DISCOVERY XL-2 PERFORMANCE

Maximum performance extracted from the most energy-efficient design. It's the XL-2's cornerstone. Start with a laminar flow wing designed by a Chief Engineer for Airbus, offering a unique blend of high speed cruise with forgiving slow-speed handling. Add the most sophisticated FADEC equipped engine to provide fuel savings unmatched by any competitor, and bolt on a modern low-inertia all-weather composite propeller with a stainless steel leading edge. Link push-rod controls throughout for ultimate control and you get an aircraft that delivers superior performance in every respect: 125knots cruise, 450 nautical mile range with IFR Reserve, 420lb payload with full fuel, and an average 5.5gph fuel burn. High speed. Low Cost.

Specifications & Performance PDF

PERFORMANCE

Stall Speed Vs1 (flaps up)
50 kts
Stall Speed Vso (flaps down)
44 kts
Rate of Climb (max. takeoff weight)
669 ft/min
Rate of  Climb  (10,000  ft)
194 ft/min (3.46 m/s)
Takeoff Ground Roll
1472 ft/449 m
Braked Roll (w/o Reverse)
--
Takeoff Distance over 50ft Obstacle
2564 ft/782 m
Landing Roll
708 ft/216 m
Landing Distance over 50ft Obstacle
1433 ft/437 m
Ceiling
12,500 ft/3810 m
Maximum Range Cruise Speed
120 kts/138 mph/222 km/h
Maximum Cruise Speed
125 kts/144 mph/232 km/h
Maximum Range
500 nmi/575 mi/926 km/w 45 min reserve

DESIGN WEIGHTS & CAPABILITIES

Fuel
AVGAS 100, 100 LL, RH-95/130
Fuel - Total Capacity
29.5 US Gal/111 L
Fuel - Total Usable
28 US Gal/106 L
Baggage Allowance
100 lbs/45 kg

EFFICIENCY & COST OF OPERATION

Fuel Efficiency
5.0 gph in the training environment
Ease of Maintenance
Easy access panels allow direct access to engine. Computer access allows for easy diagnostic and performance monitoring.
Ease of Use
Single lever power control
Range
500 nautical miles

WINDSPEED LIMITATIONS

Headwind
--
Tailwind
--
Crosswind
15 kts