FH.IV.A.K1
KnowledgePurpose of the maneuver.
From the FAA library
- Chapter 9: Basic Flight Maneuvers › Ground Reference Maneuvers
controlling the helicopter and watching for other aircraft in the vicinity. Other examples of ground reference maneuvers are flights for photographic or observation purposes, such as pipe line or power line checks. Prior to each maneuver, a clearing turn should…
- Chapter 6: Flight Controls › Flight Control Systems › Primary Flight Controls
control column and/or rudder pedals may be limited. The purpose of these design limits is to prevent the pilot from inadvertently overcontrolling and overstressing the aircraft during normal maneuvers…
- Glossary › Domestic Reduced Vertical Separation Minimum
opening near the leading edge of a wing that ducts air onto the top surface of the wing. Its purpose is to increase lift at higher angles of attack. FL. See flight level. Flameout. A condition in the operation ... Basic maneuvers, flown by reference to the instruments rather than outside visual cues, for the purpose of practicing basic attitude flying. The patterns simulate maneuvers encountered on instrument flights such as holding patterns, procedure turns, and approaches…
- Chapter 6: Flight Controls › Flight Control Systems › Ailerons
purpose of these design limits is to prevent the pilot from inadvertently overcontrolling and overstressing the aircraft during normal maneuvers. A properly designed aircraft is stable and easily controlled during normal maneuvering. Control surface inputs cause movement about the three…
- Chapter 5: Aerodynamics of Flight › Aircraft Design Characteristics
pressures more slowly. These features can be designed into an aircraft to facilitate the particular purpose of the aircraft by considering certain stability and maneuvering requirements. The following discussion summarizes the more important aspects of an aircraft’s stability, maneuverability…
- Chapter 10: Advanced Flight Maneuvers › Maximum Performance Takeoff › Technique
cyclic, as necessary, to control movement toward the desired flightpath and, therefore, climb angle during the maneuver (position 3). Maintain rotor rpm at its maximum, and do not allow it to decrease since you would probably need to lower ... clears the obstacle, or until reaching 50 feet for demonstration purposes (position 4). Then, establish a normal climb attitude and power setting (position 5). As in any maximum performance maneuver, the techniques used affect the actual results. Smooth, coordinated inputs…