Ad
related to: cessna 402 wingspan parts breakdown chart
Search results
Results from the WOW.Com Content Network
The FAA granted certification to the Cessna 401 in October 1968 and the 402 in January 1969. [4] The original Cessna 402 was introduced in 1967. A version without the large cargo door called the Cessna 401 was produced at the same time. [3] In 1969, the 402's nose was stretched for added baggage space. This model was renamed the 402A.
Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1
You are free: to share – to copy, distribute and transmit the work; to remix – to adapt the work; Under the following conditions: attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made.
Cessna (/ ˈ s ɛ s n ə / [4]) is an American brand of general aviation aircraft owned by Textron Aviation since 2014, headquartered in Wichita, Kansas.Originally, it was a brand of the Cessna Aircraft Company, an American general aviation aircraft manufacturing corporation also headquartered in Wichita.
Data from Jane's All The World's Aircraft 1965-66 General characteristics Crew: two Capacity: four to six passengers Length: 33 ft 5 + 1 ⁄ 2 in (10.20 m) Wingspan: 39 ft 10 + 1 ⁄ 4 in (12.15 m) Height: 11 ft 6 + 1 ⁄ 2 in (3.52 m) Wing area: 200 sq ft (19 m 2) Empty weight: 3,820 lb (1,733 kg) Max takeoff weight: 6,500 lb (2,948 kg) Fuel capacity: 170 US gal (140 imp gal; 640 L) standard ...
Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 only as published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.
The F406 Caravan II is a twin turboprop engined, fourteen-seat low-wing monoplane of conventional aluminium (airframe) and steel (engine internal parts, exhaust, landing gear) construction. It is a development of the Cessna 404 Titan with two Pratt & Whitney PT6A turboprop engines.
The pressurized 414 was developed to appeal to owners of unpressurized, twin-engined aircraft, and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear.
Ad
related to: cessna 402 wingspan parts breakdown chart