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Questions and Answers
What is the primary function of the hydraulic powerpack in the airplane?
What is the primary function of the hydraulic powerpack in the airplane?
- To control the airplane's navigation systems
- To operate the landing gear retraction system (correct)
- To generate electrical power for the cockpit instruments
- To provide hydraulic pressure to the brake system
Which components are included in the hydraulic system covered in the chapter?
Which components are included in the hydraulic system covered in the chapter?
- Hydraulic lines and electrical controls
- Brake system and hydraulic powerpack
- Landing gear free fall valve and hydraulic lines (correct)
- Brake system and reservoir
What is true about the airplane's brake system in relation to the hydraulic system discussed?
What is true about the airplane's brake system in relation to the hydraulic system discussed?
- It is powered by the battery system of the airplane
- It operates using the same hydraulic lines as the landing gear
- It is dependent on the hydraulic powerpack for operation
- It has an independent hydraulic system (correct)
Which component is not part of the hydraulic system described in the chapter?
Which component is not part of the hydraulic system described in the chapter?
What is the role of hydraulic lines in the hydraulic powerpack system?
What is the role of hydraulic lines in the hydraulic powerpack system?
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Study Notes
Aircraft Hydraulic System
- The hydraulic powerpack (pump) is electrically operated.
- The hydraulic system covers the hydraulic powerpack (pump) and reservoir.
- The hydraulic system also includes hydraulic lines.
- The landing gear free fall valve and actuating cylinders are covered under 32-30-00.
- The brake system uses a separate hydraulic system.
- This chapter focuses on the gear retraction system and does not cover the brake system.
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