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Avião Diamond DA42 à Venda
Avião bimotor
REF:
AS5550
Preço sob consulta
Status
Disponível
Status
Disponível
Fabricante
Diamond
Modelo
DA42
Motor
Austro Engine AE 300
Combustível
Jet A - Querosene
Ano
2023
Horas totais
190
Assentos
4
Condição
Usado
Localização
Brasil
Ano
2023
Horas totais
190
H
Assentos
4
Condição
Usado
Localização
Brasil
Galeria do PDF (Não visível na página normal)
Visão geral
Especificações
Visão geral
- Horas Disponíveis: 1.610
Equipamentos
- Radar meteorológico
- Garmin G1000 NXi Glass Panel Suite:
- Dual Garmin 10” LED Backlit Flight Displays w/ Synthetic Vision
- Dual Garmin GIA 64W WAAS GPS/NAV/COMMS
- Garmin GFC 700 Digital Autopilot w/ Yaw Damper
- Garmin Electronic Stability Protection
- Garmin GEA 71B Airframe/Engine Interface Unit
- Garmin GMA 1360 Digital Audio System
- Garmin GRS 79 Attitude Heading Reference System
- Garmin GDC 72 Digital Air Data Computer
- Garmin GMU 44 Magnetometer
- Garmin ChartView Approach Plates
- Avidyne TAS 605 Traffic Advisory System
- Garmin Flight Stream 510 (Digitally syncs EFB flightplan w/ plane)
- Garmin GTX 345R ADS-B “In & Out” Transponder
- Garmin GDL 69SXM SAT WX
- Mid-Continent MD-302 Digital Standby Instr.
- ELT 406 MHz
Especificações
Power Plant
| Engine | 2 × Austro Engine AE 300 turbocharged common-rail injected 2.0 liter diesel engine with 168 HP and EECU single lever control system |
|---|---|
| Propeller | 2 × MT propeller MTV-6-R-C-F/CF 190-69 3-blade constant speed propeller |
| Fuel grades | Jet A-1, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8 |
Performance (MTOM, ISA)
| Max. speed (16,000 ft, MCP) 1,760 kg TOW | 365 km/h TAS | 197 kts TAS |
|---|---|---|
| Max. cruising speed (16,000 ft, MCP) | 352 km/h TAS | 190 kts TAS |
| Cruise speed at 75% (16,000 ft) | 324 km/h TAS | 175 kts TAS |
| Stall speed, landing configuration | 115 km/h CAS | 62 kts CAS |
| Rate of climb (ISA SL) 1,760 kg TOW | 5.7 m/s | 1,114 ft/min |
| Single engine service ceiling (climb rate 50 ft/min) | 4,878 m | 16,000 ft |
| Single engine absolute ceiling (climb rate 0 ft/min) | 5,335 m | 17,500 ft |
| Range at 60% (12,000 ft, incl. auxiliary tank) incl. climb, no reserves | 2,038 km | 1,100 nm |
| Max. range (FL 180, 50% PWR) incl. climb, no reserves | 2,269 km | 1,225 nm |
| Consumption at 60 % in total | 39.4 l/h | 10.4 US gal/h |
| Take-off performance (MSL, ground roll / take-off obstacle) Short field t/o procedure | 375 m / 649 m | 1,230 ft / 2,129 ft |
| Landing ground roll (ISA SL) | 340 m | 1,115 ft |
| Landing performance (MSL, ground roll / landing distance) | 387 m / 647 m | 1,269 ft / 2,122 ft |
| Max. operating altitude | 5,488 m | 18,000 ft |
| Max. demonstrated crosswind | 46 km/h | 25 kts |
Dimensions
Mass and Loading
| Seats | 4 | 4 |
|---|---|---|
| Empty weight without options | 1,420 kg | 3,131 lbs |
| Max. useful load | 579 kg | 1,276 lbs |
