Eclipse 500 System Manual page 199

Section 8. Engines & Fire Protection
8.9 Engine and Fire Protection Review Questions
1. What are the four areas that the Aircraft Computer System interfaces with
the Engines & Fire Protection Systems?
a.
b.
c.
d.
2. Where do inputs from the throttles go to?
a. Through the ACS to the FADECs
b. Directly to the FADECs
c. Through the PFD to the ACS to the FADECs
d. Directly to the FMUs
3. During preflight how is the engine oil checked?
a. By using a dipstick on the side of each engine nacelle.
b. By viewing the oil level in the sight gauge.
c. Oil level is displayed on the Engine (ENG) synoptic page.
d. None of the above
4. The minimum battery voltage for a battery only engine start is:
a. 48V
b. 28V
c. 20V
d. 23V
5. FADEC stands for which of the following?
a. Full Authority Digital Engine Controller.
b. Fixed Axis Digital Engine Coupler.
c. Fuel Air Data Engine Controller.
d. None of the above.
6. What are the primary engine sensors?
a.
b.
c.
7. List the two items that the FADEC uses to activate the Automatic Power
Reserve system to automatically activate?
a.
b.
8. APR will increase thrust up to how much on the operating engine in the
event of an engine failure?
a. 25% of takeoff thrust (N1)
b. 110% of takeoff thrust (N1)
Version 2.0 April 2007
Copyright © — Eclipse Aviation Corporation
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