IP.IV.B.R3
Risk managementControl input errors, inducing undesired aircraft attitudes.
From the FAA library
- 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 › Aircraft Control During Instrument Flight
Trim (fine tune the control forces) until control pressures are neutralized. Trimming for hands-off flight is essential for smooth, precise aircraft control. Figure 6-2. Performance instruments. Figure 6-3. Navigation instruments. It allows a pilot to attend ... other flight deck duties with minimum deviation from the desired attitude. 3. Cross-check the performance instruments to determine if the established attitude or power setting is providing the desired performance. The cross-check involves both seeing and interpreting…
- 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…
- 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 6, Section II: Airplane Attitude Instrument Flying › Learning Methods › Power Control
Different aircraft demand differing amounts of throttle change to produce specific performance. It is imperative that the pilot make the specific changes on the power instruments and allow the performance to stabilize. Avoid the tendency to overcontrol. One common error ... digital readouts. This precision causes pilots to focus too much attention on establishing the exact power setting. Control and power instruments are the foundation for precise attitude instrument flying. The keys to attitude instrument flying are establishing the desired aircraft…
- 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…