SECTION 7 CESSNA
AIRPLANE AND SYSTEMS DESCRIPTION MODEL
2088 (675 SHP)
ENGINE
(Continued)
CAUTION
THE EMERGENCY POWER LEVER AND ITS
ASSOCIATED MANUAL OVERRIDE SYSTEM ARE
CONSIDERED TO BE AN EMERGENCY SYSTEM AND
SHOULD BE USED ONLY IN THE EVENT OF A FUEL
CONTROL UNIT MALFUNCTION. WHEN
ATTEMPTING A NORMAL START, THE PILOT MUST
ENSURE THAT THE EMERGENCY POWER LEVER IS
IN THE NORMAL (FULL AFT) POSITION;
OTHERWISE, AN OVER-TEMPERATURE CONDITION
MAY RESULT.
WHEN USING THE FUEL CONTROL MANUAL
OVERRIDE SYSTEM, ENGINE RESPONSE MAY BE
MORE RAPID THAN WHEN USING THE POWER
LEVER.
ADD~TIONAL
CARE
IS
REQUIRED
DURING
ENGINE ACCELERATION TO AVOID EXCEEDING
-----
~~~~~
ENGINE LIMITATIONS.
Operation of the emergency power lever is prohibited with the primary
power lever out of the IDLE position. The emergency power lever
overrides normal fuel control functions and results in the direct
operation of the fuel metering valve. The emergency power lever will
override the automatic fuel governing and engine acceleration
scheduling controlled during normal operation by the primary power
lever.
CAUTION
INAPPROPRIATE USE OF THE EMERGENCY POWER
(Continued Next Page)
Revision
23
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