the Day (11.15.25)

“Receiving our Permit to Fly and starting Phase 4 marks a defining moment for Vertical Aerospace. Our team has spent months verifying every core system under close regulatory>[...]

ANN's Daily Aero-Term (11.15.25): Middle Marker

Middle Marker A marker beacon that defines a point along the glideslope of an ILS normally located at or near the point of decision height (ILS Category I). It is keyed to transmit>[...]

NTSB Final Report: Lancair 320

The Experienced Pilot Chose To Operate In Instrument Meteorological Conditions Without An Instrument Flight Rules Clearance Analysis: The airplane was operated on a personal cross->[...]

Airborne 11.14.25: Last DC-8 Retires, Boeing Recovery, Teeny Trig TXP

Also: ATI Strike Prep, Spirit Still Troubled, New CubCrafters Dealership, A-29 Super Tucano Samaritan’s Purse is officially moving its historic Douglas DC-8 cargo jet into re>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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