An evaluation of the Reliability, Availability, Maintainability and Durability (RAMD) characteristics of the Boeing YUH-61A and the Sikorsky YUH-60A UTTAS candidates was conducted. The evaluation is based on Development Test II (DT II), and Operational Test II (OT II) data. The Boeing and Sikorsky UTTAS candidates' demonstrated RAMD characteristics are compared to each other as well as to the Bell UH-1H and the requirements as stated in the UTTAS Materiel Need (MN) and the Decision Coordinating Paper (DCP). (Author)
An Evaluation of the Reliability, Availability, Maintainability and Durability of the Utility Tactical Transport Aircraft System
1980
317 pages
Report
No indication
English
Aircraft , Logistics Military Facilities & Supplies , Helicopters , Utility aircraft , Transport aircraft , Tactical aircraft , Reliability , Maintainability , Prototypes , Test and evaluation , Availability , Durability , UTTAS(Utility Tactical Transport Aircraft System) , UH-1H aircraft , H-1 aircraft