TECHNICAL PAPERS

Icing Investigations and Product Development on MU-2B Airplanes

Date Published: 2003-06-16
Paper Number: 2003-01-2088
DOI: 10.4271/2003-01-2088

Citation:

Timmons, L., "Icing Investigations and Product Development on MU-2B Airplanes," SAE Technical Paper 2003-01-2088, 2003, doi:10.4271/2003-01-2088.

Author(s):


Lawrence M. Timmons - Aircraft Engineering Specialists, Inc.

Abstract:

Mitsubishi Heavy Industries, Ltd (MHI) produced over 704 MU-2B airplanes from 1965 through 1986, and all were approved for flight into known icing conditions. With the ATR 72 accident at Roselawn, Indiana, all turboprop airplanes were subjected to additional scrutiny concerning operation in icing and, in particular, SLD conditions. MHI sponsored extensive ground and flight test programs to verify MU-2B flight characteristics in both FAR Part 25 Appendix C and SLD conditions. As a result of this test program several product improvements and operational procedures were developed. These were offered to the field to aid pilots in recognizing and exiting both normal and severe icing conditions. This paper details results of this testing and recommendations for increased pilot awareness of icing conditions. Results and conclusions have broad application to turbopropeller driven aircraft.

File Size: 2567K

Product Status: In Stock

See papers presented at FAA In-flight Icing / Ground De-icing International Conference & Exhibition, June 2003, Chicago, IL, USA, Session: Ice Accretion Effects on Airplane Operation and Handling

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