JPE 02 H Hybrid

General Information

Fuel Diesel fuel
Engine type 4 in line – turbo diesel common rail engine
Bore mm 75
Stroke mm 88.3
Cubic capacity 1540 cc
Peak chamber pressure 180 bar
Power output (EEC)

Hybrid Kw 177 ( 230 Hp )@ 3700 rpm for 30’’

            Kw 154 ( 200 Hp )@3700 rpm for 3 Min

            Variable from 116 up to 160 Kw 10 Min

kW 115 (150HP) @3.700 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 1000
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 150

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.Maximum allowable oil consumption 1kg every 25h.Maximum allowable 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 actuator
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.

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