Skills - rate how you're doing
▸Maneuvering during slow flight
How this maneuver goes - Airplane Flying Handbook- Clear the area, gradually reduce power, raise pitch to hold altitude as airspeed bleeds off.
- Near the target (~5–10 kt above stall warning), add power to hold altitude and trim.
- Configure as required (gear/flaps), anticipating the pitch/AOA change with each change.
- Hold coordinated flight with steady right rudder; use larger, smoother inputs as the controls go mushy.
- Practice shallow turns, climbs, descents — add power in turns and counter yaw with rudder.
- React immediately to any stall warning by relaxing back pressure to lower the AOA.
- To exit: add power, ease forward to hold altitude as lift builds, clean up, re-trim.
▸Power-off stalls
How this maneuver goes - Airplane Flying Handbook- Clear the area; set landing configuration; hold altitude until speed slows to approach speed.
- Pitch to a normal approach descent attitude at idle power.
- Smoothly raise the nose to induce the stall, wings level and coordinated.
- Hold pitch until the full stall (uncommanded nose-down that can't be arrested).
- At the stall, reduce AOA with nose-down elevator until the stall warning stops.
- Level the wings with aileron, coordinate with rudder (right rudder as power comes in).
- Smoothly add power, return to the flightpath (or positive-rate go-around), retract flaps/gear, avoid a secondary stall.
▸Power-on stalls
How this maneuver goes - Airplane Flying Handbook- Clear the area; set takeoff/climb configuration; slow to normal lift-off speed.
- At lift-off speed, apply takeoff/climb power while rotating into the climb attitude.
- Raise the nose to increase AOA (elevator progressively aft), adding right rudder to stay coordinated.
- Hold until the full stall — recognize by sight, sound, feel.
- At the stall, immediately reduce AOA with nose-down elevator until the warning stops.
- Level the wings with aileron, coordinate with rudder (right rudder for yaw).
- Return to the desired flightpath with adequate airspeed and control, avoiding a secondary stall.
▸Accelerated stalls
How this maneuver goes - in the handbook's own wordsThere are two methods for performing an accelerated stall. The most common accelerated stall procedure starts from straight-and- level flight at an airspeed at or below VA or VO. The pilot rolls the airplane into a coordinated, level-flight 45° turn and then smoothly, firmly, and progressively increase the AOA through back elevator pressure until a stall occurs. Alternatively, the pilot rolls the airplane into a coordinated, level-flight 45° turn at an airspeed above VA or VO. After the airspeed slows to VA or VO, and at an airspeed 5 to 10 percent faster than the unaccelerated stall speed, the pilot progressively increases the AOA through back elevator pressure until a stall occurs. The increased back elevator pressure increases lift and the G load. The G load pushes the pilot's body down in the seat. The increased lift also increases drag, which may cause the airspeed to decrease. The pilot should know the published stall speed for 45° of bank, flaps up, before performing the maneuver. This speed is typically published in the AFM.
An airplane typically stalls during a level, coordinated turn similar to the way it does in wings-level flight, except that the stall buffet can be sharper. If the turn is coordinated at the time of the stall, the airplane's nose pitches away from the pilot just as it does in a wings-level stall since both wings will tend to stall nearly simultaneously. If the airplane is not properly coordinated at the time of stall, the stall behavior may include a change in bank angle until the AOA has been reduced. It is important to take recovery action at the first indication of a stall (if impending stall training/checking) or immediately after the stall has fully developed (if full stall training/checking) by applying forward elevator pressure as required to reduce the AOA and to eliminate the stall warning, level the wings using ailerons, coordinate with rudder, and adjust power as necessary. Stalls that result from abrupt maneuvers tend to be more aggressive than unaccelerated +1G stalls. Because they occur at higher-than-normal airspeeds or may occur at lower-than-anticipated pitch attitudes, they can surprise an inexperienced pilot. Since an accelerated stall may put the airplane in an unexpected attitude. Failure to execute an immediate recovery may result in a spin or other departure from controlled flight.
Airplane Flying Handbook, Chapter 5 — Accelerated Stalls
▸Spin awareness
How this maneuver goes - Airplane Flying Handbook- Recognize the setup: stalled wing + yaw (uncoordinated stall), most common in an overshooting base-to-final turn.
