Eclipse 500 System Manual page 200

Section 8. Engines & Fire Protection
c. 110 RPMs
d. 30% N
9. The PW-610F-A engine has how many rotors (spools)?
a. One
b. Two
c. Three
d. None of the above
10. How many channels does EACH FADEC have?
a. 4
b. 1
c. 2
d. 3
11. CONT IGN does which of the following?
a. Provides continuous ignition to prevent engine flameout.
b. Enables automatic control of continuous ignition as required by the FADEC.
c. Turns off the FADEC
d. None of the above
12. The purpose of engine dry motoring is to:
a. Start the engine quietly.
b. Pump excess fuel out of the engine by running it without adding fuel.
c. Provide engine cooling following long periods of operation.
d. None of the above.
13. How can the engines be turned off?
a. By pressing the FIRE/ARMED button once
b. By selecting CONT IGN for both engines using the engine rotary switch.
c. By selecting OFF for both engines on the engine rotary switch.
d. Both A & C
14. Fire suppression for each engine is provided by:
a. A fire extinguisher located in the cockpit.
b. PhostrEx canisters installed in each pylon
c. Four Halon bottles placed outside of the pressure vessel
d. There is no specific fire suppression system for the engines.
15. The minimum temperature for engine start is:
a. 0° F
b. -15° C
c. -25° F
d. -20° C or -4° F
16. List the three sources of power for the FADEC units:
a.
b.
c.
17. What is engine bleed air from the inboard P3 bleed port on the engine used
for?
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Copyright © — Eclipse Aviation Corporation
Eclipse 5OO Systems Manual
Version 2.0 April 2007