AP.VII.G.K1
KnowledgePrevention of unusual attitudes, including flight causal, physiological, and environmental factors, and system and equipment failures.
From the FAA library
- Appendix B: Acronyms, Abbreviations, and NOTAM Contractions
federal FEIS—Final Environmental Impact Statement FEP—front end processor FFAC—from facility FI/P—flight inspection permanent FI/T—flight inspection temporary FIFO—Flight Inspection Field Office FIG—flight inspection group FINO—Flight Inspection National Field Office FIPS—federal information publication ... standard FIR—flight information region FIRE—fire station FIRMR—Federal Information Resource Management Regulation FL—flight level FLOWSIM—traffic flow planning simulation FM—from FMA—final monitor aid FMF—facility master file FMIS—FTS2000 management information system FMS—flight management…
- 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: Flight Controls
Chapter Summary In order to sustain an aircraft in flight, a pilot must understand how thrust, drag, lift, and weight act on the aircraft. By understanding the aerodynamics of flight, how design, weight, load factors, and gravity affect an aircraft ... during flight maneuvers from stalls to high speed flight, the pilot learns how to control the balance between these forces. For information on stall speeds, load factors, and other important aircraft data, always consult the AFM/POH for specific information pertaining…
- Chapter 8: Flight Instruments › Electronic Flight Display (EFD)
altimeter to freeze at the altitude where the blockage occurred. In the case of the VSI, a blocked static system produces a continuous zero indication. [Figure 8-11] Some aircraft are equipped with an alternate static source in the flight ... deck. In the case of a blocked static source, opening the alternate static source introduces static pressure from the flight deck into the system. Flight deck static pressure is lower than outside static pressure. Check the aircraft AOM/POH for airspeed…
- Chapter 5: Mitigating Risk › Mitigating External Pressure Risks › Local Versus Transportation Flights
Cancel the Flight Canceling a flight is necessary if the pilot cannot mitigate risk sufficiently by other means. The cancellation option is easier if another means of transportation is available or if long-term rescheduling is an option. Mitigating External ... others waiting for the arrival, it is best to inform them of the need for flexibility. Local Versus Transportation Flights A local pleasure flight can still be subject to external pressures, but it is easier to cancel than a scheduled…
- Chapter 7, Section I: Airplane Basic Flight Maneuvers › Unusual Attitudes and Recoveries › Recovery from Unusual Attitudes
Recognizing Unusual Attitudes As a general rule, any time an instrument rate of movement or indication other than those associated with the basic instrument flight maneuvers is noted, assume an unusual attitude and increase the speed of cross-check ... confirm the attitude, instrument error, or instrument malfunction. Nose-high attitudes are shown by the rate and direction of movement of the altimeter needle, vertical speed needle, and airspeed needle, as well as the immediately recognizable indication of the attitude…