Search results
Results from the WOW.Com Content Network
Data from Aviat website General characteristics Crew: one Capacity: one passenger Length: 22 ft 7 in (6.88 m) Wingspan: 35 ft 6 in (10.82 m) Wing area: 183 sq ft (17.0 m 2) Empty weight: 1,275 lb (578 kg) on wheels Gross weight: 2,200 lb (998 kg) on wheels and floats Fuel capacity: 50 US gallons (190 litres) Powerplant: 1 × Lycoming O-360-A1P four cylinder, four stroke piston aircraft engine ...
The Advanced Aviation Husky, Hi-Nuski and Coyote are a family of American ultralight aircraft that was designed and produced by Advanced Aviation. The aircraft was supplied as a kit for amateur construction and introduced in 1978.
VO-435-A1B (military designation O-435-6) Vertically-mounted engine model for helicopters, with a dry sump oil system and a modified accessory section. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 391 lb (177 kg) and fitted with a Marvel MA-4-5 or MA-4-5AA carburetor.
AIO-320-A1B 160 hp (119 kW) at 2700 rpm, Minimum fuel grade 91/96 or 100LL avgas, compression ratio 8.50:1. Same as the A1A but with one impulse coupling magneto. [3] AIO-320-A2A 160 hp (119 kW) at 2700 rpm, Minimum fuel grade 91/96 or 100LL avgas, compression ratio 8.50:1. Same as the A1A but with provision for a fixed-pitch propeller. [3]
Discover the latest breaking news in the U.S. and around the world — politics, weather, entertainment, lifestyle, finance, sports and much more.
Jim Jim, a Bulldog, wears a head decoration during the 149th Annual Westminster Kennel Club Dog Show at the Jacob Javits Convention Center in New York City, U.S., February 10, 2025.
President Donald Trump on Thursday took executive action to address FAA hires and aviation safety after an Army Black Hawk helicopter collided with a passenger jet in D.C.
fuel-injected, 722 cubic inches (11.8 litres), 400 hp (298 kW), same as -A1B except has a dual magneto, certified 30 December 1976 [2] IO-720-B1A fuel-injected, 722 cubic inches (11.8 litres), 400 hp (298 kW), same as -A1A except for top exhaust cylinders and offset exhaust valve shroud tubes, certified 4 November 1965 [ 2 ]