Aircraft Overview - Eclipse 500 System Manual

Section 1. Aircraft Overview
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.
Version 2.0 April 2007
Copyright © — Eclipse Aviation Corporation
Eclipse 5OO Systems Manual
13