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Quad City Challenger II

qc-chal2
Challenger II


A two place version of the Challenger. This is a 2 seat high wing pusher microlight with a semi-enclosed cabin with a factory built airframe. All U.S. tubing. 10-15 minute set up time.

The Challenger II features two-seats and a 31.5 ft wingspan long wing. The Challenger II qualifies as a 51% kit for Experimental - Amateur-Built, can be flown with Sport Pilot Permit, and qualifies as Light Sport Aircraft.

In 2010 quick-build kits were from US$11,940 to US$16,035 ex engine with engine options being the Rotax 447, 503, 582 and HKS 700E.

The Challenger II Special is a 2 place with a 26 ft wingspan for quick roll rate and up 95 mph cruise speed.
With a 30 mph cross-wind capability and 300 ft take-off roll (average dual), the Challenger II Special qualifies as a 51% kit for Experimental - Amateur-Built, can be flown with Sport Pilot Permit, and qualifies as Light Sport Aircraft.

chal2spec
Challenger II Special


In 2010 quick-build kits were from US$13,165 to US$16,035 ex engine and engine options were the Rotax 447, 503, 582 and HKS 700E.

 

A version released in the UK circa 1998 was revised by Mike Whittaker.
 
QC-Chal2-02
Challenger II
 

 

Challenger II
Engine: Rotax 447, 42 hp
HP range: 40-52
Height: 6 ft
Length: 19 ft
Wing span: 31 ft
Wing area: 175 sq.ft
Weight empty: 310 lb
Gross: 800 lb
Fuel cap: 5 USG
Speed max: 85 mph
Cruise: 57 mph
Range: 150 sm
Stall: 25 mph
ROC: 600 fpm
Take-off dist: 200 ft
Landing dist: 200 ft
Service ceiling: 12,500 ft
Seats: 2
Landing gear: nose wheel
Cross-wind capability: 20 mph

 

Challenger II
Engine: Rotax 503, 52 hp
Wing span: 8.7 m
Wing area: 15.44 sq.m
MAUW: 386 kg
Empty weight: 175 kg
Fuel capacity: 38 lt
Max speed: 160 kph
Cruise speed: 130 kph
Minimum speed: 60 kph
Climb rate: 2.5 m/s
Certification: PFA
Seats: 2
Fuel consumption: 13 lt/hr
Kit price (1998): £9500

 

Quad City Ultralights Aircraft Challenger II
Cruise: 70 mph
Stall: 30 mph
Range: 210 sm
Rate of climb: 700 fpm
Takeoff dist: 250 ft
Landing dist: 250 ft
Engine: Rotax 503, 50 hp
HP range: 40-65
Fuel capacity: 5USG
Empty weight: 330 lb
Gross weight: 850 lb
Length: 20 ft
Wing span: 31.5 ft
Wing area: 175 sq.ft
Cockpit width: 30 in
Landing gear: nosewheel
Cross-wind capability: 20 mph

Quad City Ultralights Aircraft Challenger II CW LSS
Engine: Rotax 503, 52 hp
HP range: 50-75
Length: 20 ft
Wing span: 25 ft
Wing area: 145 sq.ft
Empty weight: 450 lb
Gross weight: 960 lb
Fuel capacity: 10 USG
Cruise: 95 mph
Stall: 40 mph
Range: 200 sm
Rate of climb: 700 fpm
Takeoff dist: 400 ft
Landing dist: 400 ft
Cockpit width: 28 in
Seats: 2
Landing gear: nosewheel
Cross-wind capability: 20 mph

Quad City Challenger II CW

Engine: Rotax 503, 52 hp
Height: 6 ft
Length: 20.5 ft
Wing span: 26 ft
Wing area: 143 sq.ft
Weight empty: 350 lb
Gross: 850 lb
Fuel cap: 5 USG
Speed max: 100 mph
Cruise: 85 mph
Range: 220 sm
Stall: 30 mph
ROC: 1000 fpm
Take-off dist: 300 ft
Landing dist: 200 ft
Service ceiling: 12,000 ft
Seats: 2
Landing gear: nose wheel
Cross-wind capability: 20 mph

Quad City Challenger II
Engine: Rotax 503, 52 hp
HP range: 52
Height: 6 ft
Length: 20.5 ft
Wing span: 26 ft
Wing area: 143 sq.ft
Empty weight: 350 lb
Gross weight: 850 lb
Fuel capacity: 5 USG
Top speed: 100 mph
Cruise: 85 mph
Stall: 30 mph
Range: 220 sm
Rate of climb: 1000 fpm
Takeoff dist: 300 ft
Landing dist: 200 ft
Service ceiling: 12,000 ft
Seats: 2
Landing gear: nosewheel
Cross-wind capability: 20 mph

Quad City Ultralights Aircraft Challenger II Special

Engine: Rotax 503, 50 hp
HP range: 50-65
Length: 20 ft
Wing span: 26 ft
Wing area: 143 sq.ft
Empty weight: 360 lb
Gross weight: 880 lb
Fuel capacity: 10 USG
Cruise: 85 mph
Stall: 36 mph
Range: 230 sm
Rate of climb: 700 fpm
Takeoff dist: 300 ft
Landing dist: 250 ft
Cockpit width: 30 in
Landing gear: nose wheel
Cross-wind capability: 20 mph

 

 


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