GENERAL
Description | The Diamond DA40 Diamond Star is an Austrian four-seat, single-engine, light aircraft constructed from composite materials. Built in both Austria and Canada, it was developed as a four-seat version of the earlier DA20 by Diamond Aircraft Industries. |
Wake Turbulence Category | L |
Aerodrome Reference Category | |
Approach Category | |
Variants | DA40, DA40 D, DA40 F, DA40 NG |
Manufacturer | Diamond |
First Flight | 5th Nov 1997 |
Launch Organisation | |
Largest Operator | |
First Registered In India | January 2009, CAE-NFTI |
Users In India | IGRUA, NFTI, APFT |
Takeoff 305m
Landing 305m
RUNWAY REQUIRED AT MTOW/MLW
SPECIFICATIONS
Crew | 1 |
Passenger Capacity | 1 |
Length | 15.27 m |
Wingspan | 10.90 m |
Height | 5.34 m |
Wing Area | 45.7 sqm |
Max Ramp Weight | 24,500 Kgs |
Fuel Capacity | 6,668 L |
Engine | SNECMA M88-4e |
Thrust | 11,250 Lbs |
Fleet Detail
MSN | TAIL | MAKER | MODEL | ENGINE | CONF | FIRST FLT | LESSOR | REMARKS |
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