LLOYD 40.08....

The aircraft was a triplane with unequal span wings. The upper wing had a span of 23.26 meters and a width of 2.40 m. The middle wing was 22.38 m long and 2.20 meters wide. The lower wing span was 16.84 meters and 2.00 meters wide. The middle wing was mounted to the bottom of the booms and center fuselage. The upper and lower wings were connected by struts and bracing. The gap between the two upper wings was 2.10 meters and the two bottom gap was 1.75 meters. The total wing area was 110 square meters. Below the main body between the upper and lower wings was an enclosed gondola, apparently the bombardier rode in this position

The forward section of the central fuselage had a large enclosed cabin for two gunners. The design provided an excellent field of vision in all directions. In the rear section of the main hull there was a engine compartment for the 12 cylinder 300 hp Daimler water cooled engine, driving a wooden two-blade pusher propeller.

The gun stations were also equipped with a spotlight. The side hulls were built from modified Lloyd C. II fuselage. Both were fitted with a six-cylinder water cooled inline Daimler engine producing160 hp each. Both ot the two blade wooden propellers revolved in the same direction.

The machine was completed on June 8, 1916 and was ready for engine testing at the airport in Aszód. The aircraft was found to be very nose-heavy and the center of gravity was too high. During ground tests prototype suffered some minor damage when it nosed over and flipped. This prompted a redesign of the chassis and the addition of a third wheel under the nose to keep it from toppling nose first into the ground. After the redesign the prototype was ready for its test flight in October of 1916,. Oberleutnant Antal Lany-Lanczendorfer was the test pilot for the flight. The flight seems to be unsuccessful because there is no evidence that the aircraft actually got airborne. In early November Flars (Fliegerarsenal) considered reducing the bomb load in order to reduce the total take-off weight. Development continued at a snail''s pace. In December Flars recommended the installation of additional chassis rails. These were added to the main undercarriage.

In March 1917 Lloyd applied for a revision of the airplane, but the application was rejected and the work came to a halt. The Lloyd 40.08 airframe placed in storage until January of 1918 when it was ordered to be transported to aircraft cemetery in Cheb.

WF2 ... that would be an interesting and short lived model.

here 's another strange bird, a triple tri-plane.

the Caproni Ca-60

How about this!! It's a Kalnin K-7