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The 5 U.S. gallons (19 L; 4.2 imp gal) fuel tank is made from aluminium. In flight steering is accomplished via foot pedals, or optionally a control stick, that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates gas strut suspension.
The aircraft has a maximum gross weight of 300 kg (661 lb). It features a 34 m 2 (370 sq ft) Ram Air brand parachute-style wing made from rip-stop nylon, two-seats-in-side-by-side configuration, tricycle landing gear and a single 50 hp (37 kW) Rotax 503 engine mounted in pusher configuration. [2] The aircraft carriage is built from metal tubing.
The CH-47JA, introduced in 1993, is a long-range version of the CH-47J, fitted with an enlarged fuel tank, an AAQ-16 FLIR in a turret under the nose, and a partial glass cockpit. [ 122 ] [ 123 ] Both versions are built under license in Japan by Kawasaki Heavy Industries , who produced 61 aircraft by April 2001.
The main landing gear incorporates spring rod suspension. The aircraft has a typical empty weight of 250 lb (110 kg) and a gross weight of 900 lb (410 kg), giving a useful load of 650 lb (290 kg). With full fuel of 5 U.S. gallons (19 L; 4.2 imp gal) the payload for the pilot, passenger and baggage is 620 lb (280 kg). [1]
The Cirrus Vision SF50, also known as the Vision Jet, is a single-engine very light jet designed and produced by Cirrus Aircraft of Duluth, Minnesota, United States.. After receiving deposits starting in 2006, Cirrus unveiled an aircraft mock-up on 28 June 2007 and a prototype on 26 June 2008.
A powered parachute, often abbreviated PPC, and also called a motorized parachute or paraplane, is a type of aircraft that consists of a parafoil with a motor and wheels. The FAA defines a powered parachute as a powered aircraft comprised of a flexible or semi-rigid wing connected to a fuselage so that the wing is not in position for flight ...
Data from ICON Aircraft General characteristics Crew: one Capacity: one passenger Length: 23 ft (7.0 m) Wingspan: 34.8 ft (10.6 m) Height: 8.1 ft (2.5 m) Empty weight: 1,080 lb (490 kg) Gross weight: 1,510 lb (685 kg) Fuel capacity: 20 US gal (76 L) Powerplant: 1 × Rotax 912 iS fuel-injected, air and liquid cooled four cylinder aircraft engine, 100 hp (75 kW) Propellers: 3-bladed composite ...
Fuel capacity: 300 l: ... Airborne operations demonstrating full deployment of the parachute system and underslung BTR-D. ... Armed Forces of Ukraine tank destroyer ...