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AI.XIII.C.S2d

Skill

Demonstrate smooth control inputs when transitioning between various airspeeds and configurations, which include:

Windmilling propeller on the inoperative engine

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From the FAA library

  • Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Approach and Landing

    With drag from only one windmilling propeller, the airplane tends to float…

  • Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › Derivation of VMC

    determination (section 23.149(b)(5)). VMC increases with increased drag on the inoperative engine. VMC is highest, therefore, when the critical engine propeller is windmilling at the low pitch, high rpm blade angle. VMC is normally determined with the critical…

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

    VMC is highest, therefore, when the critical engine propeller is windmilling at…

  • Chapter 13: Transition to Multiengine Airplanes › Operation of Systems › Feathering Propellers

    inoperative engine minimizes propeller drag. [Figure 13-2] Depending upon single-engine performance, this feature often permits continued flight to a suitable airport following an engine failure. Feathering is important because of the change in parasite drag with propeller blade ... smaller blade angles near the flat pitch position, the drag added by the propeller is large. At these small blade angles, the propeller windmilling at high revolutions per minute (rpm) can create enough drag to make the airplane difficult…

  • 14 CFR Part 135, Appendix A to Part 135—Additional Airworthiness Standards for 10 or More Passenger Airplanes

    gravity, the critical engine inoperative, the remaining engines at the maximum takeoff power or thrust, and the propeller of the inoperative engine windmilling with the propeller controls in the normal position except that, if an approved automatic feathering system…