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-04.29.24

Airborne-NextGen-04.30.24

Airborne-Unlimited-05.01.24 Airborne-AffordableFlyers--05.02.24

Airborne-Unlimited-05.03.24

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

ANN's Daily Aero-Term (05.02.24): Touchdown Zone Lighting

Touchdown Zone Lighting Two rows of transverse light bars located symmetrically about the runway centerline normally at 100 foot intervals. The basic system extends 3,000 feet alon>[...]

Aero-News: Quote of the Day (05.02.24)

“Discovery and innovation are central to our mission at Virgin Galactic. We’re excited to build on our successful record of facilitating scientific experiments in subor>[...]

Aero-News: Quote of the Day (05.03.24)

"We are reaching out to you today on behalf of the Popular Rotorcraft Association because we need your help. We are dangerously close to losing a critical resource that if lost, wi>[...]

ANN's Daily Aero-Term (05.03.24): UAS Traffic Management (UTM)

UAS Traffic Management (UTM) The unmanned aircraft traffic management ecosystem that will allow multiple low altitude BVLOS operations and which is separate from, but complementary>[...]

ANN's Daily Aero-Linx (05.03.24)

Aero Linx: Society of Aviation and Flight Educators (SAFE) SAFE is a member-oriented organization of aviation educators fostering professionalism and excellence in aviation through>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC