Quad City Challenger light sport aircraft performance specifications.

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Quad City Challenger II Light Sport Aircraft Performance data

The following are real world performance figures for the Quad City Challenger II long wing version powered by a Rotax aircraft 503 engine using the standard Challenger belt drive system and propeller.

PERFORMANCE:

CHALLENGER II


VNE
100 MPH

TOP LEVEL SPEED
75 TO 90 MPH 

CRUISE SPEED 
60 TO 65 MPH

STALL SPEED
30 MPH SOLO
35 MPH DUAL

CLIMB RATE WITH
50 HP ROTAX 503
800 FPM SOLO
450 FPM DUAL 

TAKE OFF ROLL
100 FT. SOLO
200 FT. DUAL

GLIDE RATIO 
8 TO 1 SOLO
6 TO 1 DUAL

FUEL CONSUMPTION AT CRUISE
4 TO 6 GPH

Quad City Challenger II Light Sport Aircraft Specifications

SPECIFICATIONS:

CHALLENGER II


WINGSPAN
31 FT. 6 IN.

LENGTH 
20 FT. 0 IN.

HEIGHT 
6 FT. 0 IN. 

WING AREA
173 SQ. FT.

ENGINE STANDARD
ROTAX 447, 42 H.P.

ENGINE OPTIONAL
ROTAX 503, 48 H.P.

ENGINE OPTIONAL

ROTAX 503, 52 H.P.


ENGINE OPTIONAL

ROTAX 582, 65 HP


EMPTY WEIGHT
300 LBS. WITH 447

USEFUL LOAD 
500 LBS. WITH 447

ULTIMATE LOAD 
+ 6 - 4 

BUILD TIME 
 75 TO 100 HRS
FIELD ASSEMBLY TIME 60 MIN. 

AIRFRAME TYPE
ALUMINUM
TUBE

STANDARD COVERING
PRE-SEWN DACRON, & SAILCLOTH

OPT    COVERING
CONVENTIONAL AIRCRAFT COVERING


Rotax 582 Engine Installation


Long wing Quad City Challenger
with Rotax 503 50 HP engine

 
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