Aircraft Hydraulic System Overview

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Questions and Answers

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?

  • 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?

  • 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?

<p>Main control panel (C)</p> Signup and view all the answers

What is the role of hydraulic lines in the hydraulic powerpack system?

<p>To facilitate the movement of hydraulic fluid (C)</p> Signup and view all the answers

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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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