The feasibility of a six seat variant of the Britten Sheriff twin-engined aircraft, the Marshal, was studied. Results show that the Marshal, powered by two 200 h.p. engines and at an all-up-weight (AUW) of 3550 lb, can compete in the open market, both in terms of performance and price. No major structural alterations, except on the fuselage to accommodate two additional passengers, are envisaged. This aircraft is expected to be suitable for a touring role. For business flying, a high cruise speed is favored and so a turbocharged version was also considered. The performance level attainable, with two 200 h.p. turbocharged engines, compares well with the competition. However, at an AUW of 3700 lb, certain modifications to the wing are necessary. The indication is that the Marshal is a commercially viable project.


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    Title :

    A Design Study of the Marshal


    Contributors:
    D. Suen (author) / G. H. Tan (author)

    Publication date :

    1981


    Size :

    55 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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