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Aerospace Engineering: Wing and Fuel Systems

10 Questions

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Aerospace Engineering: Wing and Fuel Systems

Created by

@IndulgentProsperity

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Questions and Answers

What type of structure is each wing panel described as?

Composite, partial monocoque type

Full cantilever, semi-monocoque type (correct)

Semi-empirical, all metal type

Lattice, fully integrated type

What is the total fuel capacity of each engine's fuel tank?

54 U.S. gallons

120 U.S. gallons

50 U.S. gallons

108 U.S. gallons (correct)

How are the wings attached to the fuselage?

By inserting the butt ends of the main spars into a spar box (correct)

By bolts through the leading edge

By using adhesive bonding techniques

By welding to the fuselage frame

What structural component provides a continuous main spar?

Spar box carry through Signup and view all the answers

Which components are attached to each wing?

Aileron, flap, main landing gear, and powerplant Signup and view all the answers

How is feathering of a propeller achieved?

By moving the control fully aft into the FEATHER position Signup and view all the answers

What is the approximate time it takes for feathering to occur?

Six seconds Signup and view all the answers

What initiates the unfeathering process of a propeller?

Moving the propeller control forward Signup and view all the answers

What happens after the propeller control is moved forward during unfeathering?

The starter engages until the propeller is windmilling Signup and view all the answers

Where are the propeller control levers located?

In the center of the power control quadrant Signup and view all the answers

Study Notes

Wing Structure

Each wing panel is constructed of metal, employing a semi-monocoque design.
The wings are designed with removable tips and access panels for maintenance.
The aileron, flap, main landing gear, and powerplant are all attached to the wing panels.
The wings are attached to the fuselage by inserting the main spars into a spar box carry through.
This spar box serves as a continuous main spar, connecting the two wings.

Fuel System

Each engine nacelle is equipped with a bladder-type fuel tank.
Each fuel tank holds 54 U.S. gallons.
The total fuel capacity of both tanks is 108 U.S. gallons.

Propeller Control

Propeller control levers are located in the center of the power control quadrant.
Moving the control fully aft through the low RPM detent, into the FEATHER position, feathers the propeller.
Feathering takes approximately six seconds.
Unfeathering is accomplished by moving the propeller control forward and engaging the starter until the propeller is wind milling.

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Description

This quiz covers the essential components of wing structures and fuel systems in aerospace engineering. Learn about the semi-monocoque design of wings and the specifications of fuel tank capacities. Perfect for students looking to understand aircraft design and functionality.