JPE04 IS A FAMILY OF FOUR -STROKE, 4-CYLINDER IN LINE, COMMON RAIL DIRECT INJECTION SYSTEM, TURBO CHARGED, LIQUID COOLED, AIR SHUT OFF VALVE, BELT REDUCTION GEAR ENGINE, WITH HYBRID CONFIGURATION HAD MAX POWER OF 400 HP UP TO 5 MIN.
General Information
| 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) | hYBRID Max Power 400 Hp (308 Kw))@4,000 rpm (crankshaft) Continuous Power 300HP ( 230 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 |
Dimensions
| Overall length | mm 871 |
| Overall width | mm 560 |
| Overall height | mm 698 |
Weights
| dry with DC generator 12V/8A | Kg 180 |
| Complete ConfigurationWith alternator, gear box,starter, etc | Kg 195 |
Other Informations
| 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 pump Maximum pressure allowed 1.5 bar Max allowable temperature 115°C |
| Oil lubrication and cooling | Internal heat exchanger.1 mechanically geared. Maximum pressure allowed 6 bar. Maximum allowable oil consumption 1kg every 25h. Maximum allowable temperature 130°C |
| 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. |
High Power Engine Comparison
| 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 |
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.
