Specifications help a buyer decide whether an aircraft deserves a closer look, but they do not describe the condition or exact capability of a used aircraft. The figures below reflect ICON Aircraft's published A5 page as accessed in August 2026.
Published baseline specifications
- Seats: two
- Engine: Rotax 912 iS Sport, 100 hp
- Maximum speed: 95 KTAS
- Published range: 427 nautical miles with a 45-minute reserve
- Fuel: 91-octane automotive gasoline or 100LL aviation fuel, subject to applicable operating guidance
- Wingspan: 34.8 feet
- Length: 23 feet
- Cockpit width: 46 inches
- Maximum baggage: 60 pounds
Why maximum takeoff weight and useful load vary
ICON publishes configuration-dependent maximum takeoff weight of 1,510 to 1,570 pounds and estimated useful load of 430 to 490 pounds. A buyer must use the aircraft's approved documents and current weight-and-balance information rather than selecting the most favorable public number.
Published takeoff and landing distances
ICON lists runway and water figures under standard conditions at sea level, including a 640-foot runway takeoff roll and an 840-foot water takeoff roll for an aircraft at 1,510 pounds. Real performance changes with loading, surface, density altitude, wind, water state, technique, aircraft condition, and other factors.
Buyer questions behind every specification
- Which exact model, certification basis, and maximum takeoff weight apply?
- What equipment is installed and reflected in weight and balance?
- Which avionics, parachute, trailer, and accessory configuration is included?
- Are current operating limitations and supplements present?
- Does the planned mission leave a practical payload and performance margin?