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Landing gear extenders installed on a Cessna 140. Landing gear extenders are devices used on conventional or tailwheel-equipped aircraft.They move the wheels forward of the landing gear leg by 2-3 inches (5–8 cm).
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
Data from Jane's All The World's Aircraft 2003–2004 General characteristics Crew: one Capacity: five passengers Length: 28 ft 3 in (8.61 m) Wingspan: 36 ft 0 in (10.97 m) Height: 9 ft 3 + 1 ⁄ 2 in (2.832 m) Wing area: 175.5 sq ft (16.30 m 2) Empty weight: 2,176 lb (987 kg) Max takeoff weight: 3,600 lb (1,633 kg) Powerplant: 1 × Lycoming IO-540-AC1A naturally aspirated air-cooled flat-six ...
The Cessna 177B Cardinal uses a Lycoming O-360-A1F6D of 180 hp (130 kW). O-360-A1F6D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1F6 except that it is equipped with one Bendix D4LN-2021 impulse coupling dual magneto instead of incorporating two single magneto. [1] [2] O-360-A1G
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.
PW535B on a Cessna Citation V Encore+. The PW530A, rated at 2,887 lbf (12.84 kN), entered service in February 1997 on the Cessna Citation II Bravo, and the PW545 in July 1998 on the Cessna Citation Excel. The PW535 powered the Cessna Citation V Encore in September 2000, and was selected for the Embraer Phenom 300, first delivered in December 2009.
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The Cessna 140 was originally equipped with a Continental C-85-12 or C-85-12F horizontally opposed, air-cooled, four-cylinder piston engine of 85 hp (63 kW). The Continental C-90-12F or C-90-14F of 90 hp (67 kW) was optional, as was the 108 hp (81 kW) Lycoming O-235-C1 engine, an aftermarket installation authorized in the type certificate .
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