MarketAeronca Champion
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Aeronca Champion

The Aeronca Model 7 Champion, commonly known as the "Champ", or "Airknocker", is a single-engine light airplane with a high wing, generally configured with fixed conventional landing gear and tandem seating for two occupants.

Design and development
The Aeronca 7 Champion line—developed in the mid-1940s as a post-World War II response to the popular Piper J-3 Cub—uses similar design features (already featured in Aeronca's wartime designs, the Aeronca Model T, Aeronca Defender, and Aeronca L-3), but also incorporates aspects of traditional Aeronca designs, including the internal main trusswork of the fuselage frame. Like its predecessors and initial rivals, the high-wing, two-seat plane has tandem seating, conventional landing gear (tailwheel-equipped), and a small piston engine. As with many light aircraft of the time, the Champ's fuselage and tail surfaces are constructed of welded metal tubing. The outer shape of the fuselage is created by a combination of wooden formers and longerons, covered with fabric. The cross-section of the metal fuselage truss is triangular, a design feature which can be traced all the way back to the earliest Aeronca C-2 design of the late 1920s. in Southern England. Note the similarities to its rival, the Piper J3 Cub Like the Piper Cub with which it competed, the Champ features tandem seating. However, while the J-3 model of the Cub is flown solo from the rear seat, the Champ can be soloed from the front, giving improved forward visibility, particularly on the ground and during takeoffs, landings, and climbs. The Champ offers far better visibility than the Cub, allowing 300 degrees of visibility to a front-seated pilot, and has a wider cabin than the Cub. Additionally, an uncommon ==Operational history==
Operational history
Built by Aeronca Aircraft Corporation, the Champ first flew in 1944, and entered production in 1945. As an economical postwar rival to the Piper Cub (which it largely improved upon), the Champ was popular with training schools who were training veterans returning from World War II, by the thousands, with government funding through the G.I. Bill. The original model 7AC Champion initially sold by the thousands, peaking in 1946, as Aeronca developed the highest-volume production line in general aviation. Between 1946 and 1947, Aeronca was producing an average 30 light aircraft per day (peaking at 50 per day at one point). But 1946 was a momentary explosion in lightplane production, industry-wide. The postwar boom-and-bust of the late 1940s and early 1950s brought an abrupt end to the massive sales, and—like the rest of the U.S. lightplane industry—Aeronca production dropped to a small fraction of 1946–1947 sales. Some of these Champ variants were acquired by the U.S. Army Air Forces (USAAF) and its successor, the U.S. Air Force (USAF), particularly for use by the U.S. Army Ground Forces and the National Guard, as replacements for the Piper L-4 variant of the Piper Cub, used as an observation and liaison aircraft. The Aeronca Champ military variants were labeled L-16, L-16A and L-16B. By the time production ended in 1951, the company had sold more than 8,000 Champions, mostly 7AC Champs (approx. 7,200). Only a handful of 7ACAs were built between 1971 and 1972. Bellanca ceased all production in the early 1980s. Fuel capacity was reduced to to conserve weight; despite this measure and various others, such as the use of aluminum landing gear legs and bare birch floorboards rather than carpet, the aircraft's payload is inadequate to carry two adults and full fuel simultaneously. The manufacturer was considering various further weight-reduction measures including the use of the lightened Continental O-200D engine previously offered in the Cessna 162 Skycatcher. Only those specific original-production 7EC airplanes certificated at a gross weight qualify for the LSA category; ==Variants==
Variants
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)==
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