Chapter 4—Slow Flight, Stalls, and Spins |
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Table of Contents Introduction Slow Flight Flight at Less than Cruise Airspeeds Flight at Minimum Controllable Airspeed Stalls Recognition of Stalls Fundamentals of Stall Recovery Use of Ailerons/Rudder in Stall Recovery Stall Characteristics Approaches to Stalls (Imminent Stalls)—Power-On or Power-Off Full Stalls Power-Off Full Stalls Power-On Secondary Stall Accelerated Stalls Cross-Control Stall Elevator Trim Stall Spins Spin Procedures Entry Phase Incipient Phase Developed Phase Recovery Phase Intentional Spins Weight and Balance Requirements |
ELEVATOR TRIM STALL The elevator trim stall maneuver shows what can happen when full power is applied for a go-around and positive control of the airplane is not maintained. [Figure 4-8] Such a situation may occur during a go-around procedure from a normal landing approach Figure 4-8. Elevator trim stall.or a simulated forced landing approach, or immediately after a takeoff. The objective of the demonstration is to show the importance of making smooth power applications, overcoming strong trim forces and maintaining positive control of the airplane to hold safe flight attitudes, and using proper and timely trim techniques. At a safe altitude and after ensuring that the area is clear of other air traffic, the pilot should slowly retard the throttle and extend the landing gear (if retractable gear). One-half to full flaps should be lowered, the throttle closed, and altitude maintained until the airspeed approaches the normal glide speed. When the normal glide is established, the airplane should be trimmed for the glide just as would be done during a landing approach (nose-up trim). During this simulated final approach glide, the throttle is then advanced smoothly to maximum allowable power as would be done in a go-around procedure. The combined forces of thrust, torque, and back-elevator trim will tend to make the nose rise sharply and turn to the left. When the throttle is fully advanced and the pitch attitude increases above the normal climbing attitude and it is apparent that a stall is approaching, adequate forward pressure must be applied to return the airplane to the normal climbing attitude. While holding the airplane in this attitude, the trim should then be adjusted to relieve the heavy control pressures and the normal go-around and level-off procedures completed. The pilot should recognize when a stall is approaching, and take prompt action to prevent a completely stalled condition. It is imperative that a stall not occur during an actual go-around from a landing approach. Common errors in the performance of intentional stalls are:
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