CITATION ASCEND
Cessna Citation Ascend · Performance Data
Overview
This document provides performance data for the Cessna Citation Ascend, a business jet designed for efficiency and high performance. It details the aircraft's specifications, including engine performance, cabin dimensions, weight limits, and operational capabilities. The information is intended for pilots and operators to understand the aircraft's performance characteristics under standard conditions. Key features include advanced avionics, fuel-efficient engines, and customizable interiors, making the Citation Ascend suitable for modern business travel.
- Max Takeoff Weight: 20,500 lb (9,299 kg)
- Max Cruise Speed: 441 ktas (817 km/h)
- 4 Passenger Range: 1,940 nm (3,593 km)
- Takeoff Field Length (MTOW): 3,800 ft (1,158 m)
- Time to Climb to FL430: 26 minutes
Document
Source
Originally published by cessna.txtav.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Performance Data
- Year
- 2025
- Pages
- 2
- File size
- 235 KB
- Publisher
- cessna.txtav.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 1,940
- Length (ft)
- 18.5
- Engine model
- (2) PW545D
- Max speed (kt)
- 441
- Empty weight (lb)
- 13,060
- Max takeoff weight (lb)
- 20,500
Performance
- Takeoff distance (ft)
- 3,800
Weight & balance
- Useful load (lb)
- 900
- Basic empty weight (lb)
- 13,060
- Max takeoff weight (lb)
- 20,500
Most owners only have the POH. Here's the essential set for the Cessna Citation Ascend.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Cessna Citation Ascendmanuals & documents
- CASR PART 91 | PLAIN ENGLISH GUIDE | VERSION 5.1Other Documents
- Flight Standardization Board ReportPilot's Operating Handbook
- Textron 2023 Fact BookPilot's Operating Handbook
- FINAL AGREEMENT 3.25.22 DISTRIBUTOR SETTLEMENT AGREEMENTChecklist
- Cessna Citation Ascend ChecklistChecklist
- Commission Regulation (EC) No 29/2009 – Data Link Services ExemptionsType Certificate
- Airworthiness Directives for the Cessna Citation AscendAirworthiness Directives
- Aviation PhysiologyTraining Manual
- Airplane Flying Handbook (FAA-H-8083-3C)Training Manual
In this document
Cabin Specifications
The cabin of the Cessna Citation Ascend offers a height of 60 inches (optional 68 inches), a width of 66 inches, and a length of 18 feet 6 inches (5.64 meters). This spacious interior is designed for comfort and functionality.
Weights
The maximum takeoff weight (MTOW) for the Citation Ascend is 20,500 pounds (9,299 kg). The basic operating weight is 13,060 pounds (5,924 kg), allowing for a full fuel payload of 900 pounds (408 kg).
Powerplant
The aircraft is powered by two Pratt & Whitney Canada PW545D engines, each producing 4,213 pounds of thrust (18.74 kN). This setup enhances the aircraft's performance and efficiency.
Performance Metrics
The Citation Ascend achieves a maximum cruise speed of 441 knots true airspeed (ktas) or 817 km/h. It has a range of 1,940 nautical miles (3,593 km) based on a four-passenger mission with NBAA IFR reserves. The takeoff field length at maximum takeoff weight is 3,800 feet (1,158 meters), and it can climb to FL430 in 26 minutes.
Full document text
TRANSCEND THE EXTRAORDINARY C I T A T I O N A S C E N D CITATION ASCEND In the new Citation Ascend™ jet, the sky is your competitive edge. With every detail considered and designed to take your business further, this aircraft is perfect for keeping you ahead of the curve. With the Citation Ascend™ jet, the best is just the beginning. CONTACT YOUR TEXTRON AVIATION REPRESENTATIVE U . S . + 1 . 8 4 4 . 4 4 .T X TAV | I N T E R N AT I O N A L + 1 . 3 1 6 . 5 1 7. 8 2 7 0 | C E S S N A . C O M © 2025 Textron Aviation Inc. All rights reserved. Cessna® & Design, Citation® and Citation Ascend™ are trademarks or service marks of Textron Aviation Inc. or an affiliate and may be registered in the United States or other jurisdictions. Garmin®, G5000®, LinxUs® and Pratt & Whitney® are trademarks and/or service marks of their respective owners. Scan to explore more. THE EPITOME OF HIGH PERFORMANCE Travel smarter for your business and the planet with new Pratt & Whitney® Canada PW545D engines featuring greater fuel efficiency, improved range and increased thrust. Reduce pilot workload with new autothrottles, allowing you to operate smoothly, comfortably and with greater peace of mind. STATE-OF-THE-ART AVIONICS Step into a flight deck that will make any pilot feel on top of the world. With Garmin® G5000® avionics, you are fully in control of your journey. BEST-IN-CLASS MAINTENANCE INTERVALS Longer maintenance intervals mean less downtime and greater savings. LinxUs® Air diagnostic technology transmits fault data during flight, providing operators with early and advanced troubleshooting information. CUSTOMIZED INTERIORS The cabin is your canvas, so personalize it with eco-friendly, refined interiors. Enjoy a flat floor or optional dropped aisle and relax with quiet cabin technology. *Performance data based on standard conditions with zero wind. Field performance assumes a level, dry, paved runway, sea level at MTOW. Range based on a four-passenger mission at HSC with NBAA IFR reserves (100 nm alternate). I N T E R I O R Cabin Height (Optional) 60 in (68 in) 1.52 m (1.73 m) Cabin Width 66 in 1.68 m Cabin Length 18 ft 6 in 5.64 m W E I G H T S Max Takeoff Weight 20,500 lb 9,299 kg Basic Operating Weight 13,060 lb 5,924 kg Full Fuel Payload 900 lb 408 kg P OW E R P L A N T Manufacturer Pratt & Whitney Canada Model (2) PW545D Output 4,213 lb ea 18.74 kN ea M A X PA S S E N G E R S 12 P E R F O R M A N C E * Max Cruise Speed 441 ktas 817 km/h 4 Passenger Range 1,940 nm 3,593 km Takeoff Field Length (MTOW) 3,800 ft 1,158 m Time to Climb (Direct) FL430 in 26 min