When you take control of the DA42 you are in command of the most technologically advanced twin today. Representing the latest in airframe design, avionics capability and new engine technology, the DA42 is designed for pilots who truly want to go places - safely and in style.
Features
Garmin GDU 1040, 10 inch primary flight display (PFD)
Garmin GDU 1040, 10 inch multi function display (MFD)
Garmin GEA 71 Airframe / Engine Interface Unit
Dual Garmin GIA 63W with Integrated radio modules with WAAS-certified IFR-approved GPS; VHF navigation with ILS; and VHF communication with 16-watt transceivers
Garmin GMA 1347 digital audio system
Garmin GTX 33 Integrated Mode S Transponder
Garmin GRS 77 Attitude Heading Reference System
Garmin GDC 74 Digital Air Data Computer
Garmin GMU44 Magnetometer
Honeywell KAP 140 Dual Axis Autopilot with Altitude Hold and Preselect
Standby instruments (Compass, Horizon, Air Speed Indicator, Altimeter)
2X Lycoming IO-360 M1A engines (counter rotating) rated at 360 HP total
2X MT 3-blade composite hydraulic constant speed propeller with unfeathering accumulator
Composite airframe and safety seats (up to 26g protection)
Lightning protection system
Fire extinguisher
3 point inertia reel safety harness (all seats)
Instrument lighting
Overhead cabin lights
Standard interior (fabric seats with grey leather trim)
Hydraulic retractable landing gear
Heated pitot / static tube
Alternate static port
Enlarged panoramic canopy
Electric operated flap system
High intensity discharge landing and taxi lights
Position and anti-collision lights
79 US gal fuel tank
4-way Baggage Compartment System
Nose baggage compartment accessible from both sides
Artex ME 406 Mhz ELT
Ground Support Equipment Package
Specifications
AIRCRAFT ITEM
INFORMATION
Engine
2x Lycoming I0-360 fuel injected counter rotating engines equipped with PowerFlow tuned exhaust system
Horsepower
360 hp total
Propellers
2x MT 3-blade composite hydraulic constant speed with unfeathering accumulator
Airworthiness category
Normal
Length
28 ft 1 in
Height
8 ft 2 in
Wing span
44 ft
Maximum take-off weight
3,935 lbs
Useful load
1,180 lbs
Fuel capacity, total / usable
79 gal / 76.4 gal
Fuel
100 LL Avgas
Take-off distance
1,590 ft
Take-off distance, 50-foot obstacle
2,450 ft
Landing ground roll
1,210 ft
Landing distance, 50-foot obstacle
2,410 ft
Rate of climb (MTOW, SL, ISA, Vy: 90kts)
1,400 fpm
Maximum demonstrated operating altitude
18,000 ft
Maximum single-engine ceiling (ROC <50 fpm)
6,400 ft
Maximum speed (Take off power, SL, ISA)
178 kts
Cruise speed at 75% power
162 ktas
Maximum Range (no reserve)
800+ nm
When you take control of the DA42 you are in command of the most technologically advanced twin today. Representing the latest in airframe design, avionics capability and new engine technology, the DA42 is designed for pilots who truly want to go places - safely and in style.
Features
- Garmin GDU 1040, 10 inch primary flight display (PFD)
- Garmin GDU 1040, 10 inch multi function display (MFD)
- Garmin GEA 71 Airframe / Engine Interface Unit
- Dual Garmin GIA 63W with Integrated radio modules with WAAS-certified IFR-approved GPS; VHF navigation with ILS; and VHF communication with 16-watt transceivers
- Garmin GMA 1347 digital audio system
- Garmin GTX 33 Integrated Mode S Transponder
- Garmin GRS 77 Attitude Heading Reference System
- Garmin GDC 74 Digital Air Data Computer
- Garmin GMU44 Magnetometer
- Honeywell KAP 140 Dual Axis Autopilot with Altitude Hold and Preselect
- Standby instruments (Compass, Horizon, Air Speed Indicator, Altimeter)
- 2X Lycoming IO-360 M1A engines (counter rotating) rated at 360 HP total
- 2X MT 3-blade composite hydraulic constant speed propeller with unfeathering accumulator
- Composite airframe and safety seats (up to 26g protection)
- Lightning protection system
- Fire extinguisher
- 3 point inertia reel safety harness (all seats)
- Instrument lighting
- Overhead cabin lights
- Standard interior (fabric seats with grey leather trim)
- Hydraulic retractable landing gear
- Heated pitot / static tube
- Alternate static port
- Enlarged panoramic canopy
- Electric operated flap system
- High intensity discharge landing and taxi lights
- Position and anti-collision lights
- 79 US gal fuel tank
- 4-way Baggage Compartment System
- Nose baggage compartment accessible from both sides
- Artex ME 406 Mhz ELT
- Ground Support Equipment Package
Specifications
| AIRCRAFT ITEM | INFORMATION |
| Engine | 2x Lycoming I0-360 fuel injected counter rotating engines equipped with PowerFlow tuned exhaust system |
| Horsepower | 360 hp total |
| Propellers | 2x MT 3-blade composite hydraulic constant speed with unfeathering accumulator |
| Airworthiness category | Normal |
| Length | 28 ft 1 in |
| Height | 8 ft 2 in |
| Wing span | 44 ft |
| Maximum take-off weight | 3,935 lbs |
| Useful load | 1,180 lbs |
| Fuel capacity, total / usable | 79 gal / 76.4 gal |
| Fuel | 100 LL Avgas |
| Take-off distance | 1,590 ft |
| Take-off distance, 50-foot obstacle | 2,450 ft |
| Landing ground roll | 1,210 ft |
| Landing distance, 50-foot obstacle | 2,410 ft |
| Rate of climb (MTOW, SL, ISA, Vy: 90kts) | 1,400 fpm |
| Maximum demonstrated operating altitude | 18,000 ft |
| Maximum single-engine ceiling (ROC <50 fpm) | 6,400 ft |
| Maximum speed (Take off power, SL, ISA) | 178 kts |
| Cruise speed at 75% power | 162 ktas |
| Maximum Range (no reserve) | 800+ nm |
