Cessna

Cessna 441 Conquest II

The Cessell 441 Conquest II, introduced by Cessna in 1977, quickly became a benchmark for twin‑engine business aviation. Developed from the earlier Model 401, the Conquest II featured a longer, more slender fuselage and upgraded Pratt & Whitney Canada PT6A‑41 turboprop engines, delivering 850 shaft horsepower each. Certified for a maximum cruising altitude of 35,000 feet, it offered a true pressurised cabin that allowed passengers to travel comfortably across continental distances at speeds up to 340 knots, surpassing many jet competitors of its era. Approximately 400 airframes were produced until production ceased in 1990, a testament to its reliability and versatile performance.

Key design elements included a low‑drag wing with a 71‑inch flap system, advanced autopilot integration, and a fuel‑efficient fuel‑burn rate of roughly 220 pounds per hour. The aircraft’s robust airframe, combined with its twin‑engine redundancy, made it a popular choice for corporate fleets, air‑ambulance services, and government missions. Its enduring reputation for dependable, high‑speed transport cemented the Conquest II’s significance, influencing subsequent Cessna turboprop developments and reinforcing the brand’s standing in the executive aviation market.

Dimensions

Length
11.89 metre

Production & History

Units Produced
362
First Flight
1974
Service Entry
1977

Design & Classification

Country of Origin
Manufacturer
Cessna
Developer
Cessna
Operator
Skippers Aviation
Wikidata ID
Q1057265