PH.II.B.R1
Risk managementUse of systems or equipment, including automation and portable electronic devices.
From the FAA library
- Chapter 4: Helicopter Components, Sections, and Systems › Stability Augmentations Systems › Force Trim
position that gave a control force to transitioning airplane pilots who had become accustomed to such control forces. The system uses a magnetic clutch and springs to hold the cyclic control in the position where it was released. The system ... controls. Some recent basic systems are referred to as attitude retention systems. Active Augmentation Systems So-called actual augmentation systems use electric actuators that provide input to the hydraulic servos. These servos receive control commands from a computer that senses…
- 14 CFR § 91.108 Use of supplemental restraint systems.
Use of supplemental restraint systems. confirmation from the operator or any individual providing the supplemental restraint system of the system's continued serviceability and readiness for its intended purpose before each takeoff; (3) May only permit an individual to use ... criteria for which the supplemental restraint system is rated; (4) Has final authority regarding whether the supplemental restraint system may be used during flight operations; and (5) Has final authority to authorize an individual to release the FAA-approved safety…
- 14 CFR Part 91, Special Federal Aviation Regulation No. 97—Special Operating Rules for the Conduct of Instrument Flight Rules (IFR) Area Navigation (RNAV) Operations using Global Positioning Systems
Regulation No. 97—Special Operating Rules for the Conduct of Instrument Flight Rules (IFR) Area Navigation (RNAV) Operations using Global Positioning Systems (GPS) in Alaska 54°00′00.00″ N., Long ... time determination system that uses satellite ranging signals to determine user location. It encompasses all satellite ranging technologies, including GPS and additional satellites. Components of the GNSS include GPS, the Global Orbiting Navigation Satellite System, and WAAS satellites. Global Positioning…
- Chapter 4: Helicopter Components, Sections, and Systems › Stability Augmentations Systems › Active Augmentation Systems
inputs adjust attitude, power and aircraft trim for a more stabilized flight. Once engaged by the pilot, these actual systems use a multitude of sensors, from stabilized gyros to electromechanical actuators, which provide instantaneous inputs to all flight controls without ... desired. Stability augmentation systems reduce pilot workload by improving basic aircraft control harmony and decreasing disturbances. These systems are very useful when the pilot is required to perform other duties, such as sling loading and search-and-rescue operations. Other…
- 14 CFR Part 135 — Operating Requirements: Commuter and on Demand Operations and Rules Governing Persons on Board Such AircraftOpen14 CFR § 135.105 Exception to second in command requirement: Approval for use of autopilot system.
Exception to second in command requirement: Approval for use of autopilot system. (a) Except as provided in §§ 135.99 and 135.111, unless two pilots are required by this chapter for operations under VFR, a person may operate an aircraft without ... second in command, if it is equipped with an operative approved autopilot system and the use of that system is authorized by appropriate operations specifications. No certificate holder may use any person, nor may any person serve, as a pilot…
- Chapter 5: Flight Instruments › Gyroscopic Systems › Electrical Systems
aircraft. A.C. is used to operate some attitude gyros and autopilots. Aircraft with only D.C. electrical systems can use A.C. instruments via installation of a solid-state D.C. to A.C. inverter, which changes ... volts D.C. into three-phase 115-volt, 400-Hz A.C. Figure 5-28. Single-engine instrument vacuum system using a steel-vane, wet-type vacuum pump. Figure 5-29. Twin-engine instrument pressure system using a carbon-vane, dry-type…