Section 1. Aircraft Overview
Eclipse 5OO Systems Manual
Copyright
© — Eclipse Aviation Corporation
Version 2.0 April 2007
13
1.8 Aircraft Overview Review Questions
1. The only hydraulic system on the Eclipse 500 is:
a. The flight control system
b. The wheel braking system
c. The landing gear actuators
d. All of the above are hydraulically operated
2. What material is the primary aircraft structure composed of?
a. Plastic
b. Fiberglass
c. Titanium
d. Aluminum
3. Describe how to remove seats from the Eclipse 500:
4. The useful load of the Eclipse 500 is:
a. 2,250
lbs
b. 2,500
lbs
c. 2,266
lbs
d. None of the above
5. Maximum Zero Fuel Weight is:
a. 5,000
lbs
b. 4,000
lbs
c. 4,860
lbs
d. None of the above
6. The maximum operating altitude for the Eclipse 500 is:
a. FL
250
b. FL
500
c. FL
250
d. FL
410
7. The design life of the Eclipse 500 is 20,000 hours or:
a. 18,183
cycles
b. 35
years
c. 40
years
d. 20,000
cycles
8. The single engine service ceiling is:
a. 25,000
feet
b. 35,000
feet
c. 41,000
feet
d. None of the above
9. What are the four major functional areas that comprise the Eclipse 500?
a.
b.