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AFAB 115 Final Study Guide Questions with 100% Correct Answers

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AFAB 115 Final Study Guide Questions with 100% Correct Answers

Institution
AFAB 115
Course
AFAB 115

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AFAB 115 Final Study Guide Questions
with 100% Correct Answers

What is ductility? - Answer-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? - Answer-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? - Answer-A
high malleability

What is brittleness? - Answer-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? - Answer-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. - Answer-True

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

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

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

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

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

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

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

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

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

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

(They do run the entire length)

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

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

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

(It is called elasticity)

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

What is an example of the bearing strength of a joint being insufficient? - Answer-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? - Answer-Alodine 1201

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

What color is applied Alodine? - Answer-gold or tan

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

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