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The Aerobat retained the normal 150's 100 hp (75 kW) Continental O-200 engine, but structurally it was stronger than the normal 150K, being rated for load factors of +6.0/−3.0 g (vs. +4.4/–1.76 g for the normal 150K) and having higher limits for its maneuvering and never-exceed speeds.
The flight experienced a mid-air collision with a Cessna 150. A major factor in the accident was the position of the sun at the time. December 1, 1974 92 0 0 TWA Flight 514: Mount Weather, near Bluemont: Virginia: Boeing 727-200: The aircraft crashed during an unstabilized approach when the aircraft descended prematurely. December 1, 1974 3 0 0
The Cutlass RG sold for about US$19,000 more than the standard 172 and featured a variable-pitch, constant-speed propeller and a more powerful Lycoming O-360-F1A6 engine of 180 horsepower (130 kW), giving it an optimal cruise speed of 140 knots (260 km/h), compared to 122 knots (226 km/h) for the contemporary 160 horsepower (120 kW) 172N or ...
For an aircraft equipped with a constant speed propeller, this is the most direct indication of the engine's operating power. A fully open throttle would show a manifold pressure roughly equal to the ambient air pressure, i.e. full power; note that the maximum therefore changes with altitude unless the engine is equipped with a turbocharger or ...
Prototype single piston engine monoplane utility airplane Cessna 150: 1957 23,839 Single piston engine monoplane utility airplane Cessna 152: 7,584 Single piston engine monoplane utility airplane Cessna 160: 1962 1 Prototype single piston engine monoplane utility airplane Cessna 162 Skycatcher: 2006 275 Single piston engine monoplane utility ...
150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Provisions for a controllable-pitch propeller and 25-degree spark advance. [2] O-320-A1B 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as A1A but with straight riser in oil sump and -32 carburetor. [4] O-320-A2A
The C90 was introduced in 1947 as a follow-on to the A65, which had been in production since 1939. [7] [8] Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the Piper J-3 Cub and PA-11 Cub Special, [9] Aeronca 7AC, [3] and Luscombe 8A. [10] The engine was developed from the earlier O-190 by increasing the stroke 1 ⁄ 4 inch.
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines.Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).
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