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Challenger Advanced Ultralight Sales and Service
Calmar, Alberta

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Performance Table

The following figures apply only to the newest Challengers and engines.
Performance of older airplanes and engines will not achieve these levels.

Challenger II
Performance
Long
Wing
Clip
Wing
Figures are for a typical Challenger II 503 Deluxe Package on wheels
with 170 lb occupants in standard sea level conditions. 
Performance will vary with density altitude, floats and load
Vne This never exceed speed is very high for ultralight aircraft. 100 mph 120 mph
Top Level Speed With a top speed of 96 mph and a stall of 24 mph, the long wing Challenger delivers an impressive high end without sacrificing friendly, low speed approaches and handling. A 4 to 1 speed range is unusually wide, few general aviation aircraft can exceed 2.8 to 1. 96 mph 100 mph
Cruise Speed Low drag tandem seating, an engine tucked out of the slipstream, and attention to streamlining result in an unusually high cruise speed. Few if any designs can deliver this speed with such an economical engine. 85 mph
(5800 RPM)

85 mph
(4000 RPM)

90 mph
(5800 RPM)

40 mph
(4000 RPM)

Stall Speed
flaperons extended
 
The Challenger's large wing area and low weight result in a very low speed and exceptionally gentle stall. This is key to short field performance and is an important safety feature. It also contributes to the long wing Challenger's unequalled soaring capability. 24 / 28 mph
(solo / dual)
32 / 37 mph
(solo / dual)
Rate of Climb
(solo/dual)
The rate of climb is very strong by any standard. This together with a climb speed in the low 40s means the plane goes forward quite slowly while going up quite quickly, resulting in a helicopter-like angle of climb! Getting out of short fields (and lakes) is a snap. 1,100 / 750 fpm
(solo / dual)
1,000 / 650 fpm
(solo / dual)
Service Ceiling
(solo/dual)
Most people think of ultralights as only flying low, near the ground. The Challenger goes high too, up into oxygen country. The heated cabin takes the nip out of the thin air found at these exalted altitudes. 14,000' / 12,500'
(solo / dual)
14,000' / 12,500'
(solo / dual)
Glide Ratio The glide ratio of Challengers is excellent by powered aircraft standards. From 5000 feet you can glide 11 miles with the engine off! Key to the unique soaring capability of the long wing are the low drag tandem seating and low wing loading, which result in a low sink rate, plus the low stall speed, which permits very small diameter turns in the thermal's core. 11 to 1 9 to 1
Minimum Sink
(solo/dual)
Engine off, the long wing Challenger drifts down at an unusually gentle rate, taking a full quarter hour to reach the ground from 5000 feet. Apart from aiding soaring, this low sink rate has obvious safety benefits. The clip wing sinks faster than the long wing but is still very gentle by General Aviation standards. 350/450 fpm
(solo / dual)
500/600 fpm
(solo / dual)

Takeoff
& Landing
The large wing and light weight together with the high power-to-weight ratio give great STOL performance. 75-200 feet 125-250 feet
Maximum
Crosswind
The crosswind capability of the Challenger actually equals or exceeds that of many General Aviation aircraft. As an example, the Cessna 172 has a crosswind capability of 17 mph. Puddlejumper amphibious floats have a steerable nose wheel which allows Challengers so equipped to retain their crosswind capabilities. 20 mph 30 mph
Fuel
Consumption
Few two-seat aircraft are as miserly on fuel. Challengers can use auto gas (87 octane), avgas (100LL) or marina gas (87-89 octane), which may be intermixed. Most owners prefer regular car gas to minimize costs. 2.0 - 4.5
US gph
2.0 - 4.5
US gph
Fuel Economy These figures assume no wind - Your Mileage May Vary - depending on how heavy you are on the gas. Remember also, that airplanes fly in straight lines, so this is a lot more miles per gallon than you get in a car. 21-25 mpg 21-25 mpg
Endurance
no reserve
Endurance depends of course on how fast you want to cruise - low and slow for sightseeing or blistering along to get somewhere soon. Our Canadian Challenger's standard fuel tank is 10 US gallons. An optional tank holding 17 US gallons provides greater endurance. 2.2 - 5.0 hrs
(10 US Gal)

3.8 - 8.5
hrs
(17 US Gal)
2.2 - 5.0
(10 US Gal)

3.3 - 7.5
hrs
(17 US Gal)
Range
no wind
no reserve
Range varies with the size of your fuel tank, how fast you cruise, how much reserve you allocate for contingencies, and of course the wind. Non-stop flights of over 300 miles have been made but it's actually more fun to make intermediate pit stops and be greeted by groundlings as if you're a movie star in a Ferrari! 200 sm
(10 US Gal)

300 sm
(17 US Gal)
200 sm
(10 US Gal)

300 sm
(17 US Gal)

Figures are for a typical Challenger II 503 Deluxe Package on wheels
with 170 lb occupants in standard sea level conditions. 
Performance will vary with density altitude, floats and load

For the Challenger II 582 Premium Package takeoffs are 1/3 to 1/2 shorter, climb is 50 to 100% faster, and, although you can climb faster, fuel consumption at any given speed is about 20% lower.

Personal experiences

  • Specifications for airplanes are generally calibrated for ICAO standard Conditions (Sea Level, 15 ºC, Standard Adiabatic Lapse Rate, etc.) 

  • Real-world experience in any airplane  can vary substantially with real density altitude.  

  • We're happy to report that the 503 Challenger does very well at our Density Altitudes out west at higher elevations.  Here are some real measurements for C-IJBN on amphibs at Wetaskiwin:

    • 2508' ASL, 12 ºC, 5 Knot wind,  C-IJBN (503), 60x44 GSC Prop, with Amphib PuddleJumpers, at close to full gross, off grass: 5' AGL and climb attitude at 55mph @ just over 600 feet total distance.  Down and stopped in less with no brakes.

    • 2508' ASL, -20 ºC, Calm Winds, C-IJBN (503), 60x44 GSC Prop, on wheels, solo, half fuel. 1500' AGL by the far threshold (3500') at 51-55 mph climb speed!

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