Envoy Flight Attendant Training LATEST EXAM ALL QUESTIONS AND CO
RECT DETAILED ANSWERS WITH (VERIFIED ANSWERS) |ALREADY GRADE
A+
Study online at https://quizlet.com/_h6e25n
1. Theory of Flight: Lift, Gravity, Thrust, and Drag
The four forces
2. Lift upward force
3. Gravity (or downward force
weight)
4. Thrust forward force
5. Drag resisting force
6. In order to take thrust, lift, weight, and drag
off, the aircraft's
__ and __ must be
sufficient to over-
come its __and __.
7. The pilot guides ailerons, elevators, and rudder
and controls the
aircraft by con-
trolling its pitch,
roll, and yaw via
the control sur-
faces. These in-
clude the __ , __ ,
and __.
8. To land, an air- thrust, drag, weight.
craft's __ must
be reduced safely
1/6
, Envoy Flight Attendant Training LATEST EXAM ALL QUESTIONS AND CO
RECT DETAILED ANSWERS WITH (VERIFIED ANSWERS) |ALREADY GRADE
A+
Study online at https://quizlet.com/_h6e25n
below its __, as its
lift is reduced to
levels less than its
__.
9. Fuselage (body) a rigid structure on which the aircraft components, e.g., wing, tail, engine, etc., are
mounted
10. Nose the forward section of an aircraft. It includes the flightdeck where the captain and
first officer sit
11. Nacelle the protective covering surrounding the aircraft engine
12. Aileron hinged portion on the trailing edge of the wing. It raises and lowers to
control the rolling motion of the aircraft.
13. Flaps hinged portion of the wing
located on the trailing (back) edges, covering the section of the wing from the
fuselage to the aileron. Flaps provide additional lift to compensate for the slower
air speeds associated with landing.
14. Elevators moveable control surfaces hinged to the horizontal stabilizer, which control pitch
or position of the nose of the aircraft relative to the horizon
15. Rudder located on the tail section. Controls the left to right movement of the aircraft
("yaw").
16. Horizontal and located in the tail section, contributes to the aircraft's stability. The horizontal
Vertical Stabilizer stabilizers can be adjusted to align the aircraft's flight path angle according to
existing wind conditions. Additional control comes from the vertical stabilizer.
17. Landing gear
2/6
RECT DETAILED ANSWERS WITH (VERIFIED ANSWERS) |ALREADY GRADE
A+
Study online at https://quizlet.com/_h6e25n
1. Theory of Flight: Lift, Gravity, Thrust, and Drag
The four forces
2. Lift upward force
3. Gravity (or downward force
weight)
4. Thrust forward force
5. Drag resisting force
6. In order to take thrust, lift, weight, and drag
off, the aircraft's
__ and __ must be
sufficient to over-
come its __and __.
7. The pilot guides ailerons, elevators, and rudder
and controls the
aircraft by con-
trolling its pitch,
roll, and yaw via
the control sur-
faces. These in-
clude the __ , __ ,
and __.
8. To land, an air- thrust, drag, weight.
craft's __ must
be reduced safely
1/6
, Envoy Flight Attendant Training LATEST EXAM ALL QUESTIONS AND CO
RECT DETAILED ANSWERS WITH (VERIFIED ANSWERS) |ALREADY GRADE
A+
Study online at https://quizlet.com/_h6e25n
below its __, as its
lift is reduced to
levels less than its
__.
9. Fuselage (body) a rigid structure on which the aircraft components, e.g., wing, tail, engine, etc., are
mounted
10. Nose the forward section of an aircraft. It includes the flightdeck where the captain and
first officer sit
11. Nacelle the protective covering surrounding the aircraft engine
12. Aileron hinged portion on the trailing edge of the wing. It raises and lowers to
control the rolling motion of the aircraft.
13. Flaps hinged portion of the wing
located on the trailing (back) edges, covering the section of the wing from the
fuselage to the aileron. Flaps provide additional lift to compensate for the slower
air speeds associated with landing.
14. Elevators moveable control surfaces hinged to the horizontal stabilizer, which control pitch
or position of the nose of the aircraft relative to the horizon
15. Rudder located on the tail section. Controls the left to right movement of the aircraft
("yaw").
16. Horizontal and located in the tail section, contributes to the aircraft's stability. The horizontal
Vertical Stabilizer stabilizers can be adjusted to align the aircraft's flight path angle according to
existing wind conditions. Additional control comes from the vertical stabilizer.
17. Landing gear
2/6
