Informazioni Generali
| 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 |
Dimensioni
| Lunghezza | mm 776 |
| Larghezza | mm 571 |
| Altezza | mm 592 |
Pesi
| Pronto al volo con alternatore, riduttore,starter, etc | Kg 120 |
Ulteriori informazioni
| 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. |
Comparazione Propulsori
| 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 | ||||||
Chi utilizza i nostri Motori?
Una domanda molto comune è : “su quali velivoli è attualmente installato il vostro motore?”
Per fornire ai potenziali acquirenti una risposta a questa domanda, contiamo sull’aiuto dei nostri clienti per fornirci immagini e commenti riguardo la loro particolare installazione. Su questo sito non sono pubblicate le immagini e le informazioni di tutte le installazioni in accordo con il consenso d’uso concesso.
