PI.IX.D.R1

From the FAA library

• Instrument Flying Handbookp. 5-27
  Chapter 5: Flight Instruments › Flight Management Systems (FMS) › Electronic Flight Instrument Systems

  Electronic Flight Instrument Systems Modern technology has introduced into aviation a new method of displaying flight instruments, such as electronic flight instrument systems, integrated flight deck displays, and others. For the purpose of the practical test standards, any flight instrument ... display that utilizes LCD or picture tube like displays is referred to as “electronic flight instrument display” and/or a glass flight deck. In general aviation there is typically a primary flight display (PFD) and a multi-function display (MFD). Although…

• Pilot's Handbook of Aeronautical Knowledgep. 8-11
  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…

• Aviation Instructor's Handbookp. 9-12
  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…

• Pilot's Handbook of Aeronautical Knowledgep. 6-2
  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…

• 14 CFR Part 91 — General Operating and Flight RulesOpen
  14 CFR § 91.1062 Duty periods and rest requirements: Flight attendants.

  Duty periods and rest requirements: Flight attendants. at least one flight attendant in addition to the minimum flight attendant complement required for the flight or flights in that duty period under the program manager's management specifications. (5) A program ... manager may assign a flight attendant to a scheduled duty period of more than 16 hours, but no more than 18 hours, if the program manager has assigned to the flight or flights in that duty period at least…

• 14 CFR Part 91 — General Operating and Flight RulesOpen
  14 CFR § 91.109 Flight instruction; Simulated instrument flight and certain flight tests.

  Flight instruction; Simulated instrument flight and certain flight tests. (a) No person may operate a civil aircraft (except a manned free balloon) that is being used for flight instruction unless that aircraft has fully functioning dual controls. However, instrument flight ... controls the elevator and ailerons, in place of fixed, dual controls, when— (1) The instructor has determined that the flight can be conducted safely; and (2) The person manipulating the controls has at least a private pilot certificate with appropriate…