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-05.19.25

Airborne-NextGen-05.20.25

AirborneUnlimited-05.21.25

Airborne-AffordableFlyers-05.22.25

AirborneUnlimited-05.23.25

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

ANN's Daily Aero-Term (05.29.25): Terminal Radar Service Area

Terminal Radar Service Area Airspace surrounding designated airports wherein ATC provides radar vectoring, sequencing, and separation on a full-time basis for all IFR and participa>[...]

ANN's Daily Aero-Term (05.30.25): Very High Frequency (VHF)

Very High Frequency (VHF) The frequency band between 30 and 300 MHz. Portions of this band, 108 to 118 MHz, are used for certain NAVAIDs; 118 to 136 MHz are used for civil air/grou>[...]

Aero-News: Quote of the Day (05.30.25)

“From approximately November 2021 through January 2022, Britton-Harr, acting on behalf of AeroVanti, entered into lease-purchase agreements for five Piaggio-manufactured airc>[...]

Airborne 05.23.25: Global 8000, Qatar B747 Accepted, Aviation Merit Badge

Also: Virtual FLRAA Prototype, IFR-Capable Autonomous A/C, NS-32 Crew, Golden Dome Missile Defense Bombardier announced that the first production Global 8000 successfully completed>[...]

ANN's Daily Aero-Linx (05.30.25)

Aero Linx: The 1-26 Association (Schweizer) The Association’s goal is to foster the helpfulness, the camaraderie, and the opportunity for head-to-head competition that is fou>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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