SH.II.C.R1
Risk managementRotor(s) engagement, as applicable.
From the FAA library
- Chapter 4: Helicopter Components, Sections, and Systems › Transmission System › Belt Drive Clutch
gradually increased. When the rotor and engine tachometer needles are superimposed, the rotor and the engine are synchronized, and the clutch is then fully engaged. Advantages of this system include vibration isolation, simple maintenance. When the clutch is not engaged…
- Chapter 11: Helicopter Emergencies and Hazards › Autorotation › Common Errors
application of controls and results in overcontrolling. 2. Failure to obtain and maintain a level attitude near the surface. 3. Failure to coordinate throttle and collective pitch properly, which results in either an engine overspeed or a loss of rotor ... Failure to coordinate proper antitorque pedal with the increase in power. 5. Late engine power engagement causing excessive temperature or torque, or rpm drop. 6. Failure to go around if not within limits and specified criteria for safe autorotation…
- Chapter 11: Helicopter Emergencies and Hazards › Autorotation › Technique (How to Practice)
engine from re-engaging. The idle detention position is a ridged stop position between idle and off in which the idle release button snaps into, prevent accidental throttle off. Helicopters with high-inertia rotor disks settle more slowly after ... throttle in the idle detent position to slow the descent and cushion the landing. The timing of collective control application and the rate at which it is applied depend upon the particular helicopter being used, its gross weight…
- Chapter 5: Engine Starting Systems › Air Turbine Starters
clutch gear to drive the output shaft of the starter. The clutch is an overrunning type to facilitate positive engagement and minimize chatter. When starter cut-out speed is reached, the start valve is closed. When ... clutch gear allowing the rotor to coast to a halt. The outboard clutch shaft continues to turn with the engine. Air Turbine Starter Troubleshooting Guide The troubleshooting procedures listed in Figure 5-25 are applicable to air turbine starting systems…