Practice Quiz

FAA Private Pilot Test Prep - Question List

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91. Ground resonance is most likely to develop when
  1. Taking off in a calm wind
  2. Landing in gusty winds
  3. When a hard landing causes shocks to the helicopter, thereby causing the rotor blades to become unbalanced
  4. Is caused by the blades while the helicopter is hovering in ground effect.
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92. If the pilot were to make a near-vertical power approach into a confined area with the airspeed near zero, what hazardous condition may develop?
  1. Autorotation
  2. Ground resonance when landing
  3. Bouncing the landing causing the tailrotor to strike the ground
  4. A settling with power condition
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93. Which is appropriate for a helicopter approaching an airport for landing?
  1. Remain below the traffic pattern at about 500 feet AG and from the opposite side of the traffic flow
  2. Flow with fixed wing aircraft
  3. Approach under fixed wing but on the same side as their normal traffic pattern.
  4. Approach the airport from the departure end of the runway so taking off fixed wing aircraft can see and avoid
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94. Refer to Figure 44 on page 46.
Determine if the helicopter weight and balance are within limits. WEIGHT ARM MOMENT (LB) (IN) (100) Empty weight 1,495.0 101.4 1,515.93 Oil, 8 qt --- 100.5 --- Fuel, 40 gal --- 96.0 --- Pilot and copilot 300.0 64.0
  1. 95.2 inches with the CG out of the envelope
  2. 95.5 inches with the CG in the envelope
  3. 95.2 inches with the CG in the envelope
  4. 95.5 inches with the CG out of the envelope
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95. Refer to igure 44 on page 46.
Calculate the weight and balance of the helicopter, and determine if the CG is within limits. WEIGHT ARM MOMENT (LB) (IN) (100) Empty weight 1,495.0 101.4 1,515.93 Oil, 8 qt --- 100.5 --- Fuel, 40 gal --- 96.0 --- Pilot 160.0 64.0 ---
  1. 96.0 within limits
  2. 97.58 within limits
  3. 95.45 out of limits
  4. 90.89 within limits
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