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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 .
This is the speed at which drag is minimised. For jet aircraft, "long-range cruise" speed (LRC) is defined as the speed which gives 99% of the maximum range, for a given weight. This results in a 3–5% increase in speed. [8] It is also a more stable speed than maximum range speed, so gives less autothrottle movement. [9]
Data from Jane's All The World's Aircraft 1961–62 General characteristics Crew: one Capacity: one passenger Length: 20 ft 0 in (6.10 m) Wingspan: 35 ft 0 in (10.67 m) Height: 6 ft 3 in (1.91 m) Wing area: 140 sq ft (13 m 2) Empty weight: 870 lb (395 kg) Gross weight: 1,400 lb (635 kg) Fuel capacity: 25 US Gallons (95 L) Powerplant: 1 × Continental C90 air-cooled flat four, 90 hp (67 kW ...
Design cruise, also known as the optimum cruise speed, is the most efficient speed in terms of distance, speed and fuel usage. [16] [17] [18] V cef: See V 1; generally used in documentation of military aircraft performance. Denotes "critical engine failure" speed as the speed during takeoff where the same distance would be required to either ...
Cessna 140 The Continental O-190 (Company designations C75 and C85 ) is a series of engines made by Continental Motors beginning in the 1940s. Of flat-four configuration, the engines produced 75 hp (56 kW) or 85 hp (63 kW) respectively.
Data from Jane's All the World's Aircraft 1993–94 General characteristics Crew: Two pilots (One pilot on II/SP) Capacity: Six to eight passengers Length: 47 ft 8 + 1 ⁄ 2 in (14.542 m) Wingspan: 52 ft 2 + 1 ⁄ 2 in (15.913 m) Height: 15 ft 0 in (4.57 m) Wing area: 342.6 sq ft (31.83 m 2) Airfoil: NACA 23000 Empty weight: 8,059 lb (3,656 kg) Max takeoff weight: 15,100 lb (6,849 kg) Fuel ...
The Cessna 400, marketed as the Cessna TTx, is a single-engine, fixed-gear, low-wing general aviation aircraft built from composite materials by Cessna Aircraft. [1] The Cessna 400 was originally built by Columbia Aircraft as the Columbia 400 until December 2007. [2] From 2013, the aircraft was built as the Cessna TTx Model T240.
The 1978 R182 has a sea-level climb rate of 1,140 ft/min (5.8 m/s) and a cruising speed (75% BHP) at 7,500 feet (2,300 m) of 156 kn (289 km/h; 180 mph) TAS at standard temperature. [ 9 ] The landing-gear retraction system in the Skylane RG uses hydraulic actuators powered by an electrically driven pump.