AFAB 115 Final Exam - Questions With Complete
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The aircraft structures basic
1 black cleco 2
construction consists of
the point at which load would
The three secondary control
3 cause an initial indication of a 4
surfaces are
permanent distortion is
Don't know?
Terms in this set (102)
The aircraft structures fuselage, wings, empennage, landing gear, and
basic construction powerplants.
consists of
, The bearing strength of Relatively equal
the sheet metal and the
shear strength of the
rivet should be what?
shear strength of the Greater than the bearing strength of the sheetmetal.
rivet must be what?
The three Primary flight Ailerons, Rudder, and Elevator
Control Surfaces of an
aircraft are
The three secondary Slats, Spoilers, and Flaps.
control surfaces are
What are structural Longerons, bulkheads, and stringers
supports that are under
the aircraft skin.
The ability of a material Strength
to withstand forces,
which tend to deform it in
anydirection, and the
ability of that material to
resist stress without
breaking iscalled its
The point at which a shear strength
materials would fail
under shear force is
the property of a metal, ductility
which permits it to be
permanently drawn, bent,
or twisted into various
shape without breaking is
The ability of a material bearing strength.
to resist the forces that
tend to damage it at
thepoint of applied load
is
Solutions
Save
Practice questions for this set
Learn 1 /7 Study with Learn
5/32
Choose an answer
The aircraft structures basic
1 black cleco 2
construction consists of
the point at which load would
The three secondary control
3 cause an initial indication of a 4
surfaces are
permanent distortion is
Don't know?
Terms in this set (102)
The aircraft structures fuselage, wings, empennage, landing gear, and
basic construction powerplants.
consists of
, The bearing strength of Relatively equal
the sheet metal and the
shear strength of the
rivet should be what?
shear strength of the Greater than the bearing strength of the sheetmetal.
rivet must be what?
The three Primary flight Ailerons, Rudder, and Elevator
Control Surfaces of an
aircraft are
The three secondary Slats, Spoilers, and Flaps.
control surfaces are
What are structural Longerons, bulkheads, and stringers
supports that are under
the aircraft skin.
The ability of a material Strength
to withstand forces,
which tend to deform it in
anydirection, and the
ability of that material to
resist stress without
breaking iscalled its
The point at which a shear strength
materials would fail
under shear force is
the property of a metal, ductility
which permits it to be
permanently drawn, bent,
or twisted into various
shape without breaking is
The ability of a material bearing strength.
to resist the forces that
tend to damage it at
thepoint of applied load
is
