PA.IX.F.S7

From the FAA library

• Airplane Flying Handbookp. 13-30
  Chapter 13: Transition to Multiengine Airplanes › Low Altitude Engine Failure Scenarios › Landing Gear Control Selected Up, Single-Engine Climb Performance Inadequate

  Landing Gear Control Selected Up, Single-Engine Climb Performance Inadequate When operating near or above the single-engine ceiling and an engine failure is experienced shortly after lift-off, a landing needs to be accomplished on whatever essentially lies ahead ... Figure 13-19] There is also the option of continuing ahead, in a descent at VYSE with the remaining engine producing power, as long as the pilot is not tempted to remain airborne beyond the airplane’s performance capability. Remaining…

• Airplane Flying Handbookp. 13-34
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Approach and Landing

  performance variations caused by engine and propeller wear, turbulence, and pilot technique, the airplane may not maintain altitude even at its published single-engine ceiling. Any further rate of sink, however, would likely be modest. An engine failure ... descent or other low power setting can be deceiving. The dramatic yaw and performance loss is absent. At very low power settings, the pilot may not even be aware of a failure. If a failure is suspected, the pilot should…

• Airplane Flying Handbookp. 9-28
  Chapter 9: Approaches and Landings › Emergency Approaches and Landings (Simulated)

  Emergency Approaches and Landings (Simulated) During dual training flights, the instructor should give simulated emergency landings by retarding the throttle and calling “simulated emergency landing.” The objective of these simulated emergency landings is to develop a pilot’s accuracy, judgment ... planning, procedures, and confidence when little or no power is available. A simulated emergency landing may be given with the airplane in any configuration. If the simulated power failure occurs while above best glide speed, the pilot allows the airplane…

• Airplane Flying Handbookp. 13-11
  Chapter 13: Transition to Multiengine Airplanes › Performance and Limitations

  highest altitude at which the airplane can maintain a steady rate of climb of 100 fpm with both engines operating. The airplane has reached its absolute ceiling when climb is no longer possible. ⦁ The single-engine service ceiling is reached ... when the multiengine airplane can no longer maintain a 50 fpm rate of climb with OEI, and its single-engine absolute ceiling when climb is no longer possible. The takeoff in a multiengine airplane should be planned in sufficient detail…

• Airplane Flying Handbookp. 13-34
  Chapter 13: Transition to Multiengine Airplanes › Engine Failure During Flight

  affected engine should be feathered and the securing failed engine checklist completed. The pilot should divert to the nearest suitable airport and declare an emergency with ATC for priority handling. Fuel crossfeed is a method of getting fuel from ... tank on one side of the airplane to an operating engine on the other. Crossfeed is used for extended single-engine operation. If a suitable airport is close at hand, there is no need to consider crossfeed. If prolonged flight…

• Airplane Flying Handbookp. 13-28
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › OEI Climb Performance

  Climb performance is reduced by the moderate sideslip. With wings level, VMC is significantly higher than published as there is no horizontal component of lift available to help the rudder combat asymmetrical thrust. Figure 13-15. Wings level engine ... engine. [Figure 13-16] This assumes no rudder input, the ball is displaced well toward the operative engine, and climb performance is greatly reduced by the large sideslip toward the operative engine. Due to the increased risk of loss…