TC 3-04.1-4 governs fundamentals of flight, including aerodynamics, aircraft performance, loads, environmental flight, and flight operations.
View TC 3-04.1-4 on armypubs.army.mil
It covers rotary-wing and fixed-wing aerodynamics, weight and balance, hazardous and external loads, environmental and night flight, terrain flight, formations, and aircraft control. It requires attention to aircraft performance, operating limitations, preflight inspections, crew coordination, and hazard avoidance.
Compressibility effects on the helicopter increase the power required to maintain rotor RPM and cause rotor roughness, vibration, cyclic shake, and an undesirable structural twisting of the blade. (paragraph 1-256)
Lift is the component of the total aerodynamic force on an airfoil and acts perpendicular to the relative wind. (paragraph 1-74)
Nets and slings with frayed or cut webbing are not used for external loads. (paragraph 2-68)
Aviators must determine which terrain flight mode to use in each segment of the planned route during the mission planning sequence. (paragraph 5-15)
The success and safety of multi-aircraft operations require all crew members in the flight to understand and utilize approved crew coordination techniques and terminology. (paragraph 6-3)