| Max. take off mass | 1,999 kg | 4,407 lbs |
| Fuel capacity total main tank auxiliary tank | 289 l / 231 kg 189 l / 151 kg 100 l / 80 kg | 76.4 US gal / 512 lbs 50.0 US gal / 333 lbs 26.4 US gal / 176 lbs |
- Horas Disponíveis: 1.610
Equipamentos
- Radar meteorológico
- Garmin G1000 NXi Glass Panel Suite:
- Dual Garmin 10” LED Backlit Flight Displays w/ Synthetic Vision
- Dual Garmin GIA 64W WAAS GPS/NAV/COMMS
- Garmin GFC 700 Digital Autopilot w/ Yaw Damper
- Garmin Electronic Stability Protection
- Garmin GEA 71B Airframe/Engine Interface Unit
- Garmin GMA 1360 Digital Audio System
- Garmin GRS 79 Attitude Heading Reference System
- Garmin GDC 72 Digital Air Data Computer
- Garmin GMU 44 Magnetometer
- Garmin ChartView Approach Plates
- Avidyne TAS 605 Traffic Advisory System
- Garmin Flight Stream 510 (Digitally syncs EFB flightplan w/ plane)
- Garmin GTX 345R ADS-B “In & Out” Transponder
- Garmin GDL 69SXM SAT WX
- Mid-Continent MD-302 Digital Standby Instr.
- ELT 406 MHz
Power Plant
| Engine | 2 × Austro Engine AE 300 turbocharged common-rail injected 2.0 liter diesel engine with 168 HP and EECU single lever control system |
|---|---|
| Propeller | 2 × MT propeller MTV-6-R-C-F/CF 190-69 3-blade constant speed propeller |
| Fuel grades | Jet A-1, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8 |
Performance (MTOM, ISA)
| Max. speed (16,000 ft, MCP) 1,760 kg TOW | 365 km/h TAS | 197 kts TAS |
|---|---|---|
| Max. cruising speed (16,000 ft, MCP) | 352 km/h TAS | 190 kts TAS |
| Cruise speed at 75% (16,000 ft) | 324 km/h TAS | 175 kts TAS |
| Stall speed, landing configuration | 115 km/h CAS | 62 kts CAS |
| Rate of climb (ISA SL) 1,760 kg TOW | 5.7 m/s | 1,114 ft/min |
| Single engine service ceiling (climb rate 50 ft/min) | 4,878 m | 16,000 ft |
| Single engine absolute ceiling (climb rate 0 ft/min) | 5,335 m | 17,500 ft |
| Range at 60% (12,000 ft, incl. auxiliary tank) incl. climb, no reserves | 2,038 km | 1,100 nm |
| Max. range (FL 180, 50% PWR) incl. climb, no reserves | 2,269 km | 1,225 nm |
| Consumption at 60 % in total | 39.4 l/h | 10.4 US gal/h |
| Take-off performance (MSL, ground roll / take-off obstacle) Short field t/o procedure | 375 m / 649 m | 1,230 ft / 2,129 ft |
| Landing ground roll (ISA SL) | 340 m | 1,115 ft |
| Landing performance (MSL, ground roll / landing distance) | 387 m / 647 m | 1,269 ft / 2,122 ft |
| Max. operating altitude | 5,488 m | 18,000 ft |
| Max. demonstrated crosswind | 46 km/h | 25 kts |
Dimensions
Mass and Loading
| Seats | 4 | 4 |
|---|---|---|
| Empty weight without options | 1,420 kg | 3,131 lbs |
| Max. useful load | 579 kg | 1,276 lbs |
| Max. take off mass | 1,999 kg | 4,407 lbs |
| Fuel capacity total main tank auxiliary tank | 289 l / 231 kg 189 l / 151 kg 100 l / 80 kg | 76.4 US gal / 512 lbs 50.0 US gal / 333 lbs 26.4 US gal / 176 lbs |
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