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Bell YFM-1 Airacuda

The Bell YFM-1 Airacuda was an American heavy fighter aircraft, developed by the Bell Aircraft Corporation for the United States Army Air Corps during the mid-1930s. It was the first military aircraft produced by Bell. Originally designated the Bell Model 1, the Airacuda first flew on 1 September 1937. The Airacuda was marked by bold design advances and considerable flaws that eventually grounded the aircraft.

Design and development
In an effort to break into the aviation business, Bell Aircraft created a unique fighter concept touted to be "a mobile anti-aircraft platform" as well as a "convoy fighter". Created to intercept enemy bombers at distances beyond the range of single-seat fighter interceptors, the YFM-1 (Y, service test; F, fighter; M, multiplace) was an innovative design incorporating many features never before seen in a military aircraft, as well as several never seen again. Using a streamlined, "futuristic" design, the Bell Airacuda appeared to be "unlike any other fighters up to that time". According to Major Alexander De Seversky's 1942 book Victory Through Air Power, the Bell Airacuda "represents a great engineering achievement. But its designation as 'convoy fighter' is erroneous, since that requires different disposition of armament. With its maximum firepower directed forward, it really offers a preview of an effective long-range interceptor fighter." Although capable of aiming the cannons, the gunners' primary purpose was simply to load them with the 110 rounds of ammunition stored in each nacelle. Design flaws The Airacuda was plagued with problems from the start. The lofty performance estimates were unobtainable as, despite its sleek looks, the Airacuda was heavy and was slower than most bombers. In the event of interception by enemy fighters, the Airacuda was not maneuverable enough to dogfight, while the meager bombload was of little use in the intended fighter-bomber role. Even the 37 mm cannons were of less value than predicted. The cannons had a tendency to fill the gun nacelles with smoke whenever fired and, additionally, fears persisted as to how the gunners would escape in an emergency, with the propellers directly behind them. An emergency bailout would have required both propellers to be feathered, Initial flight testing by Lt. Ben Kelsey proved the Airacuda virtually impossible to control with only one engine, as the aircraft would go into an immediate spin. Problems with stability in pitch were also encountered and had to be corrected by reducing power. Systems usually powered by an aircraft's engines were instead powered by the single generator. The generator, with its own supercharger, was located in the belly of the aircraft. In the event of a failure (and they occurred frequently), the crew was instructed to begin immediate emergency restart procedures, as the aircraft basically shut down. When the APU failed, the pilot had "NO fuel pressure, NO vacuum, NO hydraulic pressure, NO gear, NO flaps and NO ENGINES". Accidents Despite the aircraft's many faults, only two were lost in accidents. The seventh aircraft (38-492) was on its final test flight, on June 21, 1940, from the Buffalo factory prior to delivery to the Air Corps when pilot John Strickler, a Bell pilot and engineer/co-pilot Brian Sparks, Bell's chief test pilot, encountered problems recovering from a deliberate spin attempt which was part of the test flight profile. Despite every effort to emerge from the spin, the aircraft would not respond, and it appeared that the rudder had locked. Co-pilot Sparks shut down the engines and waited for the propellers to come to a stop before bailing out. Because of the tandem seating, it was necessary for Sparks to exit the aircraft first, and in doing so he struck the empennage, breaking his legs and in the process, freeing the rudder. ==Operational history==
Operational history
Despite these problems, one fully operational Airacuda squadron was eventually assembled, and operated from 1938 until 1940. Funds were appropriated, but never released, for the purchase of two groups of Airacudas. Near the end of the type's operational life, the aircraft were flown primarily for photo opportunities and always accompanied by a chase plane for safety. Eventually the decision was made to disperse the aircraft to various airfields to give pilots an opportunity to add the unusual aircraft to their log books. Airacudas were sent at various times to Langley Field, Virginia; Maxwell Field, Alabama; Hamilton Field, California; and Wright Field, in Dayton, Ohio. YFM-1 38-488 was displayed at the 1940 World's Fair in New York, finished in the markings of the 27th Pursuit Squadron. During this time, the aircraft saw limited flight time, as few pilots were interested in flying the unusual aircraft. Several plans were made to modify the Airacudas to give them operational status, including modifying the airframe and adding more powerful engines, but all proposals were eventually rejected. In early 1942, despite fears of enemy bomber attacks against which the Airacuda was intended, the aircraft were stricken from inventory. ==Variants==
Variants
The prototype, known as the XFM-1, incorporated a tailwheel, side "blister" ports, and a smooth, rounded canopy. This is the best known, and most produced version. An updated version called the YFM-1A eliminated the side blisters and added externally mounted radiators and turbo-superchargers. Produced in 1940, the final version designated YFM-1B, was slightly larger, had slightly less powerful Allison engines and incorporated a tricycle landing gear. The canopy was redesigned, with a flat forward windshield. A rearward-facing belly gunner's position was also added. The resulting aircraft was roughly the size of a Douglas B-18 Bolo medium bomber. Three YFM-1Bs were produced in 1939 before production was finally terminated. ;XFM-1 :(Model 1) Prototype powered by two 1,150 hp V-1710-13 engines, one (36-351) built. ;YFM-1 :(Model 7) Development aircraft powered by two 1,150 hp V-1710-23 engines and fitted with 37 mm cannons in wing nacelles, eight built, two later converted to YFM-1B. ;YFM-1A :(Model 8) Development aircraft with tricycle landing gear, three built. ;YFM-1B :YFM-1 re-engined with 1,090 hp V-1710-41 engines, two converted from YFM-1. ;YFM-1C :(Model 17) – proposed variant not proceeded with. == Scrapping ==
Scrapping
By 1942, all nine surviving YFM-1 airframes had been flown by ferry crews to a training facility at Chanute Field, Illinois, where the aircraft were assigned to the 10th Air Base Squadron to be used for ground crew instruction. By March 1942, all Airacudas had been scrapped. ==Specifications (XFM-1)==
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