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AFAB 115 Final Study Guide Questions and Answers

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What does the aircraft structures basic construction consists of? o :## The fuselage, wings, empennage, landing gear, and powerplants. What should the bearing strength of the sheet metal and the shear strength of the rivet be? o :## relatively equal True or False: the shear strength of the rivet must be greater than the bearing strength of the sheet metal o :## True What are the parts of an aircraft structure designed to carry loads and or stresses called? o :## structural members What is a spar? o :## The wings principle structural member What are the Ailerons, Rudder, and Elevator? o :## The three Primary flight Control Surfaces of an aircraft What are the three secondary control surfaces? 2024/2025 2 | P a g e o :## The Slats, Spoilers, and Flaps. What are the purposes of Slats and Flaps? o :## To increase the camber of a wing, and increase lift at slower speeds What is the purpose of spoilers? o :## To slow the aircraft and disrupt the lift of an airfoil. What are structural supports that are under the aircraft skin? o :## Longerons, bulkheads, and stringers True or False: Longerons do not run the entire length of the aircraft fuselage. o :## False. (They do run the entire length) What are are tension, compression, torsion, shear, and bending? o :## The five major stresses that act on an aircraft What is strength? 2024/2025 3 | P a g e o :## The ability of a material to withstand forces, which tend to deform it in any direction, and the ability of that material to resist stress without breaking What is shear strength? o :## The point at which a materials would fail under shear force What is ductility? o :## The property of a metal, which permits it to be permanently drawn, bent, or twisted into various shape without breaking

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AFAB 115
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Uploaded on
September 2, 2024
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Written in
2024/2025
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AFAB 115 Final Study Guide Questions and Answers
What does the aircraft structures basic construction consists of?

o :## The fuselage, wings, empennage, landing gear, and powerplants.




What should the bearing strength of the sheet metal and the shear strength of the rivet

be?

o :## relatively equal




True or False: the shear strength of the rivet must be greater than the bearing strength of

the sheet metal

o :## True




What are the parts of an aircraft structure designed to carry loads and or stresses called?

o :## structural members




What is a spar?

o :## The wings principle structural member




What are the Ailerons, Rudder, and Elevator?

o :## The three Primary flight Control Surfaces of an aircraft




What are the three secondary control surfaces?

, 2024/2025 2|Page


o :## The Slats, Spoilers, and Flaps.




What are the purposes of Slats and Flaps?

o :## To increase the camber of a wing, and increase lift at slower speeds




What is the purpose of spoilers?

o :## To slow the aircraft and disrupt the lift of an airfoil.




What are structural supports that are under the aircraft skin?

o :## Longerons, bulkheads, and stringers




True or False: Longerons do not run the entire length of the aircraft fuselage.

o :## False.




(They do run the entire length)




What are are tension, compression, torsion, shear, and bending?

o :## The five major stresses that act on an aircraft




What is strength?

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