X-Air Flap Model (Falcon)
The X-Air Flap, also known as the X-Air Falcon, is an enhanced version of the original X-Air design, built for improved performance, comfort, and control. Incorporating in-flight adjustable flaps, a streamlined profile, and refined aerodynamics, the Flap model delivers better climb rates, slower stall speeds, and shorter takeoff and landing distances—making it an ideal choice for both training and recreational flying.
With its fully enclosed, spacious cockpit, side-by-side seating, and comprehensive instrumentation, the Falcon provides a comfortable flying experience in all weather conditions. The addition of flaps increases control authority at low speeds, making approaches and landings more stable and forgiving—especially useful for newer pilots or short-field operations.
Built to the same rugged standards as the original X-Air, the Falcon features:
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In-flight adjustable flaps
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Fully enclosed cabin with improved weather protection
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Wide 42-inch cockpit with dual controls
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Tricycle landing gear with shock-absorbing suspension
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Lightweight composite nose pod for better aerodynamics
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Aircraft-grade aluminium frame with high-durability Dacron skin
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Compatible with popular engines including the Rotax 582, Rotax 912, and Jabiru 2200
With over 1,200 X-Air aircraft flying worldwide, the Flap/Falcon variant stands out as a practical, safe, and affordable solution for pilots who value reliability without sacrificing performance.
Whether you’re flying for fun, building hours, or looking for a dependable training aircraft, the X-Air Flap model offers unmatched value and versatility in the light sport and ultralight categories.
Standard Features of the X-Air
The X-Air is packed with features that make it one of the most complete and affordable light sport aircraft on the market today. Every aircraft is delivered as a quick-build kit, thoughtfully engineered for simplicity, safety, and performance.
✈️ Airframe & Build
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Supplied as a quick-build kit in two wooden crates
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Estimated build time: 100–200 hours maximum
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Stressed to +6 / –4 G airframe and ±9 G undercarriage
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Quick-detach, high-lift wings for easy storage and transport
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Aircraft-grade aluminium and hardware throughout
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Cromoly steel pilot protection cage
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Composite nose pod and large composite instrument panel
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Wrinkle-free, heavy-duty Dacron fabric covering
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Airfoil section struts for wings and undercarriage
👨✈️ Cockpit & Seating
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Spacious side-by-side 2-seat configuration (42″ wide – wider than a Cessna 172)
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Full dual controls: stick, rudder pedals, and throttle
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Full-body padded seats with adjustable headrests
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Four-point safety harnesses for both occupants
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Excellent weather and wind protection – even without doors
🛫 Landing Gear & Handling
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Tricycle undercarriage with genuine shock absorber suspension
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Trailing link front suspension for smoother landings
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Steerable nosewheel for easy ground handling
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Differential toe-operated brakes (pilot side)
⚙️ Systems & Compatibility
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In-flight adjustable elevator trim
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Pre-wired electrical harness included
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Engine mounts available for all popular engine options
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Dual fuel tanks with a total capacity of 59 litres
| TECHNICAL DATA FLAP MODEL | Rotax 582 | Jabiru 2.2 |
|---|---|---|
| Basic empty weight | 237 kgs | 262 kgs |
| Max. empty weight equipped (kg) | 281 kgs | 284 kgs |
| Max. empty weight equipped with parachute (kg) | 303.5 kgs | 306.5 kgs |
| Maximum weight (kg) | 490 kgs | 490 kgs |
| Fuel capacity (l) | 55 | 55 |
| Engine | Rotax 582 | Jabiru 2.2 |
| Cooling | water | air/oil |
| Carburetor | 2 | 1 |
| Electronic ignition | 2 | 2 |
| Power | 64hp at 6500 | 80hp at 3300 |
| Displacement | 580.3 cm3 | 2200 cm3 |
| Fuel mixture | 2% | NA |
| Fuel | 92 octane | 95 octane |
| Wingspan | 9.40m | |
| Length | 5.65 m | |
| Height | 2.55 m | |
| Cockpit width | 1.16 m | |
| Wings area | 14.32 m2 | |
| Loading | 3 | |
| PERFORMANCE | Rotax 582 | Jabiru 2.2 |
| Take off run (m) | 120 | 100 |
| Climb rate (m/s) | 500 fpm | 885 fpm |
| Max cruising speed at level | 62 knots | 70 knots |
| Cruise speed economical | 50 knots | 60 knots |
| Consumption economical (l/h) | 12 lph | 9 lph |
| Landing Distance | 80 m | 80 m |
| Sink rate | 685 fpm | 685 fpm |
| Climb speed | 43 knots | 43 knots |
| Stall speed | 28 knots | 28 knots |
| VNE | 83 knots | 83 knots |
| Service ceiling | 12,000 feet | 12,000 feet |
| Glide ratio | 8:1 @ 37 knots | 8:1 @ 37 knots |
| Distance to clear 15 m at landing | 140 m | 140 m |
| Distance to clear 15 m at take off | 220 m | 165 m |