The X-Air
Welcome back to the days of affordable flying ! The X-Air is a fully featured, affordable light aircraft, developed over several years there are now more than 1200 flying world-wide. The French designed, Indian manufactured X-Air is the total package, it's best attributes are safety, performance and affordability; it comes with so many standard features that other aircraft just cant compete. The X-Air is without question the best selling Ultralight aircraft in Europe, England the US and Australia.

The Standard X-Air Features
- Quick build kit shipped in two wooden crates build time 100 to 200 hours MAX
- 2 person side by side seating 42 inches wide (wider than a 172)
- Full dual controls (stick, rudder and throttle)
- Steerable nosewheel
- Differential pilot toe operated brakes
- Full-body padded seats with adjustable headrests
- 4 point safety harness
- Excellent weather and wind protection - even without the doors
- Wrinkle-free heavy duty Dacron covering
- Composite nosepod
- Tricycle undercarriage with real shock absorber suspension
- Trailing link front suspension
- In-flight adjustable elevator trim
- Large composite instrument panel
- Full pre-wired electrical harness
- Engine mounts for all popular engines
- Airfoil section struts for wing and undercarriage supports
- Cromoly pilot protection cage
- Aircraft grade aluminium and hardware used throughout
- Stressed to +6 -4 airframe and +/- 9 undercarriage
- Dual fuel tanks, total capacity 59 litres
- Quick detach high lift wings
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| Steerable Nose wheel with Suspension | Rear Wheels with Suspension |





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TECHNICAL DATA |
Rotax 503 |
Rotax 582 |
Jabiru 2200 |
|
Empty weight basic (kg) |
230 kgs |
237 kgs |
262 kgs |
|
Max. empty weight equipped (kg) |
284 kgs |
281 kgs |
284 kgs |
|
Max empty weight equipped with parachute (kg) |
306.5 kgs |
303.5 kgs |
306.5 kgs |
|
Maximum weight (kg) |
490 kgs |
490 kgs |
490 kgs |
|
Fuel capacity (l) |
50 liters |
50 liters |
50 liters |
|
Engine |
Rotax 503 |
Rotax 582 |
Jabiru 2200 |
|
Cooling |
air |
water |
air/oil |
|
Carburetor |
2 |
2 |
1 |
|
Electronic ignition |
2 |
2 |
2 |
|
Power |
52hp at 6500 |
64hp at 6500 |
80hp at 3300 |
|
Engine Displacement |
496.7 cm3 |
580.3 cm3 |
2200cm3 |
|
Fuel mixture |
2% |
2% |
NA |
|
Fuel |
92 octane |
92 octane |
95 octane |
|
Wingspan |
9.80 m |
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|
Length |
5.65 m |
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|
Height |
2.55 m |
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|
Cockpit width |
1.16 m |
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|
Wings area |
16,00 m2 |
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|
Loading |
+6 -3 |
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|
PERFORMANCE |
Rotax 503 |
Rotax 582 |
Jabiru 2.2 |
|
Take off run |
140 m |
120 m |
120 m |
|
Climb rate fpm |
500 fpm |
690 fpm |
590 fpm |
|
Max Cruise speed at level |
54 knots |
60 knots |
60 knots |
|
Cruise speed economical |
45 knots |
50 knots |
50 knots |
|
Consumption economical lph |
14 lph |
12 lph |
9 lph |
|
Landing |
80 m |
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|
Sink rate mini |
690 fpm |
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|
Climb speed |
38 knots |
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|
Stall speed |
26 knots |
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|
VNE |
80 knots |
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|
Service ceiling |
12,000 feet |
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|
Glide ratio |
8:1 @ 38 knots |
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|
Distance to clear 15 m at landing |
140 m |
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|
Distance to clear 15 m at take off |
250 m |
220 m |
230 m |
