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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 />

Wind<br />

The wind velocities recorded as variables on the charts of this<br />

Handbook are to be understood as the headwind or tailwind components<br />

of the reported winds.<br />

1.12c Power Terminology<br />

Takeoff Power<br />

Maximum<br />

Continuous<br />

Power (MCP)<br />

Idle Power<br />

The maximum power permissible for takeoff (may be time limited).<br />

The maximum power for unrestricted periods of use.<br />

The power required to run an engine at the lowest speed that will<br />

ensure satisfactory engine operation.<br />

1.12d Engine Controls and Instruments<br />

Throttle or<br />

Power Control<br />

Lever<br />

Propeller<br />

Control<br />

Mixture<br />

Control<br />

EGT Gauge<br />

TIT Gauge<br />

Tachometer<br />

The lever used to control engine power, from the lowest through<br />

the highest power, by controlling the air and the fuel flow. The extreme<br />

lever positions are called OPEN (forward position) and<br />

CLOSE (aft position).<br />

The lever used to select the propeller blade angle of attack. It provides<br />

a mechanical linkage to the propeller governor. In the<br />

FULL AFT position of the lever the angle of attack is high, in the<br />

FULL FORWARD position it is low.<br />

The mixture control provides a mechanical linkage with the mixture<br />

control valve of the fuel control unit, to adjust the air/fuel<br />

mixture. It is also a primary means to shut down the engine. The<br />

most forward position of the mixture control lever is called<br />

RICH, the aft position is called IDLE/CUT-OFF.<br />

The exhaust gas temperature indicator is the instrument used to<br />

identify the lean fuel flow mixtures for various power settings.<br />

A temperature measuring system that senses exhaust gas temperature<br />

at the turbine inlet.<br />

An instrument that indicates rotational speed. The speed is shown<br />

as propeller revolutions per minute (RPM).<br />

Issued: 15. October 1999<br />

1-9

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