The DA 150 has been the benchmark for power and reliability since the early 1990's. The 150L was introduced in April of 2013 with DA's new reed block and some other weight saving refinements. The 150L is now 6 oz lighter.
- 375 g lighter compared to the DA-150
- Thinner cooling fins for better cooling and weight reduction
- Even better throttle response due to the reduced crankcase volume
- Aerobatic power curve
- Low vibration due to computer simulation aided design
- The cylinder, piston and crankshaft are developed by Desert Aircraft
- CNC milled, 7075 aluminum alloy crankcase.
- Long conrod with gudgeon pin set very near piston crown for reduced side load
- Three crank bearings, long spacing between front bearings
- Four petal reed valve, bottom induction
- Walbro Carburetor
- Battery ignition with automatic advance and retard
- DA engines are designed using the latest tools and techniques,including 3D CAD and Stereo Lithography
- Displacement: 150 ccm
- Bore: 49 mm
- Stroke: 40 mm
- Weight: 3325 g
- including Ignition: 3470 g
- Output: 12,3 kW / 16,5 PS
- RPM Range: 1000 - 6500 1/min
- Max RPM: 8500 1/min
- Propellers:
- 2-Blade: 30x10, 30x12, 31x12, 32x10
- 3-Blade: 28.5x12, 29x12
| desert_aircraft_da150_views.pdf |
| da_150_manual_2-14-2013.pdf |