FH.XI.F.K2d
KnowledgeSystem and equipment malfunctions specific to the helicopter-simplified flight controls, including:
Electronic flight instrument display malfunction
From the FAA library
- Chapter 8: Flight Instruments › Electronic Flight Display (EFD) › Air Data Computer (ADC)
Air Data Computer (ADC) EFDs utilize the same type of instrument inputs…
- Chapter 8: Flight Instruments › Electronic Flight Display (EFD)
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 corrections when utilizing alternate static pressure. Figure 8-11. Blocked static system. Electronic Flight Display (EFD) Advances in technology have…
- Chapter 9: Techniques of Flight Instruction › Postflight Evaluation › First Solo Flight
First Solo Flight During the learner’s first solo flight, the instructor needs to be present to assist in answering questions or resolving any issues that arise during the flight. To ensure the solo flight is a positive, confidence-building ... experience for the learner, the flight instructor needs to consider time of day when scheduling the flight. Time of day is a factor in traffic congestion, possible winds, sun angles, and reflection. If possible, the flight instructor needs access…
- Chapter 9: Techniques of Flight Instruction › Integrated Flight Instruction › Development of Habit Patterns
Integrated Flight Instruction Integrated flight instruction is flight instruction during which learners are taught to perform flight maneuvers both by outside visual references and by reference to flight instruments. For this type of instruction to be fully effective ... instrument references should begin the first time each new maneuver is introduced. No distinction in the pilot’s operation of the flight controls is permitted, regardless of whether outside references or instrument indications are used for the performance…
- 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 ... 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 to control inputs while allowing a natural feel…
- 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…