EASA Lifts EAD On Tamarack Aerospace Active Winglets | 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-05.06.24

Airborne-NextGen-04.30.24

Airborne-Unlimited-05.01.24 Airborne-AffordableFlyers--05.02.24

Airborne-Unlimited-05.03.24

Tue, Jul 09, 2019

EASA Lifts EAD On Tamarack Aerospace Active Winglets

Decision Allows European Registered Active Winglet Equipped CitationJets To Fly Unrestricted

EASA has lifted restrictions put in place by the April Emergency Airworthiness Directive (EAD) on Cessna CitationJets equipped with ATLAS Active Winglets. This comes in the form of an STC amendment that includes EASA Service Bulletin SB1480.

The new Service Bulletin requires that all Textron Aviation models 525, 525A, and 525B fitted with Tamarack’s Active Winglet technology incorporate all existing product improvements.

This allows compliant aircraft to resume flying normally.

“Tamarack made product improvements available prior to the EAD which enhance the safety and reliability of the ATLAS active winglets. We are pleased that EASA has agreed that these improvements address the safety concern that prompted the EAD.” says Jacob Klinginsmith, President of Tamarack. “EASA and the FAA have been meeting regularly and we anticipate that the FAA will offer a solution to the limitations very shortly, in the spirit of the bi-lateral agreement in place between the agencies.”

SB1480 requires that the affected jets incorporate all existing product improvements, including SB1467, issued in April 2018, which enhances the reliability of the TACS Control Unit (TCU), found to be at fault in an April 2019 incident preceding the EASA EAD.

SB1480 also requires that the affected jets incorporate SB1475, issued in March 2019, which consists of centering strips attached to the upper and lower trailing edge of the Tamarack Active Camber Surface (TACS). In the unlikely event of a system fault, the centering strips aerodynamically force the TACS back to their faired position, reducing the impact of the fault.

(Source: Tamarack Aerospace news release. Image from file)

FMI: www.tamarackaero.com

Advertisement

More News

ANN's Daily Aero-Term (05.05.24): Omnidirectional Approach Lighting System

Omnidirectional Approach Lighting System ODALS consists of seven omnidirectional flashing lights located in the approach area of a nonprecision runway. Five lights are located on t>[...]

Aero-News: Quote of the Day (05.05.24)

"Polaris Dawn, the first of the program’s three human spaceflight missions, is targeted to launch to orbit no earlier than summer 2024. During the five-day mission, the crew >[...]

Airborne 05.06.24: Gone West-Dick Rutan, ICON BK Update, SpaceX EVA Suit

Also: 1800th E-Jet, Uncle Sam Sues For Landing Gear, Embraer Ag Plane, Textron Parts A friend of the family reported that Lt. Col. (Ret.) Richard Glenn Rutan flew west on Friday, M>[...]

Airborne 05.03.24: Advanced Powerplant Solutions, PRA Runway Woes, Drone Racing

Also: Virgin Galactic, B-29 Doc to Allentown, Erickson Fire-Fighters Bought, FAA Reauthorization After dealing with a big letdown after the unexpected decision by Skyreach to disco>[...]

Aero-News: Quote of the Day (05.06xx.24)

“Our aircrews are trained and capable of rapidly shifting from operational missions to humanitarian roles. We planned to demonstrate how we, and our BORSTAR partners, respond>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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