Quote for Aviat Eagle Ii Parts

Model No: Aviat Eagle Ii

Category: Rotary Wing Aircraft

Aircraft Type: Aerobatic

Manufacturer: Aviat Aircraft

Country: United States

Manufactured: 1977 to: Present

Engine: 1 X Lycoming AEIO-360-A1D

Power: 200 horse[Power]

Max Cruise Speed: 99 knots - 183 Km/h

Fuel Economy: 32.29 nautical mile / gallon - 15.797 kilometres / litre

Take Off Distance: 183 metre - 600.39 feet

Landing Distance: 152 metre - 498.68 feet

Max Tak eOff Weight: 3,479 Kg - 7,670 lbs

Max Payload: 251 Kg - 553 lbs

Seats Economy/General Class: 2 seats

Seats Business Class: 0

Seats First Class: 0

The Aviat Eagle II is an aerobatic biplane aircraft that was designed by Frank Christensen and is currently produced by the American manufacturer Aviat Aircraft Inc. The Eagle II is a kit form aircraft, meaning that it is intended for homebuilding. The aircraft features a box truss fuselage design and single bay staggered biplane wings. Within the Eagle II, a pilot and one passenger may be situated in tandem within a bubble canopy. The Eagle II uses a variety of materials for its structure, such as a chromoly steel fuselage and tail, aluminum skinned forward fuselage, fabric tail covering, and Sitka spruce wood wing structure.

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The Aviat Eagle II features a Lycoming AEIO-360-A1D engine configuration, capable of producing 200 horsepower to travel at a maximum cruise speed of 99 knots. The fuel engine capacity is 27 US gallons, providing for a maximum travel range of 380 nautical miles with a fuel economy averaging at 32.29 nautical miles per gallon. Currently, four variants of the aircraft exist, these being the Christen Eagle I, Christen/Aviat Eagle II, Christen Super Eagle I 540, and the Christen Super Eagle II.

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