Aircraft Performance with Inoperative Engine

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Questions and Answers

What is the effect of a critical engine inoperative on the power required and total drag?

  • Increases power required and total drag (correct)
  • No effect on power required and total drag
  • Increases power required and decreases total drag
  • Decreases power required and total drag

How does a higher gross mass at the same altitude affect the gradient and rate of climb?

  • No effect on gradient and rate of climb
  • Increases gradient and rate of climb
  • Increases gradient and decreases rate of climb
  • Decreases gradient and rate of climb (correct)

What is VX in relation to climb performance?

  • Speed for best specific range
  • Speed for best angle of flight path (correct)
  • Speed for best angle of climb
  • Speed for best rate of climb

Why does the take-off distance required increase?

<p>Due to slush on the runway (A)</p> Signup and view all the answers

What is the effect of a 75% power setting compared to a 65% power setting?

<p>Increases speed, fuel consumption, and fuel-burn/distance (B)</p> Signup and view all the answers

What happens to the power required when an engine is inoperative?

<p>Increases due to additional drag (B)</p> Signup and view all the answers

What is the effect of a higher gross mass on VY and VX?

<p>VY and VX are decreased (A)</p> Signup and view all the answers

What is the effect of headwind on take-off distance required?

<p>Increases take-off distance required (D)</p> Signup and view all the answers

What can limit the speed of a VMCL?

<p>Available maximum roll rate (C)</p> Signup and view all the answers

What is the correct combination of statements that defines VMCA?

<p>1, 2, 3, 4, and 5 (A)</p> Signup and view all the answers

Why is an MEP with inward counter-rotating propellers easier to control after an engine failure?

<p>The thrust line is closer to the longitudinal axis (A)</p> Signup and view all the answers

What happens when an MEP with clockwise rotating propellers encounters a failure of the critical engine?

<p>It becomes harder to control (C)</p> Signup and view all the answers

What is the effect of an engine failure on an MEP with inward counter-rotating propellers?

<p>It becomes easier to control (D)</p> Signup and view all the answers

What is the condition for VMCA to occur?

<p>Maximum take-off thrust is set and maintained on the remaining engines (B)</p> Signup and view all the answers

What happens when a pilot suffers an engine failure and forgets to feather the propeller?

<p>Glide angle is increased (B)</p> Signup and view all the answers

What is the net flight path gradient after take-off compared to the actual climb gradient if the aeroplane is more than 50 ft above runway elevation?

<p>Smaller (B)</p> Signup and view all the answers

What is the purpose of feathering a propeller in flight?

<p>To reduce drag and minimize yaw (A)</p> Signup and view all the answers

What happens to the yawing effect when one of the engine's propellers are feathered on an MEP aircraft?

<p>The yawing effect reduces (A)</p> Signup and view all the answers

What is the minimum VR speed for a Class B twin engine aeroplane according to CS23?

<p>90 kts (C)</p> Signup and view all the answers

When are the blades of a propeller in the feathered position?

<p>When the drag of the propeller is minimal (D)</p> Signup and view all the answers

Which engine is critical in a twin engine turbo prop with two clockwise props?

<p>The right engine (D)</p> Signup and view all the answers

What is the effect of not feathering a propeller during an engine failure?

<p>Drag and yaw are increased (B)</p> Signup and view all the answers

Which of the following statements about asymmetric effects of the propeller slipstream are correct during an engine failure of a twin-engine turboprop airplane?

<p>1, 2 (B)</p> Signup and view all the answers

What are the effects of feathering a propeller in flight?

<p>Drag and yaw decrease, climb gradient increases (A)</p> Signup and view all the answers

Which condition will result in the least asymmetric yaw and roll in case of an engine failure in a twin-engine propeller airplane?

<p>The engines are mounted on the wings (D)</p> Signup and view all the answers

What will happen to the rolling moment if the right engine fails in a twin engine turbo prop with two clockwise props?

<p>A rolling moment towards the left engine will be induced (B)</p> Signup and view all the answers

What determines the stall speeds of an aircraft?

<p>The CG at the forward limit (B)</p> Signup and view all the answers

What determines the minimum control speeds of an aircraft?

<p>The CG at the aft limit (C)</p> Signup and view all the answers

What will happen to the slipstream-induced lift if the left engine fails in a twin-engine turboprop airplane?

<p>Slipstream-induced lift will be lost on the side where the engine has failed (D)</p> Signup and view all the answers

What is the main factor that affects the net flight path gradient after take-off?

<p>Runway elevation (A)</p> Signup and view all the answers

What is the minimum control speed in the landing configuration?

<p>VMCL (C)</p> Signup and view all the answers

What is the primary factor that limits VMCL?

<p>Maximum rudder deflection (C)</p> Signup and view all the answers

What is the primary purpose of determining VMCG?

<p>To determine the minimum control speed during takeoff (A)</p> Signup and view all the answers

What is the effect of crosswind on VMCG?

<p>It increases VMCG (A)</p> Signup and view all the answers

What is the primary factor that affects VMCA?

<p>Airport density altitude (D)</p> Signup and view all the answers

What is the condition for establishing minimum control speeds during flight tests?

<p>CG position at the most unfavorable location and without nose wheel steering (B)</p> Signup and view all the answers

What must the thrust be in a straight steady climb?

<p>Greater than the drag (D)</p> Signup and view all the answers

What is the primary purpose of determining minimum control speeds?

<p>To ensure safe takeoff and landing operations (C)</p> Signup and view all the answers

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Study Notes

Critical Engine Inoperative

  • Inoperative engine increases power required and total drag due to windmilling engine and yaw moment compensation.
  • Higher gross mass at same altitude decreases gradient and rate of climb.

Performance

  • VX: speed for best angle of flight path.
  • VY: speed for best rate of climb.

Take-Off Distance

  • Increases due to higher gross mass, downhill slope, slush on runway, and headwind.

Cruise Power Settings

  • 75% power setting increases speed, fuel consumption, and fuel-burn/distance compared to 65% power setting.

Net Flight Path Gradient

  • Net flight path gradient after take-off is smaller than actual climb gradient.

VR Speed for Class B Twin Engine Aeroplane

  • Minimum VR speed is 90 kts according to CS23.

Critical Engine

  • Critical engine for twin-engine turbo prop with two clockwise props is the right engine.

Asymmetric Effects of Propeller Slipstream

  • Rolling moment towards the running engine is induced.
  • Slipstream-induced lift is lost on the side where the engine has failed.

Engine Failure

  • Yawing effect reduces when one engine's propeller is feathered on an MEP aircraft.

Stall Speeds and Minimum Control Speeds

  • Stall speeds are determined with CG at forward limit.
  • Minimum control speeds are determined with CG at aft limit.

Minimum Control Speeds

  • VMCL is the minimum control speed in the landing configuration.
  • VMCA is the minimum speed at which directional control can be maintained after engine failure.

Straight Steady Climb

  • Thrust must be greater than drag in a straight steady climb.

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