IL.XIV.I.K4
KnowledgeAircraft slope limitations.
From the FAA library
- Glossary › Pilot’s Operating Handbook/Airplane Flight Manual
airplane is capable of generating at a given speed. Also shows the safe load factor limits and the load factor that the aircraft can sustain at various speeds. Victor airways. Airways based on a centerline that extends from ... navigation aids or intersections); used to establish a known route for en route procedures between terminal areas. Visual approach slope indicator (VASI). A visual aid of lights arranged to provide descent guidance information during the approach to the runway…
- Chapter 10: Weight and Balance › Control › Weight and Balance Restrictions
runway length, runway surface, runway slope, surface wind, and the presence of obstacles. These factors may require a reduction in or redistribution of weight prior to flight. Figure 10-4. Establishing a balance. Some aircraft are designed so that ... difficult to load them in a manner that places the CG out of limits. These are usually small aircraft with the seats, fuel, and baggage areas located near the CG limit. Pilots must be aware that while within CG limits…
- 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…
- 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…
- 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…
- 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…