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-10.28.24

Airborne-NextGen-10.29.24

Airborne-Unlimited-10.30.24

Airborne-Unlimited-10.24.24

Airborne-Unlimited-10.25.24

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

Senator Pushes FAA to Accelerate Rocket Launch Licensing

States That Current Process is Damaging National Aerospace Development US Senator Jerry Morgan is pushing the FAA to speed up the process for rocket launch licensing. He argues tha>[...]

Classic Aero-TV: RJ Gritter - Part of Aviation’s Bright New Future

From 2015 (YouTube Edition): Model Aviator Aims For Full-Scale Career While at the 2015 Indoor Electric RC Festival, referred to as eFest, ANN CEO and Editor-In-Chief, Jim Campbell>[...]

Aero-FAQ: Dave Juwel's Aviation Marketing Stories -- ITBOA BNITBOB

Dave Juwel's Aviation Marketing Stories ITBOA BNITBOB ... what does that mean? It's not gibberish, it's a lengthy acronym for "In The Business Of Aviation ... But Not In The Busine>[...]

ANN's Daily Aero-Linx (10.27.24)

Aero Linx: Cardinal Flyers Online The Cardinal Flyers Online Web site was created and is maintained by me, Keith Peterson. My wife Debbie and I have owned a 1976 RG since 1985. Wit>[...]

ANN's Daily Aero-Term (10.27.24): Clearance Void If Not Off By (Time)

Clearance Void If Not Off By (Time) Used by ATC to advise an aircraft that the departure release is automatically canceled if takeoff is not made prior to a specified time. The exp>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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