General Information
| Fuel | Diesel fuel |
| Engine type | 4 in line – Diesel turbo diesel common rail engine |
| Bore mm | 75 |
| Stroke mm | 88.3 |
| Cubic capacity | 1540 cc |
| Peak chamber pressure | 180 bar |
| Power output (EEC) | kW 115(150HP)@3.650 rpm(crankshaft)/2,300 rpm kW 105 (136HP)@3000 rpm(crankshaft) continuous power |
| BestSFC @max power output | 150 gr/HPh (203gr/kWh) from 5% to 95% power output |
| BestSFC @max power output | 160 gr/HPh (218 gr/kWh) from 95% to 100% power output |
| Idle speed | rpm 1100 |
| Max. engine speed | rpm 4000 |
Dimensions
| Overall length | mm 776 |
| Overall width | mm 571 |
| Overall height | mm 592 |
Weights
| Complete ConfigurationWith alternator, gear box,starter, etc | Kg 120 |
Other Informations
| Timing system | Single level FADEC with Engine parameters Monitorcapability, UAV1553B Bus communication system,capability for compliances with DO178-B |
| Oil lubrication andcooling | 1 mechanically gearedmaximum pressure allowed 6 bar. Oil consumption 40 gramms/hour. Maximum temperature 160°C |
| Oil type and quantity | SAE 5W30 synthetic oil API SL/CF ACEA A3/B3/B4Mercedes Benz 229.3, 4.5 kg |
| Oil filter | Internal cartridge type |
| PRSU (Prop. Red. Speed Unit) |
1.6:1 ratio, Electric Pitch control |
| Temperature range | +/- 55°C ISA |
| Fuel injection | Fully electronic, 1 injectors per cylinder. DC supply with onboard aircraft battery and aircraft DC generator. |
| Engine mounts | Rubber shock mounts required. |
| Service angles | Bank: 20°.Pitch: +25°/-25° |
| G loads | According to FAA 1.1 and 23.3 aerobatic categoryInverted flight allowed only with special kit |
| TBO | 2,000h for standard use. |
Low Power Engine Comparison
| FUEL USED | MTOP/FF | MCP/FF | ECONOMY/FF | WEIGHT | TBO | |
|---|---|---|---|---|---|---|
| CONTINENTAL Centurion testuali |
Diesel (EN 590), Jet A, Jet A-1 |
99 Kw (128 hp) 5,5 gal/h (21 l/h) |
99 Kw (128 hp) 5,5 gal/h (21 l/h) |
71 Kw (92 hp) 4 gal/h (15 l/h) |
134 Kg (295 Lbs) |
1500 |
| LYNCOMNING 0-320 |
Fuel grade, octane 80/87 |
115 Kw (150 hp) 11 gal/h (35 l/h) |
110 Kw (143 hp) 10 gal/h (32 l/h) |
97 Kw (126 hp) 8,8 gal/h (33 l/h) |
126 Kg (279 Lbs) |
2000 |
| ROTAX 912 UL | Fuel grade, octane 80/87 |
84,5 Kw (140 hp) 8 gal/h (30 l/h) |
60 Kw (78 hp) 4 gal/h (15 l/h) |
60 Kw (78 hp) 4 gal/h (15 l/h) |
75 Kg (165 Lbs) |
2000 |
| DIESEL JET GA 1.4 8V |
Diesel (EN 590), Jet A, Jet A-1 |
88,4 Kw (115 hp) 6,5 gal/h (24,7 l/h) |
86 Kw (110 hp) 6 gal/h (23 l/h) |
70 Kw (90 hp) 4,5 gal/h (18 l/h) |
85 Kg (187 Lbs) |
N.A. |
| AUSTROENGINE AE300 | Diesel (EN 590), Jet A, Jet A-1 |
123,5 Kw (160 hp) 9,4 gal/h (35,1 l/h) |
114 Kw (148 hp) 8,3 gal/h (31,5 l/h) |
90 Kw (117 hp) 5,5 gal/h (21 l/h) |
185 Kg (407 Lbs) |
2000 |
| P2M JPE01 | Diesel (EN 590), Jet A, Jet A-1 |
115 Kw (150 hp) 6 gal/h (23 l/h) |
95 Kw (123 hp) 4,7 gal/h (18 l/h) |
65 Kw (85 hp) 3,2 gal/h (12 l/h) |
120Kg (265 Lbs) |
2000 |
| P2M JPE H 02 | Diesel (EN 590), Jet A, Jet A-1 |
155 Kw (201 hp) 6 gal/h (23 l/h) |
95 Kw (123 hp) 4,7 gal/h (18 l/h) |
65 Kw (85 hp) 3,2 gal/h (12 l/h) |
150 Kg (330 Lbs) |
2000 |
| best fuel consumption | ||||||
Who's using our Engines?
A question very commonly asked is: “Which aircraft already use this Engine?”.
To provide prospective buyers with an answer to this question, we will be relying on the help of our customers to provide us with pictures and comments regarding their particular engine installation. Not all installations are published here as we only wish to show pictures with consent of the owner.
