Winglets - Citation X
The installation of Elliptical Winglets per the Winglet Technology’s STC will require a high degree of experience and understanding of the Citation X. The work performed to enable the installation of the winglet will require considerable modification to the existing wing structure to insure proper fit and alignment.
The installation will require, but is not limited to, the following actions:
- Removal of present wingtip, outboard rib and lighting
- Installation of a larger access door/panel in the outer wingtip area
- Installation of a new lower wing skin doubler, worked through existing access panels
- Out board wing structural reinforcement worked through existing access panels
- Installation of new wingtip rib
- Installation of new empennage mounted LED position and anti-collision lights
- Honeywell IAC Upgrade
- Final fit and installation of the new elliptical winglet
- Painting of effected area and new winglet
Starting at :
$660,935 USD
Pricing is subject to change based on model, configuration, and location.
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Example image(s) do not necessarily reflect exact applications.
| Item Number | Description | Price | Quantity |
|---|---|---|---|
| 750winglets | Citation X Winglets | $660,935.56/ea. |
|
Performance information provided by Winglet Technologies
- Reduced time-to-climb
- FL430 reduced from 137 to 37 minutes @ MTOW and ISA +10 temperatures
- FL450 reduced from 84 to 27 minutes @ MTOW and ISA temperatures
- FL470 reduced from 138 to 31 minutes @ 34,000lbs and ISA temperatures
- Higher initial flight levels
- Direct to FL 430 @ MTOW and ISA +10 temperatures
- Direct to FL 450 @ MTOW and ISA temperatures
- Direct to FL 470 @ 34,000 lbs and ISA temperatures
- Increased speed at higher altitudes
- Up to 12kts at ISA temperatures
- Up to 20kts at ISA +10 temperatures
- Increased range capability
- Up to 220 NM, HSC, NBAA IFR reserves, ISA temperature
- Up to 550 NM, Flap 15, NBAA IFR reserves, WAT limited take-off
- Improved hot day / high altitude takeoff performance
- Up to 4° C or 1,200 lbs for flaps 5 departures
- Up to 5° C or 1,270 lbs for flaps 15 departures
- Improved climb gradient
- 1/2 % 1st & 2nd segment climb gradient improvement
- Reduced fuel consumption
- Up to 5 % for high speed cruise missions
- Reduced direct operating costs
- Increased range reduces en-route technical stops
- 1800 - 2100 pound fuel savings per technical stop avoided
- Enhanced aircraft resale value
STC Installation supported by Cessna
- 5 year workmanship warranty on winglet installation
- 24/7 spares support and component warranty
- Existing airframe warranty unaffected by winglet installation
STC Kit supported by Winglet Technology
- 5 year transferable material warranty on winglet kit
- Starts on “return to service” date
As stated in Winglet Technology’s Purchase Agreement “The winglet retrofit kit does not include updates to the flight management computer software,” (TOLD). An updated version of CPCal which incorporates the performance benefits will be provided to those customers who have previously purchased CESNAV from Cessna.
The installation of Elliptical Winglets per the Winglet Technology’s STC will require a high degree of experience and understanding of the Citation X. The work performed to enable the installation of the winglet will require considerable modification to the existing wing structure to insure proper fit and alignment.
The installation will require, but is not limited to, the following actions:
- Removal of present wingtip, outboard rib and lighting
- Installation of a larger access door/panel in the outer wingtip area
- Installation of a new lower wing skin doubler, worked through existing access panels
- Out board wing structural reinforcement worked through existing access panels
- Installation of new wingtip rib
- Installation of new empennage mounted LED position and anti-collision lights
- Honeywell IAC Upgrade
- Final fit and installation of the new elliptical winglet
- Painting of effected area and new winglet
| Document | Size | Type |
|---|
| Aircraft Type | Model | |
|---|---|---|
| Citation X Series® | Citation X® | Contact Us |
| Name | Reference Number | Type | Status |
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