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Quad City Challenger

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United States Quad City Challenger
Quad City Challenger. Photo: Ahunt at English Wikipedia, Public domain, via Wikimedia Commons
Quad City Challenger. Photo: Ahunt at English Wikipedia, Public domain, via Wikimedia Commons
Make Quad City
Model Quad City Challenger
Type Ultralight aircraft
Country United States United States
First flight 1983
Built 1983-present
Status In production (2018)
Number built 3,571 (2011)
Registered in the US 754 (FAA register, October 30, 2026)
Seats one, one passenger and 500 lb (227 kg) useful load
Engine Rotax 503, 50 hp
Cruise speed 85 mph (Challenger II)


Max weight 960 lb (Challenger II)


More aircraft · For sale

The Quad City Challenger is a family of one- and two-seat ultralight and light-sport kit airplanes with a pusher engine, built by Quad City Aircraft Corporation of Moline, Illinois, since 1983.[1] In the U.S. there are 754 with a valid registration, most of them two-seat Challenger IIs.[2]

History

The Challenger has a high wing, tricycle landing gear and a frame of 6061-T6 aluminum tubing joined with aircraft bolts and rivets, covered in Dacron envelopes or aircraft fabric. The engine sits behind the cabin and turns the propeller through a cogged rubber belt reduction drive.[1] The kit comes in four parts (tail, fuselage, wings and engine), with the hardest work already done at the factory.[1]

Models

  • Challenger I: one seat, 31.5 ft wing; with a 22 hp Hirth engine it can fly as a U.S. Part 103 ultralight. About 800 were reported flying by 2011.[1]
  • Challenger I Special: one seat with a shorter 26 ft wing for faster roll; about 300 flying by 2011.[1]
  • Challenger II: two seats in tandem, 31.5 ft wing, can be fitted with floats; Rotax 447, 503, 582 or HKS engines.[1]

Registered in the United States

The FAA register lists 754 of these airplanes with a valid U.S. registration. Here they are by the model name the FAA uses.[2]

FAA model name Registered
CHALLENGER II 558
CHALLENGER 2 26
CHALLENGER I 24
CHALLENGER 21
CHALLENGER II SPEC 18
CHALLENGER 1 15
CHALLENGER II CWS 11
CHALLENGER II SPECIA 7
CHALLENGER II LSS 6
CHALLENGER II CW 6
CHALLENGER II LW 4
CHALLENGER SPECIAL 3
CHALLENGER II CLIP W 3
CHALLENGER 2 PLACE 3
CHALLENGER II CLP WG 3
CHALLENGER CWS 2
CHALLENGER II STANDA 2
CHALLENGER IISPECIAL 2
CHALLENGER II XL65 2
CHALLENGER II XL-65 2
35 other model names 36

Specifications (Challenger II)

Item Challenger II
Crew one
Passengers / capacity one passenger and 500 lb (227 kg) useful load
Length 20 ft
Wingspan 31 ft 6 in
Height 6 ft
Wing area 177 sq ft
Empty weight 460 lb
Maximum takeoff weight 960 lb
Engine Rotax 503, 50 hp (twin cylinder, inline, two stroke, piston aircraft engine)
Maximum speed 96 mph
Cruise speed 85 mph
Stall speed 28 mph
Never-exceed speed 100 mph
Rate of climb 750 ft/min

Figures as given in the Wikipedia article and its sources.[1]

Owner and mechanic notes: coming soon. What to check before you buy, common problems and what they cost to fix. Airplane Wiki is gathering this from owners and mechanics.

Photos

All photos are from Wikimedia Commons; click a photo for its full credit and license.

Buying a Quad City Challenger

For sale listings: coming soon. Airplane Wiki will list Quad City Challengers for sale here, with the facts on this page beside every listing.

Sources

  1. ↑ 1.0 1.1 1.2 1.3 1.4 1.5 1.6 Wikipedia, "Quad City Challenger", read November 1, 2026. Airplane Wiki's text is written in its own words; facts are checked against this article and its sources.
  2. ↑ 2.0 2.1 Federal Aviation Administration, Releasable Aircraft Database, file dated October 30, 2026. Valid registrations of fixed-wing airplanes whose FAA maker and model names belong to this family. Airplane Wiki uses only counts from this file, never owner names or addresses.