An evaluation of the anti-icing and de-icing systems was conducted on a leased airplane. The anti-icing system was found satisfactory. It was recommended that the L-23F Airplane be retrofitted with a self-contained pressure system and de-icing boots that would equal or surpass the operational suitability of the de-icing system used on the L-23D. The anti-icing systems and the de-icing systems tested were lightweight pneumatic boot de-icing system and an electrothermal anti-icing system for the wings, empennage, propellers, and windshield. (Author)


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    Title :

    Evaluation of L-23F de-Icing and Anti-Icing Systems


    Publication date :

    1962


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English