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Multimission helicopter display subsystem: transition to flight test

Four operator displays are being integrated into the US Navy multi-mission helicopter, SH-60R with a planned initial operating capability date of 2001. These active matrix liquid crystal displays (AMLCDs), one 10.4 inch display used in three locations in the cockpit, and one 16 inch display used in the cabin, have moved from development status to avionics lab integration and preliminary flight testing. This paper presents the general approach taken to develop, evaluated, integrate, and test the AMLCD displays in the avionics system.