Customer:Royal Air MarocCasablanca, MorroccoFacility Type:100,000 lbf Turbofan and 6000 shp Turboshaft/APU Repair & Overhaul Gas Turbine Engine Test FacilityEngine Types:Turbofan: PW 2037, CFM56-3C, CF6-80C2, & ATAR 9K50 (a military engine with afterburner capability); and Turboshaft/APU: PW120A, T56-A15-LFE, & Garrett APUs (GTCP 85-98Ck/-129, GTCP 36-280, GTCP 331-200Description:MDS was responsible for all aspects of this turnkey project, including project management, architectural design, and facility construction. This multi-test bed facility is now equipped for repair and overhaul testing of turbofan, turboshaft, and APU gas turbines.Scope of Work: Inlet and Exhaust Systems; Quick engine change out capability; 100Hz Steady-State and Transient Data Measurement; Thrust Measurement System; Monorail Engine Handling; Engine Adapters; Fuel Delivery and Measurement Systems; Engine Start Systems; Oil Inhibiting and Preservation Systems; Hydraulic Lift Platform;