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The Excalibur was designed as "clone" [1] of the Quad City Challenger II aircraft. The company took the basic Challenger design and incorporated many changes, including mounting the engine upright allowing larger propellers and the Rotax gearbox to be mounted, lengthening the tailboom and enlarging the tail vertical surface to increase stability, shortening the ailerons and replacing control ...
The new design differed so much from the original Excalibur, that a different model designation was needed. It was first given the temporary designation L-104, then it was later officially designated the Model 49 or "Excalibur A". In time, the Model 49 would become a completely different aircraft from the original Model 44.
The Romanian Air Force (RoAF) (Romanian: ForČ›ele Aeriene Române) is the air force branch of the Romanian Armed Forces.It has an air force headquarters, an operational command, five air bases, a logistics base, an air defense brigade, an air defense regiment and an ISR brigade.
Pages in category "Aircraft with fixed tricycle landing gear" The following 200 pages are in this category, out of approximately 385 total. This list may not reflect recent changes .
The Excalibur Ib has improved reliability and lower unit cost than the previous Excalibur Ia-1 and Ia-2. At the time of the award, over 690 Excalibur projectiles had been fired in theater. [ 50 ] In February 2014, the U.S. Army and Raytheon fired 30 Excalibur Ib shells at test targets to confirm the performance and reliability of the ...
The SA26 Merlin is a pressurized Excalibur fitted with a different Lycoming TIGO-540 6-cylinder geared piston engine. The TIGO 540 was used despite the fact that one of the reasons the IO-720 was used in the Excalibur was that the Queen Air series' IGSO-480 and IGSO-540 engines from the same manufacturer were so troublesome.
F.15F Excalibur - F.15F built by JSC Sokol at Nizhny Novgorod, Russia for assembly by Eurospace in Italy. Pre-production aircraft assembled by HOAC in Austria and flown in October 1994. Orders for 33 aircraft at end of 1995, with about 100 in various stages of construction or assembly at that time.
[1] [3] The reduction drive is a choice of two integral gearboxes: the A-type gearbox has a 2.58:1 ratio and can accommodate propellers of up to 4,000 kg/cm2 inertial load; the B-type gearbox has a 3.47:1 ratio and can accommodate propellers of up to 6,000 kg/cm2. [1] [3] The 700E burns 9 L (2.4 US gal) per hour in cruise flight at 4,750 rpm.