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         The Hannover CL II (aka 
         Hannoveraner) was a successful relatively small, two-seat aircraft that 
         was used in the escort fighter and attack roles. The CL designation was 
         for fast two-seater, multi-role aircraft. It was first used as an 
         escort fighter for C class photo-reconnaissance manchines. Allied 
         fighters often attacked it thinking it was a single-seat scout and got 
         a surprise when the rear-gunner fired at them.  
         The CL II was a biplane 
         of conventional layout apart from its biplane tail, which was designed 
         to offer the rear gunner a better arc of fire over the tail. The body 
         was deep and fairly narrow, which afforded excellent visibility 
         downwards. It was highly manoeuvrable and versatile. It first flew in 
         late-1917 and participated with newly formed Schlachtstaffeln (Battle 
         Flights) in the heavy ground-attacks during the German spring offensive 
         of 1918. 639 were built by Hannover Waggonfabrik Aktien Gesellschaft. 
         The Hannover CL III was a development of the CL II. It was a bit 
         smaller and lighter but with the same configuration. 537 were built.
          
          
         Technical Details  
          
         Type: CL II 
         The CLII carried a crew of two, the standard of pilot and rear gunner. 
         It was powered by the 180hp (134 kW) Opel-Argus As III inline engine. 
         Maximum speed was 101 mph (165km/h), with a ceiling of 24600ft (7500 m) 
         and an endurance time of 3h 30m. It was armed with the standard German 
         machine guns, typically 7.92 mm, being a single synchronized Spandau 
         gun fuselage mounted and a ring-mounted Parabellum for the gunner.  
          
         Type: CL IIIa 
         The Hannover CL III was a development of the CLII with the same layout. 
         It was produced in response to criticism from crews in the field about 
         a lack of lateral control at low levels. The wingtips were modified and 
         the ailerons now incorporated overhung balances. This modification was 
         important because the improved lateral control was more immediately 
         necessary when manoeuvring close to the ground as the changed role of 
         the aircraft (ground attack) now dictated. The response to questions of 
         performance were answered by installing the 160 hp. Mercedes engine, 
         which was lighter and although rated lower in horsepower, actually 
         performed better, particularly at altitude. Unfortunately, the Mercedes 
         engine was required more urgently for single seaters, so the type 
         reverted to the Argus engine and in this guise was designated the 
         CL.IIIa. The CL III had an Mercedes D.III engine, the CL IIIa an Argus 
         As III engine. All other aspects of their abilities seem to be the same 
         as the CL II.  
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