NTSB Final Report: Cirrus Design Corp SR22 | 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

Tue, Sep 30, 2025

NTSB Final Report: Cirrus Design Corp SR22

Student Pilot Added Engine Power To Execute A Go-Around But Could Not Stop The Airplane’s Left Drift

Location: Cleburne, Texas Accident Number: CEN25LA324
Date & Time: August 13, 2025, 13:00 Local Registration: N654CD
Aircraft: Cirrus Design Corp SR22 Aircraft Damage: Substantial
Defining Event: Loss of control in flight Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Instructional

Analysis: The student pilot stated for the preparation for his initial solo flight, he successfully completed three takeoffs and landings with his flight instructor at the airport that was planned to be used for the solo flight. During the solo flight, the student pilot completed two full stop landings without any issues prior to attempting a third takeoff and landing. The student pilot stated that during the third attempt, the airplane crossed the runway threshold about 82 to 84 kts with full wing flaps. When the airplane crossed over the runway numbers, he reduced the engine power to idle, and the airplane entered a normal float but began to drift left. He tried to arrest the drift with rudder application, but he could not maintain the runway centerline. The student pilot added engine power to execute a go-around but could not stop the airplane’s left drift. The airplane impacted the ground in a left wing and nose down attitude, which resulted in substantial damage to the left wing, the engine firewall, and the rudder. The student pilot stated there was no mechanical malfunction/failure of the airplane that would have precluded normal airplane operation.

Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this accident to be -- The student pilot’s failure to maintain airplane directional control during the approach and subsequent go-around.

FMI: www.ntsb.gov

Advertisement

More News

Classic Aero-TV: Extra; the Airplane, the Man, and His Grand DeLand Plan

From 2023 (YouTube Edition): Germany’s Best by Way of Florida Established in 1980 by German aerobatic pilot Walter Extra as a means by which to design and develop his own air>[...]

ANN FAQ: Follow Us On Instagram!

Get The Latest in Aviation News NOW on Instagram Are you on Instagram yet? It's been around for a few years, quietly picking up traction mostly thanks to everybody's new obsession >[...]

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>[...]

ANN's Daily Aero-Term (11.27.25): Ultralight Vehicle

Ultralight Vehicle A single-occupant aeronautical vehicle operated for sport or recreational purposes which does not require FAA registration, an airworthiness certificate, or pilo>[...]

ANN's Daily Aero-Linx (11.27.25)

Aero Linx: The de Havilland Moth Club Ltd The de Havilland Moth Club evolved from a belief that an association of owners and operators of Moth aeroplanes should be formed to create>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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