Design Competition Origins
The Taylor JT-2 Titch emerged from John F. Taylor's entry in the 1964 Midget Racer Design Competition sponsored by Rollason Aircraft. Among 42 competing designs, Taylor's creation achieved second place by meeting strict requirements: maximum wing area of 65 square feet, weight limit of 750 pounds, and structural loads of ±6g for aerobatic capability. Taylor developed the Titch as an evolution of his earlier Taylor Monoplane, specifically targeting homebuilders who sought high-performance characteristics without factory production costs.
Tragic First Flight and Continued Legacy
The prototype G-ATYO made its maiden flight on January 4, 1967, at Southend Airport in Essex. Tragically, designer John Taylor perished in a crash of this same prototype aircraft on May 16, 1967, at Southend Airport, marking the first of what would become at least 20 recorded accidents involving the type through 2023, resulting in 12 total fatalities. Despite this setback, Taylor's family continued marketing the construction plans, with his wife initially taking over operations followed later by his son.
Construction Innovation and Homebuilder Appeal
Taylor's design philosophy emphasized construction simplicity for amateur builders while maintaining professional performance standards. The all-wood structure utilized minimal metal fittings, with innovative features like a tailplane attachment system requiring no metal hardware and a rear spar-to-fuselage connection using just four bolts. The wing employed a modified N.A.C.A. airfoil optimized for easy shaping by homebuilders while providing improved stall characteristics. Full-size rib plans eliminated the scaling errors common in amateur construction projects.
Engine Specifications and Performance
The prototype featured a Continental C85-12F, a four-cylinder horizontally-opposed air-cooled engine producing 85 horsepower. The design accommodated engines ranging from 65 to 100 horsepower, allowing builders flexibility in powerplant selection. Common alternatives included Continental O-200, Lycoming, Rotax, and Walter Mikron engines, though Volkswagen automotive conversions were specifically not recommended. With a 10-imperial-gallon fuel capacity and consumption of 4.2 gallons per hour, the Titch achieved a useful range for cross-country touring.
Performance Characteristics
The Titch delivered impressive performance figures for its weight class. Maximum cruise speed reached 160 mph at altitude, while stall speed with flaps deployed dropped to just 48 mph, providing a wide operating envelope. The maximum takeoff weight of 750 pounds, combined with an empty weight of 500 pounds, allowed for 250 pounds of useful load including fuel and pilot. The design's structural certification for full aerobatic flight expanded its appeal beyond simple cross-country touring to include sport aerobatic applications.
Global Homebuilder Community
By early 1991, approximately 500 sets of construction plans had been distributed worldwide, with 32 completed aircraft flying at that time. This number grew to 40 flying examples by 2011, with construction activity continuing into 2025. The international appeal attracted builders across the United Kingdom, United States, New Zealand, and Switzerland, creating a diverse global community of Titch operators and enthusiasts.
Enduring Design Relevance
The 50th anniversary of the first flight in 2017 prompted renewed interest in the design, with flight testing confirming the aircraft's continued relevance for modern homebuilders. The Taylor Titch represented a significant achievement in making high-performance aerobatic capability accessible to amateur builders through thoughtful design and comprehensive documentation. Today, construction plans remain available through enthusiast websites like taylortitch.co.uk, ensuring the design's availability for future generations of homebuilders seeking a proven combination of performance, economy, and construction simplicity.