Instrument Rating – Helicopter › VII. Emergency Operations › Task B. Instrument Approach and Landing with an Inoperative Engine (Simulated) (Multiengine Helicopter Only)

IH.VII.B.R5

Risk management

Configuring the helicopter.

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Helicopter Flying Handbook p. 2-26
Chapter 3: Helicopter Flight Controls
limited to the single main rotor type helicopter but are employed in one form or another in most helicopter configurations. All examples in this chapter refer to a counterclockwise main rotor blade rotation as viewed from above. If flying…
Helicopter Flying Handbook p. 1-4
Chapter 1: Introduction to the Helicopter › Rotor System › Rotor Configurations
Rotor Configurations Most helicopters have a single, main rotor but require a separate rotor to overcome torque which is a turning or twisting force. This is accomplished through a variable pitch, antitorque rotor or tail rotor. This is the design…
Instrument Flying Handbook p. 8-3
Chapter 8: Helicopter Attitude Instrument Flying › Instrument Flight › Aircraft Control
reference to the instruments, it is important to know the approximate power settings required for a particular helicopter in various load configurations and flight conditions. Trim, in helicopters, refers to the use of the cyclic centering button, if the helicopter…
Helicopter Flying Handbook p. 1-4
Chapter 1: Introduction to the Helicopter › Rotor System › Intermeshing Rotors
mounted on a mast, with the same axis of rotation, one above the other. This configuration is a noted feature of helicopters produced by the Russian Kamov helicopter design bureau. [Figure 1-7] Intermeshing Rotors Intermeshing rotors on a helicopter ... intermesh without colliding. [Figure 1-8] This arrangement allows the helicopter to function without the need for a tail rotor. It has high stability and powerful lifting capability. This configuration is sometimes referred to as a synchropter. The arrangement…
Helicopter Flying Handbook p. 1-2
Chapter 1: Introduction to the Helicopter › Turbine Age
main rotor, it was the single main rotor with an antitorque tail rotor configuration that would come to be recognized worldwide as the helicopter. Figure 1-1. Search and rescue helicopter conducting a pinnacle approach. Figure 1-2. Search…
Instrument Procedures Handbook p. 7-3
Chapter 7: Helicopter Instrument Procedures › Helicopter Flight Manual Limitations
using two pilots. In addition, the Helicopter Flight Manual (HFM) defines systems and functions that are required to be in operation or engaged for IFR flight in either the single or two-pilot configurations. Often, in a two-pilot operation ... Figure 7-2] • VNEI (never exceed speed—IFR) • Maximum approach angle • Weight and center of gravity (CG) limits • Helicopter configuration limitations (such as door positions and external loads) • Helicopter system limitations (generators, inverters, etc.) • System testing requirements (many avionics…