Informazioni Generali
| Fuel | JET-A-1, Chinese Jet Fuel No.3, TS-1, JB-8, JP-8+100, Diesel (EN590 ) |
| Engine type | 4 in line – turbo diesel common rail engine |
| Bore mm | 83 |
| Stroke mm | 99 |
| Cubic capacity | 2143 cc |
| Peak chamber pressure | 160 bar |
| Power output (EEC) | Max Power 300 Hp (188 Kw))@4,000 rpm (crankshaft) Continuous Power 250HP ( 192 Kw ) @3500 rpm (crankshaft) |
| BestSFC @max power | 150 gr/HPh (203gr/kWh) from 5% to 95% power output |
| Idle speed | rpm 800 |
| Max. engine speed | rpm 4000 |
Dimensioni
| Lunghezza | mm 871 |
| Larghezza | mm 560 |
| Altezza | mm 698 |
Pesi
| a secco con alternatore standard 12V/8A | Kg 160 |
| Pronto al volo con alternatore, riduttore,starter, etc | Kg 175 |
Ulteriori informazioni
| Timing system | Single level FADEC with Engine parameters Monitorcapability, UAV1553B Bus communication system, capability for compliances with DO178-B |
| Cooling | 70% in weight Ethylene Glycol – 30% Water (kg 1.2 inside the engine)Mechanical water pumpMaximum pressure allowed 1.5 barMax allowable temperature 115°C |
| Oil lubrication and cooling |
Internal heat exchanger mechanically geared. |
| Oil type and quantity | SAE 5W30 synthetic oil API SL/CF ACEA A3/B3/B4 Mercedes Benz 229.3, 4.5 kg |
| Oil filter | Internal cartridge type |
| PRSU (Prop. Red. Speed Unit) | / |
| Temperature range | +/- 55 deg C |
| Fuel injection | -50°C/+55°C ISACRDI System FADEC controlled |
| Engine mounts | Rubber shock mounts required. |
| Service angles | Rubber shock mounts required.Bank: 60°.Pitch: +45°/-45° |
| G loads | +7 / – 2 |
| TBO | According to FAA 1.1 and 23.3 aerobatic category.Inverted flight allowed only with special kit.2,000h for standard use. |
Comparazione Propulsori
| FUEL USED | MTOP/FF | MCP/FF | ECONOMY/FF | WEIGHT | TBO | |
|---|---|---|---|---|---|---|
| LYNCOMING 0-540 A | Fuel grade, octane 80/87 |
192 Kw (250 hp) 20,5 gal/h (77 l/h) |
176 Kw 230 hp) 16,5 gal/h (62 l/h) |
146 Kw (190 hp) 15 gal/h (56 l/h) |
185 Kg (405 Lbs) |
2000 |
| LYNCOMING 0-5450 S | Fuel grade, octane 80/87 |
230 Kw (300 hp) 24 gal/h (90 l/h) |
190 Kw (250 hp) 21 gal/h (79 l/h) |
173 Kw (225 hp) 16 gal/h (60 l/h) |
213 Kg (475 Lbs) |
1800 |
| Continental TSIO-550 | Fuel grade, octane 80/87 |
230 Kw (300 hp) 24 gal/h (90 l/h) |
N.A. | N.A. | 226 Kg (497 Lbs) |
N.A. |
| Safram SR305 | Diesel (EN 590), Jet A, Jet A-1 |
174 Kw (227 hp) 10,6 gal/h (38 l/h) |
150 Kw (195 hp) 8 gal/h (30 l/h) |
125 Kw (162 hp) 6,5 gal/h (25 l/h) |
205 Kg (455 Lbs) |
2400 |
| P2M JPE03 | Diesel (EN 590), Jet A, Jet A-1 |
190 Kw (247 hp) 10 gal/h (38 l/h) |
170 Kw (221 hp) 9 gal/h (34 l/h) |
154 Kw (200 hp) 8,2 gal/h (31 l/h) |
160 Kg (353 Lbs) |
2000 |
| P2M JPE H 04 | Diesel (EN 590), Jet A, Jet A-1 |
239 Kw (312 hp) 10 gal/h (38 l/h) |
170 Kw (221 hp) 9 gal/h (34 l/h) |
154 Kw (200 hp) 8,2 gal/h (31 l/h) |
180 Kg (397 Lbs) |
2000 |
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.
