AkroTech Aviation G-222

Fixed Wing Single Engine

Aircraft Information

ICAO Code
CP22
Manufacturer
AkroTech Aviation
Model
G-222
Aircraft Type
Fixed Wing Single Engine
Primary Role
Aerobatic

Technical Data

Engine Type
Inline
Engine Model
AEIO-360-A1E
Production Years
1995-2020s
Units Produced
At least 26
First Flight
1995
Notable Operators
Wayne Handley

The Giles G-222 represents the pinnacle of unlimited aerobatic aircraft design, engineered for extreme-performance competition and demonstration flying. First flown in 1995, it is a tandem two-seat, low-wing monoplane constructed entirely from carbon fiber composite materials. Powered by a single Lycoming AEIO-360-A1E engine producing 235 horsepower, the aircraft achieves a roll rate exceeding 420 degrees per second and can withstand loads of +/-10g. At least 26 examples were built by AkroTech Aviation in Troutdale, Oregon.

Design Excellence

Richard Giles conceived the G-222 as an evolution of his single-seat G-200 design, creating what would become one of the most capable aerobatic aircraft ever built. The transition to a two-seat configuration opened new possibilities for instruction and passenger flights while maintaining the extreme performance characteristics that defined Giles aircraft. The all-composite construction represented cutting-edge technology in the mid-1990s, when most aerobatic aircraft still relied on traditional aluminum structures.

Manufacturing and Production

AkroTech Aviation manufactured the G-222 as a kit aircraft from their facility in Troutdale, Oregon, beginning production in the mid-1990s. The company produced at least 26 examples through the early 2020s, with each aircraft representing hundreds of hours of precise composite fabrication. A parallel production line emerged in France, where Avions Mudry manufactured a slightly modified version designated as the CAP 222, expanding the design's international reach.

Performance Characteristics

The G-222's performance envelope places it among the most capable aerobatic aircraft ever constructed. With a maximum takeoff weight of 1,600 pounds for cruise operations and 1,400 pounds for aerobatic flight, the aircraft demonstrates remarkable agility. The Lycoming AEIO-360-A1E engine, specifically designed for inverted flight operations, provides 235 horsepower through a four-cylinder, fuel-injected configuration. This powerplant enables a cruise speed of 161 mph while maintaining a never-exceed speed of 258 mph.

Record-Breaking Achievements

The aircraft's capabilities were dramatically demonstrated in 1999 when airshow performer Wayne Handley established a world record by completing 78 consecutive flat spins in his G-222. This achievement showcased not only the aircraft's structural integrity but also its exceptional controllability during extreme maneuvers. The record highlighted the design's ability to maintain control authority even during the most demanding aerobatic sequences.

Operational Flexibility

Dual fuel system configurations distinguish the G-222 from conventional aircraft. In cruise configuration, the aircraft carries 58 gallons of fuel, providing substantial range for cross-country flights. For aerobatic operations, fuel capacity reduces to just 10 gallons, lowering weight and minimizing fuel movement during inverted flight. This system consumes between 40-60 liters per hour depending on flight regime, with aerobatic flying typically requiring higher fuel flows.

Safety Considerations

Despite its advanced design, the G-222 has experienced several fatal accidents that highlight the inherent risks of extreme aerobatic flight. On August 28, 2015, a G-222 crashed at Stewart International Airport near New Windsor, New York, when the tail separated during an ascending maneuver, killing the pilot. Additional fatal accidents occurred near Wasilla, Alaska, in May 2019 during takeoff, and near Ulm, Germany, in October 2022, claiming two lives.

Technical Innovation

The G-222's carbon fiber construction provides exceptional strength-to-weight ratio while enabling the precise control responses demanded by unlimited aerobatic competition. The tandem seating arrangement optimizes the aircraft's center of gravity while providing excellent visibility for both occupants. With a stall speed of just 66 mph, the aircraft maintains controllability across an unusually wide speed range, from near-stall conditions to its 258 mph maximum velocity.

Current Status

While production continued into the early 2020s, the current operational status of AkroTech Aviation remains unclear based on available information. The G-222 design represents a significant achievement in composite aerobatic aircraft engineering, demonstrating that carbon fiber construction could successfully withstand the extreme loads imposed by unlimited aerobatic flight. The aircraft's influence extends beyond its production numbers, having established new benchmarks for aerobatic aircraft performance and construction techniques that continue to influence modern designs.