The Fokker E.IV was the final variant of the Eindecker fighter aircraft that was operated by Germany during World War I. Design and development Given the Fokker designation of M.15, the E.IV was essentially a lengthened Fokker E.III powered by the 119 kW (160 hp) Oberursel U.III two-row, 14-cylinder rotary engine, a copy of the Gnome Double Lambda. The more powerful engine was intended to enable the Eindecker to carry two or three 7.92 mm (.312 in) machine guns, thereby increasing its firepower and providing redundancy if one gun jammed - a common occurrence at the time. However, the E.IV was a troubled design that never achieved the success of its predecessor and was soon out-classed by French and British fighters. The prototype E.IV was accepted for testing by the German Inspektion der Fliegertruppen in September 1915. It was fitted with three forward-firing 7.92 mm (.312 in) lMG 08 "Spandau" machine guns, mounted to fire upwards at 15°. Anthony Fokker demonstrated the E.IV at Essen but the complicated triple-synchronization gear failed and the propeller was damaged. The removal of the left-side gun is believed to have been pioneered on Oswald Boelcke's E.IV, believed to have borne IdFlieg serial 123/15, with a simpler double-synchronisation system used on the retained center-line and right side MG 08 Spandau guns. The fitment of dual MG 08 "Spandau" forward-firing, synchronized machine guns became the standard armament for production E.IVs, and indeed for all subsequent German D-type biplane fighters. The angling of the guns was also abandoned. Operational history The modified prototype underwent combat evaluation on the Western Front by Oberleutnant Otto Parschau in October 1915, making it the first twin-gun fighter in service. Leading German ace Oswald Boelcke evaluated the E.IV at Fokker's Schwerin factory in November. The pilots discovered that mounting the much heavier Oberursel U.III onto the Eindecker airframe did not produce a better aircraft - one pilot described it as "practically a flying engine." The inertial and gyroscopic forces of the spinning mass made the E.IV less manoeuvrable than the E.III and any loss of efficiency from the notoriously unreliable engine made the aircraft virtually uncontrollable, requiring the engine to be switched off. Turning under such conditions was exceedingly difficult because the E.IV still used wing warping instead of ailerons. Furthermore, the engine worked well when new, but lost power after only a few hours of operation. Only 49 E.IVs were built