JPE 04 H Hybryd

General Information

Fuel Diesel fuel/jp4/jetA1
Engine type 4 in line –  turbo diesel common rail engine
Bore mm 82
Stroke mm 90.4
Cubic capacity 1910 cc
Peak chamber pressure 180 bar
Power output (EEC)

Hybrid Kw 230 ( 300 Hp )@ 4300 rpm for 30’’

            Kw 192 ( 250 Hp )@3700 rpm for 3 Min

            Variable from 155 up to 230 Kw 10 Min

154 Kw (200HP)@4.300 rpm (crankshaft)

130 Kw (180HP)@3700 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 1000
Max. engine speed rpm 4500

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.

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