Winglet Technology Receives Citation X FAA STC TOLD And MZFW Approvals | 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-06.10.24

Airborne-NextGen-06.11.24

Airborne-Unlimited-06.12.24 Airborne-FltTraining-06.13.24

Airborne-Unlimited-06.14.24

Fri, Nov 20, 2015

Winglet Technology Receives Citation X FAA STC TOLD And MZFW Approvals

Increases Maximum Zero Fuel Weight And Upgrades Take-Off And Landing Data

The FAA has granted an STC To Wichita, Kansas-based Winglet Technology for Take-Off and Landing Data (TOLD) and Maximum Zero Fuel Weight (MZFW) increase upgrades for winglet equipped Citation X. Winglet Technology is offering the FMS TOLD and 150 lb MZFW increase service bulletin upgrades to Citation X winglet customers. The FMS TOLD upgrade requires an upgrade of the Integrated Avionics Computer (IAC) which includes the long awaited NZ6.1 FMS upgrade.

The TOLD service bulletin installs the winglet STC AFM take-off and landing v-speed database and upgraded IAC required to accept the STC AFM TOLD. The MZFW service bulletin increases the MZFW from 24,400 lb to 24,550 lb to offset the 135 lb empty weight increase of the winglet STC installation.

Winglet Technology was granted an FAA Supplemental Type Certificate (STC) to install their elliptical winglet design for Cessna’s Citation X, the world’s fastest business jet, in July of 2009. Cessna Aircraft Company has made Winglet Technology’s winglet design standard for its larger, faster upgraded version of the Citation X beginning with delivery of aircraft S/N 501.

Winglet Technology’s elliptical winglet design provides superior aerodynamic performance across a broad range of Mach number and operating conditions. The elliptical design ensures the lift distribution of the wing closely matches optimum lift distribution along the span of the wing, which minimizes the induced drag of the aircraft. The resulting induced drag reduction enhances the overall operational performance and translates into a range of performance improvements for the both the Cessna Citation X and Sovereign aircraft.

(Image provided with Winglet Technologies news release)

FMI: www.winglet-technology.com

Advertisement

More News

ANNouncement: Now Accepting Applications For Oshkosh 2024 Stringers!!!

An Amazing Experience Awaits The Chosen Few... Oshkosh, to us, seems the perfect place to get started on watching aviation recover the past couple of years... and so ANN is putting>[...]

Aero-News: Quote of the Day (06.13.24)

“NBAA has a tremendous responsibility to the business aviation industry, and we are constantly collaborating with them. Our flight departments, professionals and aircraft own>[...]

ANN's Daily Aero-Term (06.13.24): Dead Reckoning

Dead Reckoning Dead reckoning, as applied to flying, is the navigation of an airplane solely by means of computations based on airspeed, course, heading, wind direction, and speed,>[...]

ANN's Daily Aero-Linx (06.13.24)

Aero Linx: Vertical Aviation Safety Team (VAST) We are a public–private initiative to enhance worldwide flight operations safety in all segments of the vertical flight indust>[...]

ANN FAQ: How Do I Become A News Spy?

We're Everywhere... Thanks To You! Even with the vast resources and incredibly far-reaching scope of the Aero-News Network, every now and then a story that should be reported on sl>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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