Aircraft Dornier DO 228-101 (D-CODE)

Infrastructure
Description

Research Aircraft

Main technical characteristics

Type of flight vehicle Fixed Wing Aircraft
Main features 2 x Garret Turboprop TPE 331-5; Turboshaft Engine; max. take-off weight 5980 kg; cruise speed 370 km/h; range up to 2700 km
Control system Experimental Autopilot with interface for external control input
Maximum altitude 7.600 m (25.000 ft)
Measurement instruments5 Acquisition of data provided by onboard avionic systems and experimental equipment
Comment F / T Research Aircraft

Contact Information
EREA