Aviat Eagle II

The aerobatic biplane built for competitive performance.

Overview

Aviat United States 1977–Present $270,000

The Aviat Eagle II is a two-seat aerobatic biplane introduced in the 1990s. Designed for competition and recreational aerobatics, it emphasizes structural strength and agility. The aircraft remains popular in aerobatic communities.

Specifications

Units
Engine
1 × Lycoming AEIO-360-A1D
Engine type
Piston
Power
200 hp · 149 kW
Avionics
—
Wing tips
No winglets
Seats
2
Crew
—
Cabin width
—
Cabin height
—
Cabin length
—
Exterior length
17 ft 11 in  ·  5.46 m
Tail height
6 ft 6 in  ·  1.98 m
Fuselage diameter
—
Wing span
19 ft 11 in  ·  6.07 m
Baggage volume
—
Gross weight
—
Empty weight
—
Max takeoff weight
1,600 lb  ·  700 kg
Max landing weight
—
Max payload
550 lb  ·  250 kg
Fuel capacity
30 gal · 100 L · 100 kg (AvGas)
Max cruise speed
143 kt  ·  165 mph  ·  265 km/h
Maximum speed
—
Cruise speed
—
Approach speed
50 kt  ·  58 mph  ·  93 km/h
Range
380 nm  ·  440 mi  ·  700 km
Fuel burn
32.29 nm/gal  ·  15.80 km/L
Ceiling
1,700 ft  ·  518 m
Rate of climb
2,100 ft/min  ·  11 m/s
Takeoff distance
600 ft  ·  180 m
Landing distance
500 ft  ·  150 m
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Aviat Eagle II

Operational Context

Aviat Eagle II — aerobatic biplane

The Eagle II entered service in the early 1990s as an evolution of earlier Pitts designs. It features a steel tube fuselage and fabric covering. The aircraft was engineered for advanced aerobatic maneuvers.

A piston engine producing approximately 200 horsepower powers the aircraft. Cruise speed approaches 130 knots (241 km/h). Maximum takeoff weight exceeds 1,800 pounds (816 kg).

The Eagle II has competed in aerobatic championships and remains in production. Its handling characteristics suit experienced pilots. The aircraft continues a long tradition of American biplane aerobatic design.