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Exam (elaborations)

AFAB 115 Final Study Guide Latest 2025 Fully Solved

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AFAB 115 Final Study Guide Latest 2025 Fully Solved What does the aircraft structures basic construction consists of? - Answers 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? - Answers relatively equal True or False: the shear strength of the rivet must be greater than the bearing strength of the sheet metal - Answers True What are the parts of an aircraft structure designed to carry loads and or stresses called? - Answers structural members What is a spar? - Answers The wings principle structural member What are the Ailerons, Rudder, and Elevator? - Answers The three Primary flight Control Surfaces of an aircraft What are the three secondary control surfaces? - Answers The Slats, Spoilers, and Flaps. What are the purposes of Slats and Flaps? - Answers To increase the camber of a wing, and increase lift at slower speeds What is the purpose of spoilers? - Answers To slow the aircraft and disrupt the lift of an airfoil. What are structural supports that are under the aircraft skin? - Answers Longerons, bulkheads, and stringers True or False: Longerons do not run the entire length of the aircraft fuselage. - Answers False. (They do run the entire length) What are are tension, compression, torsion, shear, and bending? - Answers The five major stresses that act on an aircraft What is strength? - Answers 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? - Answers The point at which a materials would fail under shear force What is ductility? - Answers The property of a metal, which permits it to be permanently drawn, bent, or twisted into various shape without breaking What is the ability of a material to resist the forces that tend to damage it at the point of applied load called? - Answers bearing strength What does a metal which can be hammered, rolled, or pressed, into various shapes without cracking, breaking, or having some other detrimental effect have? - Answers A high malleability What is brittleness? - Answers The property of a metal, which allows little bending, or deformation without shattering What is the point at which load would cause an initial indication of a permanent distortion called? - Answers yield strength True or false: Tensile strength is measured by the resistance of a material to a force that would tend to pull it apart. - Answers True True or false: The property of metal to return to its natural shape is called ductility. - Answers False

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AFAB 115 Final Study Guide Latest 2025 Fully Solved

What does the aircraft structures basic construction consists of? - Answers 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? - Answers
relatively equal

True or False: the shear strength of the rivet must be greater than the bearing strength of the sheet
metal - Answers True

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

What is a spar? - Answers The wings principle structural member

What are the Ailerons, Rudder, and Elevator? - Answers The three Primary flight Control Surfaces of an
aircraft

What are the three secondary control surfaces? - Answers The Slats, Spoilers, and Flaps.

What are the purposes of Slats and Flaps? - Answers To increase the camber of a wing, and increase lift
at slower speeds

What is the purpose of spoilers? - Answers To slow the aircraft and disrupt the lift of an airfoil.

What are structural supports that are under the aircraft skin? - Answers Longerons, bulkheads, and
stringers

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



(They do run the entire length)

What are are tension, compression, torsion, shear, and bending? - Answers The five major stresses that
act on an aircraft

What is strength? - Answers 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? - Answers The point at which a materials would fail under shear force

What is ductility? - Answers The property of a metal, which permits it to be permanently drawn, bent, or
twisted into various shape without breaking

What is the ability of a material to resist the forces that tend to damage it at the point of applied load
called? - Answers bearing strength

, What does a metal which can be hammered, rolled, or pressed, into various shapes without cracking,
breaking, or having some other detrimental effect have? - Answers A high malleability

What is brittleness? - Answers The property of a metal, which allows little bending, or deformation
without shattering

What is the point at which load would cause an initial indication of a permanent distortion called? -
Answers yield strength

True or false: Tensile strength is measured by the resistance of a material to a force that would tend to
pull it apart. - Answers True

True or false: The property of metal to return to its natural shape is called ductility. - Answers False



(It is called elasticity)

What is The outer covering of an aircraft called? - Answers The skin

What is an example of the bearing strength of a joint being insufficient? - Answers If a bolt were
installed in a hole that was too large, and the head was pulled through the material when torque was
applied

What is a non flammable, chromic acid based coating chemical? - Answers Alodine 1201

What does Alodine 1201 produce? - Answers A chrome conversion coating on aluminum and its alloys

What color is applied Alodine? - Answers gold or tan

What does Applied Alodine do? - Answers It becomes part of the aluminum surface

What does Alodine create? - Answers A chrome conversion coating that allows for both paint adhesion
and corrosion resistance

What is the Alodine Application process? - Answers Clean the part with an approved solvent solution,
water rinse the part after solvent clean, place the part into the Alodine for a specified time, remove the
part and water rinse, allow the part to air dry.

True or false: Material used on aircraft, for the replacement or reinforcement of damage, should always
be weaker material than the original material. - Answers False



(It should never be weaker)

What is an example of negligible damage? - Answers Small dents, scratches, cracks, or holes that can be
sanded or hammered out or repaired without the use of additional material

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