TYPE: Four-seat lightplane.
PROGRAMME: First flight (F-WSQO) 27 March 1972; certified 10 May 1972. Later versions with additional cabin windows.
CUSTOMERS: See main DR 400 entry; total 363 delivered by early 1999. Some nine built in 2000 and at least 11 in 2001 and six in 2002.
DESIGN FEATURES: Generally as for DR 400 series; two-seat rear bench.
Differences from DR 400/160 listed below:
POWER PLANT: One 134 kW (180 hp) Textron Lycoming O-360-A flat-four engine driving a Sensenich 76EM8S5-0-64 two-blade, fixed-pitch aluminium propeller. Fuel tankage unchanged.
ACCOMMODATION: Basically as for DR 400/160. Baggage capacity 60 kg (132 lb).