Slow flight is when the airplane is flown at an angle of attack (AOA) just below the angle that causes an aerodynamic buffet or the activation of a stall warning device. A small increase in AOA may result in an impending stall, which increases the risk of an actual stall.
For pilot training and testing purposes, slow flight includes two main elements:
Left-Turning Tendencies: In propeller-driven airplanes, torque, slipstream effect, and P-factor produce strong left yaw, which requires right rudder input to maintain coordinated flight.
Reduced Control Effectiveness: The airplane is less responsive to flight control inputs at slower airspeeds. Pilots sometimes refer to it as "sloppy" or "mushy" controls.
Reduced Forward Visibility: The horizon may not be visible in front of the airplane in high-pitch attitudes. The "Lindbergh" visual reference can help maintain coordinated flight.
Power:
Region of Reversed Command:
Feel: Control pressures change as airspeed is reduced. Just before the stall occurs, buffeting, uncommanded rolling, or vibrations may begin to occur.
Vision: When a stall results from an unusual attitude, vision is useful for checking the pitch attitude. However, an airplane can also be stalled in a normal attitude, in which case vision cannot aid in detecting the stall.
Hearing: As airspeed decreases, a change in sound is made by the air flowing along the airplane structure. A loss of engine RPM is noticeable in an airplane with a fixed-pitch propeller.
Kinesthesia: Changes in direction or speed can be sensed by experienced pilots to warn of an impending stall.
Maneuvering the airplane in slow flight is practiced at an airspeed just above the speed that would result in a stall warning (e.g., aircraft buffet or stall horn). If a stall warning occurs, the expectation is the pilot will take the appropriate action to correct it.
One procedure to establish this airspeed is to:
Previously, pilots were trained to maneuver during slow flight at the minimum controllable airspeed, the airspeed at which any further increase in AOA, an increase in load factor, or reduction in power would result in an immediate stall. The FAA has since found that it is not appropriate for a pilot to fly with the stall warning present.
At All Times:
Turns:
Climbs and Descents:
Target Speed:
Configuration: As specified by the evaluator.
Airspeed | Altitude | Bank | Heading |
---|---|---|---|
+10/-0 KIAS (SPT, PVT) +5/-0 KIAS (COM) No stall warning | ±100' (SPT, PVT) ±50' (COM) ≥ 1,500′ AGL (ASEL) ≥ 3,000' AGL (AMEL) | ±10° (SPT, PVT) ±5° (COM) | ±10° |