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WorkSheet Part 1 20 Question

Quiz yourself by thinking what should be in each of the black spaces below before clicking on it to display the answer.
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Question
Answer
1. Why is the pulley stop screw on a propeller governor adjustable? - a. To limit the maximum engine speed during takeoff. - b. To maintain the proper blade angle for cruising. - c. To limit the maximum propeller pitch for takeoff.   show
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2. What is the primary purpose of the metal tipping which covers the blade tips and extends along the leading edge of each wood propeller blade? -- a. To increase the lateral strength of the blade. -- b. To prevent impact damage to the tip and leading edge of the blade. c. To increase the longitudinal strength of the blade.   show
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show c. The mechanical limits in the propeller pitch range  
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show b. aircraft velocity and propeller speed  
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show a. Blade back.  
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show a. dowel pins  
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show b. decrease from the tip to the shank  
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8. Blade angle is an angle formed by a line perpendicular to the crankshaft and a line formed by the -- a. relative wind. -- b. chord of the blade. -- c. blade face.   show
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9. Propeller aerodynamic (thrust) imbalance can be largely eliminated by -- a. Correct blade·contouring and angle setting -- b. Keeping the propeller blades within the same plane of rotation -- c. Static balancing -- d. Prevented maintenance on the propeller blades   show
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show b. Maximum efficiency during level flight  
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11. How can a steel propeller hub be tested for cracks? -- a. By anodizing. -- b. By magnetic particle inspection. -- c. By etching.   show
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show c. both 1 and 2 are true  
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13. Propeller blade tracking is the process of determining -- a. the plane of rotation of the propeller with respect to the aircraft longitudinal axis. -- b. that the blade angles are within the specified tolerance of each other. -- c. the positions of the tips of the propeller blades relative to each other.   show
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14. How is the speed of a constant-speed propeller changed in flight? -- a. By varying the output of the governor booster pump. -- b. By advancing or retarding the throttle. -- c. By changing the load tension against the flyweights in the governor.   show
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15. Surface treatment to counter the effects of dye-penetrant inspection on a propeller is accomplished by -- a. washing off with solvent. -- b. wiping with alcohol. -- c. rinse the blade in alodine solution.   show
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16. What would the installation of a propeller governor or feathering system be considered? -- a. Maintenance -- b. Minor repair -- c. Major alteration   show
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17. What are the two ranges of the power level quadrant? -- a. Alpha/Beta -- b. Beta/Delta -- c. Alpha/Charlie -- d. Beta/Charlie   show
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show a. Blade pitch  
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19. It is important that nicks in aluminum alloy propeller blades be repaired as soon as possible in order to -- a. maintain equal aerodynamic characteristics between the blades. -- b. eliminate stress concentration points. -- c. equalize the centrifugal loads between the blades.   show
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20. Inspection of propeller blades by dye-penetrant inspection is accomplished to detect -- a. cracks or other defects. -- b. corrosion at the blade tip. -- c. torsional stress.   show
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Created by: sampizzuto