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EA 400 - Extra Aircraft

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Pilot’s Operating Handbook<br />

<strong>EA</strong> <strong>400</strong><br />

Section 1<br />

General<br />

1.3 Engine<br />

1 Number of Engines: 1<br />

2 Engine Manufacturer: Teledyne Continental Motors<br />

3 Engine Model Number: TSIOL-550-C<br />

4 Engine Type:<br />

Six-cylinder, horizontally opposed, liquid cooled, turbocharged,<br />

intercooled, fuel-injected, direct drive engine, 9014 ccm (550 cubic<br />

inch) displacement.<br />

a Takeoff Power 261 KW (350 BHP) at 2,600 RPM*<br />

b<br />

Maximum Continuous Power:<br />

242 KW (325 BHP) at 2,500 RPM**<br />

*) and 39.5 inches Hg. manifold pressure<br />

**) and 37.5 inches Hg. manifold pressure<br />

1.4 Propeller<br />

1 Number of Propellers: 1<br />

2 Propeller Manufacturer: MT-Propeller<br />

3 Propeller Model Number: MTV-14-D/195-30a<br />

4 Number of Blades: 4<br />

5 Propeller Diameter: 1.95 m (76.77 in.)<br />

6 Propeller Type:<br />

constant speed, hydraulic actuated, pitch range: 26°<br />

1.5 Fuel<br />

1 Fuel Grade:<br />

100 or 100LL (Minimum Grade Aviation Gasoline conforming<br />

to ASTM D910-76 & MIL-G-5572, latest revision)<br />

1 Total Capacity: 468 l (124 U.S. Gallons)<br />

2 Total Usable Fuel: 404 l (107 U.S. Gallons)<br />

3 Unusable Fuel: 64 l (17 U.S. Gallons)<br />

1.6 Oil<br />

1 Oil Grade (SAE):<br />

a All temperatures: SAE 20W-50<br />

b above 4°C (40°F) ambient air (S.L.): SAE 50<br />

Issued: 15. October 1999<br />

1-5

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