This is a pilot's operating handbook
This handbook contains the required information for safe operation of the Express, including descriptive data, performance charts, and weight‑and‑balance procedures. It follows the GAMA specification and is organized into sections covering general information, engine and propeller details, fuel capacities, and airspeed terminology.
The manual also explains revision procedures, supplemental equipment approvals, and provides definitions for meteorological and power terminology needed by pilots and owners of this experimental aircraft.
| Engine | Lycoming IO-360 C1C6 |
|---|---|
| Propeller | Hartzell 2‑Blade 7666A‑2, HCE2YR Hub |
| Fuel Type | 100LL Av gas |
| Main Usable Fuel Capacity | 46.0 US gallons |
| Auxiliary Wing Tank Capacity | 34.0 US gallons |
| Oil Capacity | 8 US quarts |
| Maximum Take‑off Weight | 2,895 lbs |
| Maximum Landing Weight | 2,895 lbs |
| Cabin Height | 44.5 inches |
| Cabin Width (front) | 45 inches |
| Cabin Width (rear) | 42.75 inches |
| Baggage Compartment Volume | 20.6 cu ft |
| Wing Loading (200 HP) | 21.1 lbs/ft² |
| Power Loading (200 HP) | 14.5 lbs/hp |
| Useful Load (200 HP) | 1,195 lbs |
The Express is equipped with a Lycoming IO‑360 C1C6 engine.
The maximum take‑off weight is 2,895 lb.
The main tank holds 46.0 U.S. gallons of usable fuel.