PH.VIII.F.R5
Risk managementLow inertia rotor systems.
From the FAA library
- Chapter 11: Helicopter Emergencies and Hazards › Autorotation › RPM Control
Control Rotor rpm in low inertia rotor systems has been studied in simulator flight evaluations which indicate that the simultaneous application of aft cyclic, down collective, and alignment with the relative wind (trim) at a wide range of airspeeds, including…
- Chapter 11: Helicopter Emergencies and Hazards › Low-G Conditions and Mast Bumping
energy and inertia in the rotor system can sever the mast or allow rotor blades to strike the tail or other portions of the helicopter. Figure 11-8. Result of improper corrective action in a low-G condition. Turbulence, especially…
- Chapter 11: Helicopter Emergencies and Hazards › System Malfunctions › Reducing the Onset of LTE
Reducing the Onset of LTE To help reduce the onset of LTE…
- OPERATIONAL CONSIDERATIONS
helicopter to settle to the ground, then reduce collective pitch to the full down position. In helicopters with low inertia rotor systems, an autorotation to a hard surface requires a more aggressive flare to a near-zero groundspeed to ensure…