NTSB Factual Report: RV8 Damaged During Crosswind Landing | 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-12.08.25

AirborneNextGen-
12.02.25

Airborne-Unlimited-12.03.25

Airborne-FltTraining-12.04.25

AirborneUnlimited-12.05.25

AFE 2025 LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Sun, Apr 19, 2020

NTSB Factual Report: RV8 Damaged During Crosswind Landing

Slot In The Tailwheel Fork That Held The Spring-Actuated Key Slide Was Slightly Deformed

Location: Harrison, OH Accident Number: CEN20CA114
Date & Time: 03/04/2020, 1402 EST Registration: N878DZ
Aircraft: Vans RV8 Aircraft Damage: Substantial
Defining Event: Loss of control on ground Injuries: 2 None

The pilot of the tailwheel-equipped airplane reported that he made a normal landing approach to the runway with a direct crosswind of 15 knots and gusts reaching 23 knots. The pilot reported that he was initially able to maintain directional control with normal flight control inputs after the airplane touched down on the main landing gear; however, when the tailwheel touched down the tail began to weathervane and the airplane veered to the right. The pilot was unable to regain directional control with an application of full left rudder and left brake before the airplane departed the right side of the runway and struck a precision approach path indicator lights (PAPI) system.

The left wing, left horizontal stabilizer, and left elevator were substantially damaged during the collision with the PAPI system. A postaccident examination and functional test of the steerable tailwheel revealed that the spring-actuated key slide would stick in the retracted position within the tailwheel fork, which allowed the tailwheel to caster instead being steerable within the normal limits intended for takeoff and landing. Additional examination revealed that the slot in the tailwheel fork that held the spring-actuated key slide was slightly deformed, and that the key had several raised edges that caused the key to bind when fully retracted in the slot.

It is likely that the tailwheel was able to caster during landing, which resulted in the pilot's inability to maintain directional control after the tailwheel had touched down during landing roll.

FMI: www.ntsb.gov

Advertisement

More News

NTSB Final Report: Patriot Aircraft LLC CX1900A

After Draining Both Wing Fuel Tanks, A Significant Amount Of Water Was Observed In The Right Wing Fuel Tank Analysis: The pilot, who was also the owner of the experimental amateur->[...]

Aero-News: Quote of the Day (12.06.25)

“Airbus apologises for any challenges and delays caused to passengers and airlines by this event. The Company thanks its customers, the authorities, its employees and all rel>[...]

ANN's Daily Aero-Term (12.06.25): High Speed Taxiway

High Speed Taxiway A long radius taxiway designed and provided with lighting or marking to define the path of aircraft, traveling at high speed (up to 60 knots), from the runway ce>[...]

ANN's Daily Aero-Linx (12.06.25)

Aero Linx: Taylorcraft Foundation, Inc. The Taylorcraft Foundation is exclusively organized for charitable, educational & scientific activities and will preserve the history an>[...]

Airborne-NextGen 12.02.25: Honda eVTOL, Arctus High-Alt UAS, Samson Patent

Also: USAF Reaper Accident, Baikonur Damage, Horizon eVTOL IFR/FIKI, New Glenn Update Honda has outlined its clearest timeline yet for its entry into the world of electric vertical>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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