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Specification

DIAMOND DA42 TWINSTAR

DIAMOND DA42 TWINSTAR

The DA42 Twin Star is a twin engined light utility and trainer aircraft manufactured by Diamond Aircraft Industries. The aircraft is operated by flight training schools and aerial surveillance and mapping operators.

1 DA42 Twinstar aircraft in our fleet

TC-SRN

TECHNICAL SPECIFICATIONS

ENGINE

2 x TAE 125-02-99

POWER

2 X 135 HP

PROPELLER(s)

2 x MT Propeller MTV 6-A-C-F Constant Speed

AVIONICS

Flight Instruments

Garmin 1000

Engine Instruments

Garmin 1000

PERFORMANCE

Max Speed

197 TAS

Cruise Speed

176 TAS

Range

1215 nm (%60 Power)

Stall Speed (Vs0)

61 CAS

Cross Wind Limitations

25kts

Service Ceiling

18.000 ft

Take-off Distance (Ground Roll / Over 50ft)

280 m

Landing Distance (Ground Roll / Over 50ft)

340m

WEIGHT AND CAPACITY

Empty Weight

1410 kg

Useful Load

589 kg

Maximum Take-off Weight

1999 kg

Fuel Capacity

Main tank: 2×50 US gal

Aux tank:2×26.4 US gal

Total: 76.4 US gal

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