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-06.23.25

Airborne-NextGen-06.24.25

AirborneUnlimited-06.25.25

Airborne-AffordableFlyers-06.26.25

AirborneUnlimited-06.27.25

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

NTSB Prelim: Piper PA-23

Pilot Also Reported That Due To A Fuel Leak, The Auxiliary Fuel Tanks Were Not Used On June 4, 2025, at 13:41 eastern daylight time, a Piper PA-23, N2109P, was substantially damage>[...]

ANN FAQ: Submit a News Story!

Have A Story That NEEDS To Be Featured On Aero-News? Here’s How To Submit A Story To Our Team Some of the greatest new stories ANN has ever covered have been submitted by our>[...]

Classic Aero-TV: One Man’s Vietnam

From 2023 (YouTube Edition): Reflections on War’s Collective Lessons and Cyclical Nature The exigencies of war ought be colorblind. Inane social-constructs the likes of racis>[...]

ANN's Daily Aero-Linx (07.03.25)

Aero Linx: Colorado Pilots Association (CPA) Colorado Pilots Association was incorporated as a Colorado Nonprofit Corporation in 1972. It is a statewide organization with over 700 >[...]

ANN's Daily Aero-Term (07.03.25): High Speed Taxiway

High Speed Taxiway A long radius taxiway designed and provided with lighting or marking to define the path of aircraft, traveling at high speed (up to 60 knots), from the runway ce>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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