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Aero 2 > Performance and Maneuvering 2.4 > Flashcards

Performance and Maneuvering 2.4 Flashcards

1
Q

Define Takeoff and Landing Airspeed in terms of Stall Speed.

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2
Q

State the various forces acting on an airplane during the Takeoff and Landing Transitions.

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3
Q

State the factors that determine the coefficient of Rolling Friction.

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4
Q

Describe the effects on Takeoff and Landing Performance, given variations in WT, Alt., Temp., Humidity, Wind,and Braking.

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5
Q

Describe the effects of Outside Air Temperature (OAT) on airplane Performance Characteristics.

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6
Q

Define Maximum Angle of Climb and Maximum rate of Climb Profiles.

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7
Q

Explain the Performance Characteristics Profiles that Yield Maximum Angle of Climb and Maximum Rate of Climb for Turboprops.

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8
Q

Describe the effect of changes in WT, Alt., Config.,, and Wind on Maximum Angle of Climb and Maximum Rate of Climb Profiles.

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9
Q

Describe the Performance Characteristics and Purpose of the Best Climb Profiles for the T-6B.

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10
Q

Define Absolute Ceiling, Service Ceiling, Cruise Ceiling, Combat Ceiling, and Maximum Operating Ceiling.

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11
Q

State the Maximum Operating Ceiling of the T-6B.

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12
Q

State the Relationship Between Fuel Flow, Power Available, Power Required, and Velocity for a Turboprop Airplane in Straight and Level Flight.

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13
Q

Define Maximum Range and Maximum Endurance Profiles.

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14
Q

Explain the Performance Characteristics Profiles that yield Maximum Endurance and Maximum Range for TurboProps.

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15
Q

Describe the Effect of Changes in WT, Alt., Config., Wind on Maximum Endurance and Maximum Range Performance and Airspeed.

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16
Q

Define Mach Number.

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17
Q

Define Critical Mach.

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18
Q

State the Effects of Altitude on Mach Number and Critical Mach Number.

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19
Q

Define Maximum Glide Range and Maximum Glide Endurance Profiles.

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20
Q

Explain the Performance characteristics profiles that yield Maximum Glide Range and Maximum Glide Endurance.

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21
Q

Describe the effect of changes in WT, Alt., Config., Wind and Propeller Feathering on Maximum Glide Range and Maximum Glide Endurance Performance and Airspeed.

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22
Q

Describe the Locations of the Regions of Normal and Reverse Command on the TuboProp Power Curve.

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23
Q

Explain the relationship between Power Required ad Airspeed in the Regions of Normal and Reverse Command.

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24
Q

Define NoseWheel LiftOff/TouchDown Speed.

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25
Q

State the Pilot Speed and Attitude Inputs necessary to control the Airplane during a Crosswind landing.

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26
Q

Stat the crosswind Limits fo the T-6B.

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27
Q

Define Hydroplaning.

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28
Q

State the Factors that affect the Speed at which an airplane will hydroplane.

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29
Q

Describe the effects of Propeller Slipstream swirl, P-Factor, Torque, and Gyroscopic Precession as they to the T-6B.

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30
Q

Describe what the pilot must do to compensate for propeller slipstream swirl, P-Factor, Torque, and Gyroscopic Precession as they apply to the T-6B.

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31
Q

Describe the effect of Lift on Turn Performance.

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32
Q

Describe the Effect of Weight on Turn Performance.

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33
Q

Describe the Effect of Thrust on Turn Performance.

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34
Q

Describe the effect of Drag on Turn Performance.

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35
Q

Define Turn Radius and Turn Rate.

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36
Q

Describe the effects of Changes in Bank Angle on Turn Performance.

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37
Q

Describe the effects of changes in Airspeed on Turn Performance.

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38
Q

Describe the effects of Aileron and Rudder Forces during Turns.

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39
Q

Explain the Aerodynamic Principle that requires 2 G’s of back stick pressure to maintain level, constant airspeed flight, at 60 degrees Angle of Bank.

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40
Q

Describe the relationship between Load Factor and Angle of Bank for Level, Constant Airspeed flight.

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41
Q

Define Load, Load Factor Limit Load Factor, and Ultimate load Factor.

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42
Q

Define Static Strength, Static Failure, Fatigue Strength, Fatigue Failure, Service Life, Creep, Overstress/Over-G.

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43
Q

Define Maneuvering Speed, Cornering Velocity, Redline Airspeed, Accelerated Stall Lines, and the Safe Flight Envelope.

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44
Q

Describe the boundaries of the Safe Flight Envelope, including Accelerated Stall Lines, Limit Load Factor, Maneuvering Point, and Redline Airspeed.

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45
Q

Define Asymmetric Loading and State he Associated Limitations for the T-6B.

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46
Q

Define Static Stability and Dynamic Stability.

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47
Q

Describe the Characteristics exhibited by aircraft with Positive, Neutral, and Negative Dynamic Stabilities, when disturbed from Equilibrium.

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48
Q

Describe the Characteristics of Damped, Undamped, and Divergent Oscillations, and the Combination of Static and Dynamic Stabilities that result in Each.

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49
Q

Explain the Relationship between Stability and Maneuverability.

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50
Q

State the Methods for Increasing an airplane’s Maneuverability.

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51
Q

State the effects of airplane components on an airplane’s Longitudinal Static Stability.

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52
Q

Explain the Criticality of WT and Balance.

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53
Q

State the effects of Airplane Components on an airplane’s Directional Static Stability.

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54
Q

State the effects of airplane components on an airplane’s Lateral Static Stability.

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55
Q

State the Static Stability requirements for, and the effects of, Directional Divergence

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56
Q

State the static stability requirements for and the effects of Spiral Divergence.

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57
Q

State the static stability requirements for and the effects of Dutch Roll.

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58
Q

Define Proverse Roll.

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59
Q

Define Adverse Yaw.

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60
Q

Explain how an airplane develops Phugoid Oscillations.

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61
Q

Explain how an airplane develops Pilot Induced Oscillations.

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62
Q

Define Asymmetric Thrust.

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Aero 2 (3 decks)

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