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rying type and embodies practically the latest conception of pilot locations, passenger location, engine installation, and disposition of fuel tanks. The fuel tanks are located underneath the bottom wing so as to obviate any danger of fire in case of a crash. The landing gear has a shock absorber in the rear leg of the landing gear "vee".

THIS BRISTOL JUPITER 400 H.P. 9-CYLINDER AIR-COOLED ENGINE.
     The characteristics of this engine are as follows:

          Bristol Jupiter engine,
            air-cooled radial - - - 380 h.p.
          Code name for telegraphic 
            and other purposes - - - Jupiter. 
          Direction of rotation  - - Left hand tractor.
          Number of cylinders  - - -  9.
          Bore - - - - - - - - - - -  5 3/4 in.
          Stroke - - - - - - - - - -  7 1/2 in.
          Rated full power at normal
            r. p. m. - - - - - - - - 380 B. H. P.
          Normal speed - - - - - - - 1,575 r. p. m.
          Maximum speed  - - - - - - 1,625 r. p. m.
          Weight - - - - - - - - - -   725 lbs.
          Fuel consumption per B.H.P.
            hour - - - - - - - - - -       .6 pint.
          Oil consumption per B.H.P.
            hour - - - - - - - - - -       .45 pint.

       The engine to be constructed in accordance with General Arrangement, Detail and Installation Drawings, Supervision Sheets, Schedule of Parts, and Material Specifications, which shall first

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