Performance and Maneuvering 2.4 Flashcards
Define Takeoff and Landing Airspeed in terms of Stall Speed.
L
State the various forces acting on an airplane during the Takeoff and Landing Transitions.
L
State the factors that determine the coefficient of Rolling Friction.
L
Describe the effects on Takeoff and Landing Performance, given variations in WT, Alt., Temp., Humidity, Wind,and Braking.
L
Describe the effects of Outside Air Temperature (OAT) on airplane Performance Characteristics.
L
Define Maximum Angle of Climb and Maximum rate of Climb Profiles.
L
Explain the Performance Characteristics Profiles that Yield Maximum Angle of Climb and Maximum Rate of Climb for Turboprops.
L
Describe the effect of changes in WT, Alt., Config.,, and Wind on Maximum Angle of Climb and Maximum Rate of Climb Profiles.
L
Describe the Performance Characteristics and Purpose of the Best Climb Profiles for the T-6B.
L
Define Absolute Ceiling, Service Ceiling, Cruise Ceiling, Combat Ceiling, and Maximum Operating Ceiling.
L
State the Maximum Operating Ceiling of the T-6B.
L
State the Relationship Between Fuel Flow, Power Available, Power Required, and Velocity for a Turboprop Airplane in Straight and Level Flight.
L
Define Maximum Range and Maximum Endurance Profiles.
L
Explain the Performance Characteristics Profiles that yield Maximum Endurance and Maximum Range for TurboProps.
L
Describe the Effect of Changes in WT, Alt., Config., Wind on Maximum Endurance and Maximum Range Performance and Airspeed.
L
Define Mach Number.
L
Define Critical Mach.
L
State the Effects of Altitude on Mach Number and Critical Mach Number.
L
Define Maximum Glide Range and Maximum Glide Endurance Profiles.
L
Explain the Performance characteristics profiles that yield Maximum Glide Range and Maximum Glide Endurance.
L
Describe the effect of changes in WT, Alt., Config., Wind and Propeller Feathering on Maximum Glide Range and Maximum Glide Endurance Performance and Airspeed.
L
Describe the Locations of the Regions of Normal and Reverse Command on the TuboProp Power Curve.
L
Explain the relationship between Power Required ad Airspeed in the Regions of Normal and Reverse Command.
L
Define NoseWheel LiftOff/TouchDown Speed.
L
State the Pilot Speed and Attitude Inputs necessary to control the Airplane during a Crosswind landing.
L
Stat the crosswind Limits fo the T-6B.
L
Define Hydroplaning.
L
State the Factors that affect the Speed at which an airplane will hydroplane.
L
Describe the effects of Propeller Slipstream swirl, P-Factor, Torque, and Gyroscopic Precession as they to the T-6B.
L
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.
L
Describe the effect of Lift on Turn Performance.
L
Describe the Effect of Weight on Turn Performance.
L
Describe the Effect of Thrust on Turn Performance.
L
Describe the effect of Drag on Turn Performance.
L
Define Turn Radius and Turn Rate.
L
Describe the effects of Changes in Bank Angle on Turn Performance.
L
Describe the effects of changes in Airspeed on Turn Performance.
L
Describe the effects of Aileron and Rudder Forces during Turns.
L
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.
L
Describe the relationship between Load Factor and Angle of Bank for Level, Constant Airspeed flight.
L
Define Load, Load Factor Limit Load Factor, and Ultimate load Factor.
L
Define Static Strength, Static Failure, Fatigue Strength, Fatigue Failure, Service Life, Creep, Overstress/Over-G.
L
Define Maneuvering Speed, Cornering Velocity, Redline Airspeed, Accelerated Stall Lines, and the Safe Flight Envelope.
L
Describe the boundaries of the Safe Flight Envelope, including Accelerated Stall Lines, Limit Load Factor, Maneuvering Point, and Redline Airspeed.
L
Define Asymmetric Loading and State he Associated Limitations for the T-6B.
L
Define Static Stability and Dynamic Stability.
L
Describe the Characteristics exhibited by aircraft with Positive, Neutral, and Negative Dynamic Stabilities, when disturbed from Equilibrium.
L
Describe the Characteristics of Damped, Undamped, and Divergent Oscillations, and the Combination of Static and Dynamic Stabilities that result in Each.
L
Explain the Relationship between Stability and Maneuverability.
L
State the Methods for Increasing an airplane’s Maneuverability.
L
State the effects of airplane components on an airplane’s Longitudinal Static Stability.
L
Explain the Criticality of WT and Balance.
L
State the effects of Airplane Components on an airplane’s Directional Static Stability.
L
State the effects of airplane components on an airplane’s Lateral Static Stability.
L
State the Static Stability requirements for, and the effects of, Directional Divergence
L
State the static stability requirements for and the effects of Spiral Divergence.
L
State the static stability requirements for and the effects of Dutch Roll.
L
Define Proverse Roll.
L
Define Adverse Yaw.
L
Explain how an airplane develops Phugoid Oscillations.
L
Explain how an airplane develops Pilot Induced Oscillations.
L
Define Asymmetric Thrust.
L
