AI.XIII.B.K3

From the FAA library

• Airplane Flying Handbookp. 13-26
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › VMC Demo Stall Avoidance

  airplane to the entry airspeed. Note that noise within the flight deck may mask the sound of the stall warning horn. While the VMC demonstration shows the earliest onset of a loss of directional control when performed in accordance with ... foregoing procedures, avoid a stalled condition. Avoid stalls with asymmetrical thrust, such that the VMC demonstration does not degrade into a single-engine stall. A VMC demonstration that is allowed to degrade into a single-engine stall with high asymmetrical…

• Airplane Flying Handbookp. 13-23
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › Derivation of VMC

  recognize and recover from loss of directional control associated with the red radial indicated airspeed by performing a VMC demonstration. Since the object of a VMC demonstration is not performance, sideslip occurs during the maneuver. Detailed discussion on both ... loss of directional control and maximum OEI climb performance follows. Derivation of VMC VMC is a speed established by the manufacturer, published in the AFM/POH, and marked on most airspeed indicators with a red radial line. A knowledgeable and competent…

• Airplane Flying Handbookp. 13-25
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › ⦁ All propeller controls in the recommended takeoff position throughout VMC determination

  determination of VMC in certification is solely concerned with the minimum speed for directional control under a very specific set of circumstances, and not the optimum airplane attitude or configuration for climb performance. During dynamic VMC determination in aircraft certification ... cuts of the critical engine using the mixture control are performed by flight test pilots while gradually reducing the speed with each attempt. VMC is the minimum speed at which directional control could be maintained within 20° of the original…

• Airplane Flying Handbookp. 1-13
  Chapter 1: Introduction to Flight Training › Safety Considerations › Stall Awareness

  understand that there are several flight maneuvers that may produce an increase in the wing’s AOA, but the stall does not occur until the AOA becomes excessive. This critical AOA varies from 16°–20° depending on the airplane design ... Figure 1-15] Figure 1-14. All student pilots receive and log flight training in stalls and stall recoveries prior to their first solo flight. Figure 1-15. Stalls occur when the airfoil's angle of attack reaches the critical…

• Stall and Spin Awareness Trainingp. 9
  CHAPTER 2. FLIGHT TRAINING: STALLS › 200. STALL TRAINING

  CHAPTER 2. FLIGHT TRAINING: STALLS 200. STALL TRAINING. Flight instructor-airplane and flight instructor-glider applicants must be able to give stall training. The flight instructor should emphasize that techniques and procedures for each aircraft may differ and that pilots ... each aircraft flown. The most effective training method contained in Report No. FAA-RD-77-26, General Aviation Pilot Stall Awareness Study, is the simulation of scenarios that can lead to inadvertent stalls by creating distractions while the student…

• Stall and Spin Awareness Trainingp. 9
  CHAPTER 2. FLIGHT TRAINING: STALLS › 200. STALL TRAINING › a. Stall Avoidance Practice at Slow Airspeeds

  This loss of power will result in a VMC lower than the stall speed at higher altitudes. (VMC is the minimum control speed with the critical engine inoperative). Also, some airplanes have such an effective rudder that even ... level VMC is lower than stall speed. For these airplanes, demonstrating loss of directional control may be safely conducted by limiting rudder travel to simulate maximum rudder available. Limiting rudder travel should be accomplished well above the power-off stall…