Flight Instructor for Powered-Lift Category › X. Performance Maneuvers › Task B. Inflight Conversion During Straight-and-Level Flight

IL.X.B.K2

Knowledge

Aerodynamic effects of changing aircraft configuration.

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Study note

Get a short, cited explanation of this element written from the FAA handbooks: the core idea, the numbers that matter, common test traps, and a quick self-check.

From the FAA library

Pilot's Handbook of Aeronautical Knowledge p. 5-47
Chapter 5: Aerodynamics of Flight › Boundary Layer Separation › Shock Waves
A considerable increase in thrust (power) is required to increase flight speed…
Pilot's Handbook of Aeronautical Knowledge p. 5-18
Chapter 5: Aerodynamics of Flight › Aircraft Design Characteristics › Lateral Stability (Rolling)
There are four main design factors that make an aircraft laterally stable…
Pilot's Handbook of Aeronautical Knowledge p. 5-5
Chapter 5: Aerodynamics of Flight › Lift/Drag Ratio
At high AOA, small changes in the AOA cause significant changes in…
Pilot's Handbook of Aeronautical Knowledge p. 5-48
Chapter 5: Aerodynamics of Flight › Boundary Layer Separation › Sweepback
In addition to the delay of the onset of compressibility effects, sweepback…
Airplane Flying Handbook p. 5-11
Chapter 5: Maintaining Aircraft Control: Upset Prevention and Recovery Training › Slow Flight › Maneuvering in Slow Flight
Practicing this maneuver in other configurations, such as a clean or takeoff…