Occurs during approach/landing, especially during base-to-final turns or when flaring too aggressively.
Clearing turns – Ensure area is safe.
Configuration – Landing config: full flaps, gear down (if retractable).
Power Reduction – Reduce to idle as if on final approach.
Establish Approach Speed – Trim for final approach speed (~65 knots typical).
Initiate Stall – Smoothly pitch up to simulate flare, increasing AOA.
Recognize Stall – Indications: buffet, stall horn, nose drop.
Recovery:
Reduce AOA immediately.
Apply full power.
Retract flaps incrementally as needed.
Climb at Vx/Vy.
Why power-off stalls are critical near the ground.
How improper pitch or uncoordinated turns increase risk.
Importance of stabilized approaches.
How to avoid by managing approach speeds and attitudes.
Occurs during takeoff or go-around when excessive pitch is applied, especially with full power.
Clearing turns – Ensure area is safe.
Configuration – Takeoff config: flaps set (per POH), climb pitch.
Apply Full Power – Or at least 65%.
Pitch Up – Smoothly raise nose to takeoff attitude and beyond.
Hold Pitch – Maintain until stall occurs.
Recognize Stall – Indications: buffet, stall horn, nose drop, wing drop.
Recovery:
Reduce AOA immediately.
Maintain full power.
Level wings with rudder (avoid a spin).
Return to climb attitude at Vx/Vy.
Dangers during takeoff/go-around.
Effects of high power + high AOA.
Importance of rudder use during slow flight.
Spin awareness and how poor coordination can lead to a spin.
Occurs during steep turns or abrupt maneuvers where load factor increases (e.g., base-to-final overshoot corrections).
Clearing turns – Ensure area is safe.
Configuration – Clean (no flaps).
Establish Steep Turn – 45° or greater, coordinated.
Abrupt Back Pressure – Increase load factor intentionally.
Induce Stall – Stall occurs at a higher-than-normal airspeed.
Recognize Stall – Buffeting, nose drop, higher-speed stall break.
Recovery:
Release back pressure immediately.
Level wings.
Apply power if needed.
Return to straight-and-level flight.
Stalls can happen at any speed if AOA exceeds critical value.
Load factor increases stall speed (Vₛ increases with bank).
Real-world scenarios: tight turns, turbulence during turns, abrupt maneuvers.
Importance of smooth, coordinated control inputs.
Emphasize critical angle of attack over airspeed.
Teach stall recognition: feel, sound, visual cues.
Stress coordination: use of rudder to prevent spins.
Discuss spin awareness, but spin entry and recovery is a separate required maneuver for CFI.
Encourage calm, immediate recovery techniques.
Occurs when the pilot tries to compensate for overshooting the runway centerline by applying excessive rudder (toward the turn) while holding opposite aileron.
Most dangerous at low altitudes (e.g., during landing pattern).
Clearing Turns – Make sure airspace is safe.
Configuration – Landing config (flaps as needed, gear down if applicable).
Simulate Base-to-Final Turn – Begin a gentle turn.
Introduce Cross-Control Inputs:
Apply inside rudder (skid the turn).
Apply opposite aileron to prevent further banking.
Pitch Up – Simulate trying to "stretch" glide path to runway.
Induce Stall – Stall develops quickly due to uncoordinated inputs.
Recognize Stall – Often accompanied by wing drop and tendency to yaw (spin entry risk).
Recovery:
Neutralize controls (rudder and aileron).
Reduce AOA.
Apply power.
Level wings with coordinated rudder input.
Return to safe flight attitude.
Cross-control stalls are highly asymmetric, leading to spins if not corrected immediately.
Slips (with opposite rudder) are safe if done correctly—but skids (with inside rudder) are dangerous near the ground.
Teach proper approach planning to avoid needing aggressive corrections.
Reinforce coordinated flight, especially in the pattern.
Difference between slip (safe, controlled) vs. skid (dangerous, especially low and slow).
Real-world accident scenarios (stall/spin from base-to-final).
Ball indicator importance: keep it centered.
Spin awareness: A cross-controlled stall can quickly lead to an incipient spin if unchecked.