Illustrated description of 4-cyl horizontally opposed engine designed for use in lighter weight airplanes; bore 3 5/8 in.; stroke 3 1/2 in.; rated 50 hp at 2300 rpm; constructional details. (See also Aero Digest v 32 n 2 Feb 1938 p 64; Can Aviation v 11 n 8 Aug 1938 p 36; Western Flying v 18 n 2 Feb 1938 p 34)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Lycoming 0-145


    Additional title:

    Aviation


    Published in:

    Aviation ; 37 , n 3


    Publication date :

    1938


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Lycoming T53

    Engineering Index Backfile | 1956


    Lycoming 0-145

    Engineering Index Backfile | 1938


    Lycoming Turbofans

    Engineering Index Backfile | 1963


    Lycoming 0-145

    Engineering Index Backfile | 1938


    Lycoming 0-145

    Engineering Index Backfile | 1938