Various versions of the Champ have been tested and produced since 1944, including military, aerobatic, cropduster, tricycle-gear and (as the
402 Lancer) a twin-engined variant. (Other 65-hp engines by Lycoming and Franklin were also fitted.) A
supplemental type certificate allows the installation of a
Lycoming O-235. The Champ featured a conventional landing gear configuration, with shock absorption in the main gear provided by oleo struts. The aircraft had no electrical system. It is distinguishable from nearly all other variants by the absence of a dorsal fin at the leading edge of the vertical tail (most later models had the enlarged tail). Approximately 7,200 were built between 1945 and 1948—far outnumbering all other subsequent variants combined, and far outnumbering most rival designs of the period. Some were acquired by the U.S. military and designated
L-16—not to be confused with the L-16A and L-16B derived from later Champ variants. 71 were produced. 509 were built.
7CCM, L-16B An improved version of the L-16, the L-16B/7CCM featured a Continental C90-8 engine, an enlarged vertical tail, hydraulic brakes, and a gross weight increase to ; an additional gross weight increase to is allowed when "Long Stroke Oleo Landing Gear" is installed and placard, "Intentional spinning prohibited when baggage carried", is installed on the instrument panel. Gross weight increases to when configured as an
S7CCM floatplane. 100 L-16B/7CCM aircraft were built. 100 7DC aircraft were produced. Standard gross weight is , or with "Lower End Landing Gear Oleo Strut Assembly." The optional
S7EC floatplane configuration has a gross weight of . The last Champ produced at Aeronca was a 7EC, and when Champion reintroduced the Champ in 1955, it was with their version of the 7EC, very little changed from Aeronca's. An enhanced version called the
Champion DeLuxe Traveler offered a metal propeller with spinner,
wheel pants, a steerable tailwheel, and
navigation lights. Differing in a number of ways from earlier 7ECs, this new version in particular replaced the wood-spar wings of the earlier versions with a metal-spar wing and used aluminum gear legs. To fit within the Light Sport requirements, the maximum weight was reduced to 1,320 pounds (599 kilograms). Standard gross weight of the 7FC is with an increase to allowed with the installation of "Wide Track Main Gear." 472 7FC aircraft were built. Gross weight is in standard configuration, in seaplane configuration. 396 were made. 195 built. 25 were built. 4 were built. ==Specifications (7AC)==