AFAB 115 Final Exam Questions With
Correct Answers
The aircraft structures basic construction consists of
| | | | | |
fuselage, wings, empennage, landing gear, and powerplants.
| | | | | |
The bearing strength of the sheet metal and the shear strength of the rivet
| | | | | | | | | | | | | |
should be what?
| |
Relatively equal |
shear strength of the rivet must be what?
| | | | | | |
Greater than the bearing strength of the sheetmetal.
| | | | | | |
The three Primary flight Control Surfaces of an aircraft are
| | | | | | | | |
Ailerons, Rudder, and Elevator
| | |
The three secondary control surfaces are
| | | | |
Slats, Spoilers, and Flaps.
| | |
,What are structural supports that are under the aircraft skin.
| | | | | | | | |
Longerons, bulkheads, and stringers
| | |
The ability of a material to withstand forces, which tend to deform it in
| | | | | | | | | | | | | |
anydirection, and the ability of that material to resist stress without breaking
| | | | | | | | | | | |
iscalled its|
Strength
The point at which a materials would fail under shear force is
| | | | | | | | | | |
shear strength
|
the property of a metal, which permits it to be permanently drawn, bent, or
| | | | | | | | | | | | | |
twisted into various shape without breaking is
| | | | | |
ductility
The ability of a material to resist the forces that tend to damage it at thepoint of
| | | | | | | | | | | | | | | | |
applied load is
| |
bearing strength.
|
, A metal which can be hammered, rolled, or pressed, into various shapeswithout
| | | | | | | | | | | |
cracking, breaking, or having some other detrimental effect has
| | | | | | | |
high malleability.
|
The property of a metal, which allows little bending, or deformation
| | | | | | | | | | |
withoutshattering, is |
brittleness
the point at which load would cause an initial indication of a permanent
| | | | | | | | | | | | |
distortion is |
yield strength
|
What is measured by the resistance of a material to a force that would tend to
| | | | | | | | | | | | | | | |
pull it apart
| |
Tensile strength |
The property of metal to return to its natural shape is
| | | | | | | | | |
elasticity
Correct Answers
The aircraft structures basic construction consists of
| | | | | |
fuselage, wings, empennage, landing gear, and powerplants.
| | | | | |
The bearing strength of the sheet metal and the shear strength of the rivet
| | | | | | | | | | | | | |
should be what?
| |
Relatively equal |
shear strength of the rivet must be what?
| | | | | | |
Greater than the bearing strength of the sheetmetal.
| | | | | | |
The three Primary flight Control Surfaces of an aircraft are
| | | | | | | | |
Ailerons, Rudder, and Elevator
| | |
The three secondary control surfaces are
| | | | |
Slats, Spoilers, and Flaps.
| | |
,What are structural supports that are under the aircraft skin.
| | | | | | | | |
Longerons, bulkheads, and stringers
| | |
The ability of a material to withstand forces, which tend to deform it in
| | | | | | | | | | | | | |
anydirection, and the ability of that material to resist stress without breaking
| | | | | | | | | | | |
iscalled its|
Strength
The point at which a materials would fail under shear force is
| | | | | | | | | | |
shear strength
|
the property of a metal, which permits it to be permanently drawn, bent, or
| | | | | | | | | | | | | |
twisted into various shape without breaking is
| | | | | |
ductility
The ability of a material to resist the forces that tend to damage it at thepoint of
| | | | | | | | | | | | | | | | |
applied load is
| |
bearing strength.
|
, A metal which can be hammered, rolled, or pressed, into various shapeswithout
| | | | | | | | | | | |
cracking, breaking, or having some other detrimental effect has
| | | | | | | |
high malleability.
|
The property of a metal, which allows little bending, or deformation
| | | | | | | | | | |
withoutshattering, is |
brittleness
the point at which load would cause an initial indication of a permanent
| | | | | | | | | | | | |
distortion is |
yield strength
|
What is measured by the resistance of a material to a force that would tend to
| | | | | | | | | | | | | | | |
pull it apart
| |
Tensile strength |
The property of metal to return to its natural shape is
| | | | | | | | | |
elasticity
