.png){kind=logo}
PDF Download
FREE AND STUDY GAMES ABOUT RODINA-2209 MIDTERM
EXAM QUESTIONS
Actual Qs and Ans Expert-Verified Explanation
This Exam contains:
-Guarantee passing score -91 Questions and Answers -format set of multiple-choice -Expert-Verified Explanation Question 1: Placing a piece of cloth around a stainless steel control cable and running it back and forth over the length of the cable is generally a satisfactory method of inspecting for?
Answer:
broken strands.Question 2: If all instructions issued by the swaging tool manufacturer are followed when swaging a cable terminal, the resultant swaged terminal strength should be?
Answer:
the full rated strength of the cable.Question 3: The dihedral angle of a wing may be measured by placing a straightedge and level protractor on the?
Answer:
front spar.
Question 4: Excessive wear on both of the sides of a control cable pulley groove is evidence of?
Answer:
pulley misalignment.
Question 5: what are Trim tabs ?
Answer:
on the Trailing edge of primary fight control surfaces, Reduces the force needed to move a primary control surface.Question 6: a removable cover or housing placed over or around an aircraft fuselage?
Answer:
cockpit
Question 7: which resource contains the flight control travel limits?
Answer:
TCDS
Question 8: what controls the horizontal movement of an helicopter?
Answer:
cyclic Question 9: The cable-operated control system of an all-metal aircraft, not incorporating a temperature compensating device, has been rigged to the correct tension in a heated hangar. If the aircraft is operated in very cold weather, the cable tension will?
Answer:
decrease when the aircraft structure and cables become cold.
Question 10: what are Servo tabs?
Answer:
on the Trailing edge of primary fight control surfaces, Assists or provides the force for moving a primary flight control.Question 11: If control cables are adjusted properly and the control surfaces tend to vibrate, the probable cause is?
Answer:
worn attachment fittings.
Question 12: how are lift and drag proportional?
Answer:
directly
Question 13: what is an ultimate load?
Answer:
1.5 times the load limit factor
Question 14: the centerline of the fuselage?
Answer:
buttline
Question 15: what is the elevator/ stabilator?
Answer:
Primary flight control on the horizontal stabilizer. controls Pitch movement about the Lateral axes, and controls Longitudinal stability Question 16: what is the removeable cover/housing placed over or around the engine?
Answer:
cowling Question 17: a framework of vertical and longitudinal members covered with a structural skin that carries a large percentage of the stresses imposed on the structure?
Answer:
monocoque
Question 18: fairleads are Teflon or plastic sections that cables can?
Answer:
run across/ rub against
Question 19: The angle of incidence of an airplane at rest?
Answer:
does not change when in flight.
Question 20: During inspection of the flight control system of an airplane equipped with differential-type aileron control, side-to-side movement of the control stick will cause?
Answer:
each aileron to have a greater up travel (from the streamlined position) than down travel.
Question 21: what condition affects cables?
Answer:
temperature.Question 22: a principal longitudinal member of the framing of an aircraft fuselage?
Answer:
longeron Question 23: Where does the breakage of control cable wires occur most frequently?
Answer:
Breakage usually occurs where cables pass over pulleys and through fairleads.
Question 24: what controls the vertical flight of the helicopter?
Answer:
collective Question 25: Washing-in the left wing of a monoplane, for purposes of rigging corrections after flight test, will have what effect on the lift and drag of that wing?
Answer:
Both drag and lift will increase due to increased angle of attack.
Question 26: a stress that tends to crush or press together?
Answer:
compression Question 27: the body of an aircraft to which the wings and tail unit are attached?
Answer:
fuselage
.png)