HI.V.A.R2

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 11-5
  Chapter 11: Aircraft Performance › Performance › Straight-and-Level Flight

  Level Flight All of the principal components of flight performance involve steady-state flight conditions and equilibrium of the aircraft. For the aircraft to remain in steady, level flight, equilibrium must be obtained by a lift equal to the aircraft ... weight and a powerplant thrust equal to the aircraft drag. Thus, the aircraft drag defines the thrust required to maintain steady, level flight. As presented in Chapter 4, Aerodynamics of Flight, all parts of an aircraft contribute to the drag…

• Aviation Instructor's Handbookp. C-4
  Appendix C: Certificates, Ratings, and Endorsements › Flight Instructor Endorsements › Aircraft Checkouts/Transitions

  Flight Instructors as Certifying Officials for Student Pilot and Remote Pilot Applicants, has process details for instructors and applicants. Aircraft Checkouts/Transitions Certificated pilots depend on flight instructors for aircraft checkouts and transition training including high performance airplanes, tail wheel airplanes ... motor gliders, and aircraft capable of flight at high altitudes. The flight instructor who checks out and certifies the competency of a pilot in an aircraft for which a type rating is not required by regulation accepts major responsibility…

• Pilot's Handbook of Aeronautical Knowledgep. 1-15
  Chapter 1: Introduction To Flying › Aircraft Classifications and Ultralight Vehicles

  Airplane—an engine-driven fixed-wing aircraft heavier than air, that is supported in flight by the dynamic reaction of the air against its wings. • Glider—a heavier-than-air aircraft, that is supported in flight by the dynamic reaction ... against its lifting surfaces and whose free flight does not depend principally on an engine. • Lighter-than-air aircraft—an aircraft that can rise and remain suspended by using contained gas weighing less than the air that is displaced…

• Pilot's Handbook of Aeronautical Knowledgep. 5-14
  Chapter 5: Aerodynamics of Flight › Aircraft Design Characteristics

  Aircraft Design Characteristics Each aircraft handles somewhat differently because each resists or responds to control pressures in its own way. For example, a training aircraft is quick to respond to control applications, while a transport aircraft feels heavy ... controls and responds to control pressures more slowly. These features can be designed into an aircraft to facilitate the particular purpose of the aircraft by considering certain stability and maneuvering requirements. The following discussion summarizes the more important aspects…

• Pilot's Handbook of Aeronautical Knowledgep. 9-7
  Chapter 9: Flight Manuals and Other Documents › Aircraft Documents › Certificate of Aircraft Registration

  flight tests by the manufacturer or in flights that are necessary for the sale of the aircraft by the manufacturer or a dealer. The dealer must remove the certificate when the aircraft is sold. Upon complying with 14 CFR part ... section 47.31, the pink copy of the application for an Aircraft Registration Application, Aeronautical Center (AC) Form 8050-1, provides authorization to operate an unregistered aircraft for a period not to exceed 90 days. Since the aircraft is unregistered…

• Pilot's Handbook of Aeronautical Knowledgep. 5-15
  Chapter 5: Aerodynamics of Flight › Aircraft Design Characteristics › Longitudinal Stability (Pitching)

  Negative dynamic stability—over time, the motion of the displaced object increases and becomes more divergent. Stability in an aircraft affects two areas significantly: • Maneuverability—the quality of an aircraft that permits it to be maneuvered easily and to withstand ... stresses imposed by maneuvers. It is governed by the aircraft’s weight, inertia, size and location of flight controls, structural strength, and powerplant. It too is an aircraft design characteristic. • Controllability—the capability of an aircraft to respond…