IP.VII.B.S9
SkillMaintain control and fly within the aircraft’s operating limitations.
From the FAA library
- Chapter 6: Flight Controls › Flight Control Systems › Spoilers
Trim Systems Although an aircraft can be operated throughout a wide range of attitudes, airspeeds, and power settings, it can be designed to fly hands-off within only a very limited combination of these variables. Trim systems are used ... relieve the pilot of the need to maintain constant pressure on the flight controls, and usually consist of flight deck controls and small hinged devices attached to the trailing edge of one or more of the primary flight control surfaces…
- Chapter 6: Flight Controls › Flight Control Systems › Primary Flight Controls
Flight Control Systems Flight Controls Aircraft flight control systems consist of primary and secondary systems. The ailerons, elevator (or stabilator), and rudder constitute the primary control system and are required to control an aircraft safely during flight. Wing flaps, leading ... edge devices, spoilers, and trim systems constitute the secondary control system and improve the performance characteristics of the airplane or relieve the pilot of excessive control forces. Primary Flight Controls Aircraft control systems are carefully designed to provide adequate responsiveness…
- Chapter 6, Section I: Airplane Attitude Instrument Flying
Adjust the miniature aircraft with reference to the horizon bar for the particular airplane while on the ground. For some tricycle-gear airplanes, a slightly nose-low attitude on the ground gives a level flight attitude at normal cruising speed ... Shut Down When shutting down the engine, note any abnormal instrument indications. Chapter 6, Section I: Airplane Attitude Instrument Flying Attitude instrument flying is defined as the control of an aircraft’s spatial position by using instruments rather than outside…
- Chapter 6, Section I: Airplane Attitude Instrument Flying › Learning Methods › Pitch Control
Attitude Instrument Flying Using the Primary and Supporting Method Another basic method for teaching attitude instrument flying classifies the instruments as they relate to control function, as well as aircraft performance. All maneuvers involve some degree of motion about ... lateral (pitch), longitudinal (bank/ roll), and vertical (yaw) axes. Attitude control is stressed in this handbook in terms of pitch control, bank control, power control, and trim control. Instruments are grouped as they relate to control function and aircraft performance…
- Chapter 6, Section I: Airplane Attitude Instrument Flying › Learning Methods › Attitude Instrument Flying Using the Control and Performance Method
Learning Methods The two basic methods used for learning attitude instrument flying are “control and performance” and “primary and supporting.” Both methods utilize the same instruments and responses for attitude control. They differ in their reliance on the attitude indicator ... interpretation of other instruments. Attitude Instrument Flying Using the Control and Performance Method Aircraft performance is achieved by controlling the aircraft attitude and power. Aircraft attitude is the relationship of both the aircraft’s pitch and roll axes in relation…
- Chapter 8: Helicopter Attitude Instrument Flying › Instrument Flight › Aircraft Control
Aircraft Control Controlling a helicopter is the result of accurately interpreting the flight instruments and translating these readings into correct control responses. Aircraft control involves adjustment to pitch, bank, power, and trim in order to achieve a desired flight path ... Pitch attitude control is controlling the movement of the helicopter about its lateral axis. After interpreting the helicopter’s pitch attitude by reference to the pitch instruments (attitude indicator, altimeter, airspeed indicator, and vertical speed indicator (VSI)), cyclic control adjustments…