Demonstrate how trim during a go-around can cause a stall. | | Overcoming trim forces in a G/A is required to prevent a stall. |
- Landing configuration, trim
- G/A power
- Nose-up tendency
- Remedy:
- Anticipate trim forces
- Elevator pressure
- Procedure
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- Pre-maneuver checklist
- Slow to landing speed, full flaps
- ~65 knots, ~800fpm down, trimmed for descent
- Apply takeoff power
- Let nose rise
- Keep coordination with rudder
- Verbalize stall warning
- Stall break
- Push nose-low
- Accelerate
- Retract flaps and recovery
- Recovery at VY
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- Coordination
- Secondary stall
- Spins
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- Over-reliance on airspeed or ball
- Accelerated stall in recovery
- Secondary stall
- Negative load factor in recovery
- Premature recovery
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