Performance and Maneuvering 2.4

Question 1

Define Takeoff and Landing Airspeed in terms of Stall Speed.

Answer 1

L

Question 2

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

Answer 2

L

Question 3

State the factors that determine the coefficient of Rolling Friction.

Answer 3

L

Question 4

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

Answer 4

L

Question 5

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

Answer 5

L

Question 6

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

Answer 6

L

Question 7

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

Answer 7

L

Question 8

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

Answer 8

L

Question 9

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

Answer 9

L

Question 10

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

Answer 10

L

Question 11

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

Answer 11

L

Question 12

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

Answer 12

L

Question 13

Define Maximum Range and Maximum Endurance Profiles.

Answer 13

L

Question 14

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

Answer 14

L

Question 15

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

Answer 15

L

Question 16

Define Mach Number.

Answer 16

L

Question 17

Define Critical Mach.

Answer 17

L

Question 18

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

Answer 18

L

Question 19

Define Maximum Glide Range and Maximum Glide Endurance Profiles.

Answer 19

L

Question 20

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

Answer 20

L

Question 21

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

Answer 21

L

Question 22

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

Answer 22

L

Question 23

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

Answer 23

L

Question 24

Define NoseWheel LiftOff/TouchDown Speed.

Answer 24

L

Question 25

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

Answer 25

L

Question 26

Stat the crosswind Limits fo the T-6B.

Answer 26

L

Question 27

Define Hydroplaning.

Answer 27

L

Question 28

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

Answer 28

L

Question 29

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

Answer 29

L

Question 30

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.

Answer 30

L

Question 31

Describe the effect of Lift on Turn Performance.

Answer 31

L

Question 32

Describe the Effect of Weight on Turn Performance.

Answer 32

L

Question 33

Describe the Effect of Thrust on Turn Performance.

Answer 33

L

Question 34

Describe the effect of Drag on Turn Performance.

Answer 34

L

Question 35

Define Turn Radius and Turn Rate.

Answer 35

L

Question 36

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

Answer 36

L

Question 37

Describe the effects of changes in Airspeed on Turn Performance.

Answer 37

L

Question 38

Describe the effects of Aileron and Rudder Forces during Turns.

Answer 38

L

Question 39

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.

Answer 39

L

Question 40

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

Answer 40

L

Question 41

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

Answer 41

L

Question 42

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

Answer 42

L

Question 43

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

Answer 43

L

Question 44

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

Answer 44

L

Question 45

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

Answer 45

L

Question 46

Define Static Stability and Dynamic Stability.

Answer 46

L

Question 47

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

Answer 47

L

Question 48

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

Answer 48

L

Question 49

Explain the Relationship between Stability and Maneuverability.

Answer 49

L

Question 50

State the Methods for Increasing an airplane’s Maneuverability.

Answer 50

L

Question 51

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

Answer 51

L

Question 52

Explain the Criticality of WT and Balance.

Answer 52

L

Question 53

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

Answer 53

L

Question 54

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

Answer 54

L

Question 55

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

Answer 55

L

Question 56

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

Answer 56

L

Question 57

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

Answer 57

L

Question 58

Define Proverse Roll.

Answer 58

L

Question 59

Define Adverse Yaw.

Answer 59

L

Question 60

Explain how an airplane develops Phugoid Oscillations.

Answer 60

L

Question 61

Explain how an airplane develops Pilot Induced Oscillations.

Answer 61

L

Question 62

Define Asymmetric Thrust.

Answer 62

L