Cessna 441 Conquest II

The development of a new turboprop executive aircraft, designated Model 441, was announced by Cessna on November 15, 1974. The prototype first flew on August 26, 1975. By the time deliveries began, the aircraft had received the name Conquest II.

Cessna developed the Conquest II hoping to occupy a niche in the business aviation market between jet aircraft and piston-engine aircraft. However, in 1978, the company had to adjust its plans after one of the production aircraft crashed. Flights of the Conquest II were suspended to determine the causes of the incident and develop solutions to the problem.

Redesign and Re-certification

Cessna developed a new tail empennage design, and after re-certification, all previously built aircraft underwent the necessary modifications. This ensured the safety and reliability of the fleet, allowing the Conquest II to resume its market presence.

Design and Production

The Conquest incorporated the landing gear and wing of the Model 404 Titan aircraft, although the wingspan was increased with tip inserts. Its pressurized, air-conditioned cabin could accommodate one pilot and up to 10 passengers, with a luxury variant also available for four passengers.

Production of the Conquest II ceased in 1986. By the time manufacturing stopped, a total of 353 units had been sold, marking its presence in the executive turboprop market for over a decade.

Technical Specifications

Modification	Cessna 441
Wingspan, m	15.04
Aircraft length, m	11.89
Aircraft height, m	4.01
Wing area, m2	23.56
Empty weight	2631
Maximum takeoff weight	4468
Engine type	2 Turboprop engines Garrett TPE331-8-401S/402S
Power, hp	2 x 635
Maximum speed, km/h	595
Cruising speed, km/h	547
Practical range, km	4245
Practical ceiling, m	10670
Crew	2
Payload	10 passengers or 4 passengers in VIP class

Image and diagram gallery of the Cessna 441 Conquest II

Cessna 441 Conquest II	Cessna 441 Conquest II
Cessna 441 Conquest II	Cessna 441 Conquest II
Cessna 441 Conquest II