Flight Controls Review Questions - Eclipse 500 System Manual

Section 3. Flight Controls

3.9 Flight Controls Review Questions

1. The flight control system on the Eclipse 500 is:
a. A fly-by-wire system which uses an on-board flight computer and flight
control servo motors for each individual primary flight controls.
b. A mechanical system that uses cables, pulleys, bell cranks, and pushrods.
c. Hydraulically controlled.
d. None of the above.
2. What are two components of the Flight Control System that have Aircraft
Computer System interfaces?
a.
b.
3. The trim system on the Eclipse 500 is best described as:
a. Electrically powered and operated.
b. Manually powered via a mechanically operated trim wheel.
c. Pitch trim is electronically powered; aileron and rudder trim are both powered
manually via a mechanically operated trim wheel.
d. None of the above.
4. The flaps on the Eclipse 500 are best described as:
a. Hydraulically powered fowler flaps.
b. Electrically powered fowler flaps.
c. Pneumatically powered fowler flaps.
d. Manually powered fowler flaps.
5. Vfe for flaps in the T/O (takeoff) position is:
a. 150 KEAS
b. 175 KEAS
c. 120 KEAS
d. 200 KEAS
6. Vfe for flaps in the LDG (landing) position is:
a. 120 KEAS
b. 150 KEAS
c. 200 KEAS
d. 175 KEAS
7. List the functions of the All Interrupt switch:
a.
b.
c.
d.
e.
f.
Version 2.0 April 2007
Copyright © — Eclipse Aviation Corporation
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