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| Diamond DA42 Twin Star |  | | | Starting
from € 379-900,-*) |
| Engines | 2x
THIELERT Centurion 1.7 | | Max.
T/O Power/ cont. Power | 2
x 650lb Thrust/ 2 x 136BHP, 2300 rpm | | Propeller | MT,
3 blade hydraulic constant speed propeller, Ø 1870 mm |
| Hydraulic retractable landing
gear | |
| Panel | Standard
or optional glass-cockpit | |
| Performance / consumption |
| Take-off distance,
ground roll | 290 m |
951 ft | | Take-off
distance over 50 ft obstacle | 470
m | 1542 ft |
| Rate of climb sea level by MTOW |
8.78 m/s | 1730
fpm | | Rate
of climb in 10.000 ft | 7.87 m/s |
1550 fpm |
| Cruising speed 90% @ in 12.500 ft TAS |
376 km/h | 203
kt | | Fuel
consumption | 48 l/h |
12.7 USgal/h |
| Cruising speed 60 % @ in 10.000 ft |
311 km/h | 168
kt | | Fuel
consumption | 29.6 l/h |
7.8 USgal/h |
| Maximum operating altitude |
5.486 m | 18.000
ft | | Range
@ 60 % Standard/10,000 ft/no reserve | 1912
km | 1061 nm |
| optional tank |
2677 km | 1485
nm | |
| Length |
8.5 m | 27.8
ft | | Height
approx. | 2.6 m |
8.5 ft | | Wing
span | 13.42 m |
44 ft | | Wing
area | 16.46 m² |
177.17 sq ft |
| Seats | 4 |
4 | | Empty
weight | 1080 kg |
2381 lbs |
| Max. Take-off weight | 1650
kg | 3637 lbs |
| Usable fuel capacity
standard | 195 l |
51.5 USgal |
| optional | 280
l | 73.9 USgal |
| Fuel grades |
Jet A1/Diesel | |
| Useful load IFR |
570 kg | 1256
lbs | |
| Power plant |
| Engine | 2
x Centurion 1.7 | | Max.
T/O-Power / cont. Power | 2 x 650 lb Thrust/2 x 136BHP,
2.300 rpm | | Propeller | MT,
3 blade, hydraulic constant speed propeller, Ø 1.870 mm |
| Hydraulic retractable landing gear | |
| Panel | Glass-cockpit
GARMIN G 1000 | |
| Performance |
| Take-off
distance ground roll (over 50 obstacle) MTOW |
290 m 470 m |
951 ft 1.542 ft |
| Rate of climb, sea level by MTOW |
8,78 m/s | 1.730
fpm | | Rate
of climb in 10.000 ft | 7,87 m/s |
1.550 fpm |
| Cruising speed 90 % @ in 12.500 ft TAS Fuel
consumption | 376 km/h 48
l/h | 203 ktas 12,7
US gal/h | |
Cruising speed 60% @ in 10.000 ft Fuel consumption |
311 km/h 29,6 l/h |
168 ktas 7,8 US gal/h |
| Max. operation altitude |
5.486 m | 18.000
ft | | Range
@ 60% standard/10.000 ft/no reserve optional |
1.912 km/ 2.677 km | 1.061
NM/ 1.485 NM | |
| Specifications/Weights |
| Length |
8,5 m | 27,8
ft | | Height
approx. | 2,6 m |
8,5 ft |
| Wing span | 13,42
m | 44 ft |
| Wing area | 16,46
m² | 177,17 sq ft |
| Seats |
4 | 4 |
| Empty weight |
1.080 kg | 2.381
lbs | | Max.
take-off weight (mass) | 1.650
kg | 3.637 lbs |
| Useable fuel capacity
standard/ optional | 195
l / 280 l | 51,5 US gal / 73,9 US
gal | | Fuel
grades | Jet A1/Diesel | |
| Payload IFR |
570 kg | 1.256
lbs | |
| Airframe |
 |
- Safety cabin design and safety seats (up to 26 g’s)
- Self adapting
cushions on seats and backrest (comfort gel foam)
- Power supply socket
for hand held GPS
- Instrument lighting
- Overhead cabin light
- 3-point
safety belts, automatic, all seats
- High gloss multi layer paint
- FAILSAFE
airframe design
- Lightning protection system
- Standard design
- Registration
markings
- 195 litre (52 USgal.) fuel tank
- Electrically operated
flap system
- Landing lights
- Taxi lights
- Position lights
- ACL
- Heated
pitot static tube
| |
| Engine |
| |
- 2 x THIELERT Centurion 1.7
- MT, 3 blade, constant speed propeller
|
|
| Avionic/ Monitoring
system |
 |
- Integrated Engine Indicating System
- Compass
- Horizon
- Air
speed indicator (kts)
- Altimeter (ft)
- 10-inch Primary Flight Display
(PFD)
- 10-inch Multifunction Display (MFD)
- Alternate static port
- OAT
indicator
- Digital Audiosystem
- Integrated solid-state Attitude
and Heading Reference System (AHRS)
- Dual integrated COM/NAV/GPS
- Integrated
Transponder Mode S
- Remote DME
- Fully integrated KAP140 Dual Axis
AP
| |
| Interior + Extras |
 |
- Leather de Luxe
- 4 ANR Headsets with Smartplugs
- ELT ACK
E-01
- Towbar, First Aid Kit, Fire Extinguisher, Tools)
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