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)
Evaluation of L-23F de-Icing and Anti-Icing Systems
1962
10 pages
Report
No indication
English
European Patent Office | 2021
|NTIS | 1971
NTIS | 1979