PA.IX.E.S2

From the FAA library

• Airplane Flying Handbookp. 13-31
  Chapter 13: Transition to Multiengine Airplanes › Low Altitude Engine Failure Scenarios › Control

  Single-Engine Climb Performance Adequate If the single-engine rate of climb is adequate, the procedures for continued flight should be followed. [Figure 13-20] There are four areas of concern: control, configuration, climb, and checklist. Figure ... Landing gear up—adequate climb performance. Control The first consideration following engine failure during takeoff is to maintain control of the airplane. Maintaining directional control with prompt and often aggressive rudder application and STOPPING…

• Airplane Flying Handbookp. 3-2
  Chapter 3: Basic Flight Maneuvers › Effect and Use of Flight Controls

  airplane. Think of this movement from the pilot’s head to the pilot’s feet. ⦁ When right pressure is applied to the aileron control, which rotates the control wheel or yoke clockwise, or deflects the control stick ... Think of this movement from the pilot’s head to the pilot’s right hip. ⦁ When left pressure is applied to the aileron control, which rotates the control wheel or yoke counterclockwise, or deflects the control stick…

• Airplane Flying Handbookp. 3-10
  Chapter 3: Basic Flight Maneuvers › Trim Control

  then hold the wings level with aileron flight control pressure while rudder control pressure is trimmed out. Finally, aileron trim should be adjusted to relieve any aileron flight control pressure. A properly trimmed airplane is an indication ... good piloting skills. Any control forces that the pilot feels should be a result of deliberate flight control pressure inputs during a planned change in airplane attitude, not a result of forces being applied by the airplane…

• 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…

• Airplane Flying Handbookp. 3-8
  Chapter 3: Basic Flight Maneuvers › Straight-and-Level Flight › Straight Flight

  that reason, the pilot should not form the habit of unnecessarily moving the flight controls. The pilot needs to learn to recognize when corrections are necessary and then to make a measured flight control response precisely, smoothly ... continually, generally to the left due to the pilot’s left seat position and consequently focus attention in that direction. This not only gives a restricted angle from which the pilot is to observe but also causes the pilot…

• 14 CFR Part 91 — General Operating and Flight RulesOpen
  14 CFR § 91.109 Flight instruction; Simulated instrument flight and certain flight tests.

  Flight instruction; Simulated instrument flight and certain flight tests. (c) No person may operate a civil aircraft in simulated instrument flight unless— (1) The other control seat is occupied by a safety pilot who possesses at least ... purposes of providing training for a solo cross-country endorsement under § 61.93 of this chapter, a flight instructor certificate with an appropriate sport pilot rating and meets the requirements of § 61.412 of this chapter. (2) The safety pilot has adequate…