- At the first sign of an approaching stall, prevent yaw and hold coordinated flight — averting yaw prevents the spin.
- If a spin begins, recognize it by low constant airspeed and rotation; read direction from the turn coordinator, not the ball.
- Recover at the incipient phase (before 360°): reduce power to idle.
- Neutralize the ailerons.
- Apply and hold full rudder opposite the rotation, briskly, until rotation stops.
- Briskly apply forward elevator to break the stall (don't wait for rotation to stop).
- When rotation stops, neutralize rudder, then smoothly raise the nose to level flight. `[verify — always follow the manufacturer's spin recovery procedure]`
Words for this area
- flightpath
- pilot complacency
- maneuvering
- phase of flight
- uncoordinated flight
- equipment malfunctions
- pitch
- bank angle
- airspeeds inappropriate for the conditions
- instrument rating
- startle effect
- microbursts
- overspeeds
- Environmental factors
- instrument flight
- airfoil
- Mechanical factors
- asymmetrical flaps
- autothrottles
- AFM/POH
- VMC — Visual Meteorological Conditions
- vertigo
- spatial disorientation
- task saturation
- pitot heat
- annunciations
- autoflight system
- stall warning
- aerodynamic buffet
- roll
- startle response
- scenario-based training
- marginal VMC
- natural horizon
- aerobatic training
- diversion of attention
- airmanship
- Sensory Overload/Deprivation
- wing leveler
- aviation training devices
- normal category
- aerobatic category
- startle
- coordinated flight
- recovery
- counterintuitive control movements
- relative wind
- ADM — aeronautical decision making
- trailing edge
- stalling speed
- overstressing the airplane
- L/DMAX
- instrument malfunction
- backside of the power curve
- unload the airplane
- aerobatic-capable airplane
- unplanned excursions
- airplane-based UPRT
- landing configuration
- torque
- slipstream effect
- FSTD-based UPRT
- P-factor
- left yaw
- right rudder
- straight-and-level
- yaw
- impending stall
- buffeting
- stick shaker
- angle of attack
- stick pusher
- kinesthesia
- CG — center of gravity
- multiengine airplanes
- GA — general aviation
- yaw effects
- aircraft buffet
- aileron inputs
- control surfaces
- washout
- power-off stall
- power-on stall
- stall recovery
- single-engine airplane
- speedbrakes
- secondary stall
- glider
- reduced airspeeds
- practical test
- takeoff/departure
- approach/landing phases of flight
- controlled flight
- positive rate of climb
- slip
- lift-off speed
- accelerated stall
- aural warning
- VA — design maneuvering speed
- propeller-driven airplanes
- uncommanded rolling motion
- VO — operating maneuvering speed
- stall recognition
- aural alert
- cross-control stall
- skidding cross-control stall
- overshoot
- AOA indicator
- Autorotation
- sideslip
- spiraling slipstream
- gyroscopic precession
- stall characteristics
- seat of the pants sensations
- Preflight inspection
- slip-skid indicator centered
- spiral dive
- spin recovery
- syllabi
- intentional spins
- upset prevention and recovery
- utility category
- climbing turn
- unload the wing
- speedbrakes/spoilers
- VY
- wing flaps
- climb attitude
- commercial pilot
- Aerodynamics of Flight
- AFM
- G load
- tailwind component
- inside or bottom rudder pressure
- inside rudder pressure
- medium-banked turn
- bottom rudder pressure
- skidding turn
- glide speed
- elevator trim stall
- propwash
- elevator trim
- downward corkscrew path
- corkscrew path
- vertical axis
- POH — Pilot's Operating Handbook
- aileron deflection
- directional control
- spin procedures
- airworthiness standards
- anti-spin control deflections
- incipient phase
- developed phase
- recovery phase
- full rudder
- inadvertent IMC encounter
- incipient spin
- recurrent practice/training
- turbojet-powered airplanes
- unrecoverable spin
- opposite rudder
- CFRs — Code of Federal Regulations
- G-load
- kinesthetic sensations
- airframe structural damage
- rolling pullout
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