AP.VII.D.S1
SkillRecognize and correctly identify powerplant(s) failure, complete memory items (if applicable), and maintain positive aircraft control.
From the FAA library
- Chapter 5: Aerodynamics of Flight › Axes of an Aircraft
Whenever an aircraft changes its flight attitude or position in flight, it rotates about one or more of the three axes. [Figure 5-18] The aircraft’s motion about its longitudinal axis resembles the roll of a ship from side ... side. In fact, the names used to describe the motion about an aircraft’s three axes were originally nautical terms. They have been adapted to aeronautical terminology due to the similarity of motion of aircraft and seagoing ships. The motion…
- Chapter 3: Aircraft Construction › Aircraft Design, Certification, and Airworthiness › A Note About Light Sport Aircraft
Note About Light Sport Aircraft Light sport aircraft are not designed according to FAA airworthiness standards. Instead, they are designed to a consensus of standards agreed upon in the aviation industry. The FAA has agreed the consensus of standards ... acceptable as the design criteria for these aircraft. Light sport aircraft do not necessarily have individually type certificated engines and propellers. Instead, a TC is issued to the aircraft as a whole. It includes the airframe, engine, and propeller. Aircraft…
- Chapter 3: Aircraft Construction › Lift and Basic Aerodynamics
Weight pulls the aircraft downward because of the force of gravity. It opposes lift and acts vertically downward through the aircraft’s center of gravity (CG). Lift opposes the downward force of weight, is produced by the dynamic effect ... wing, and acts perpendicular to the flight path through the wing’s center of lift (CL). An aircraft moves in three dimensions and is controlled by moving it about one or more of its axes. The longitudinal, or roll, axis…
- 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…
- 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…
- CHAPTER 2. REDUCING GENERAL AVIATION ACCIDENTS › 2.2 Manual Flight After Automation Failure › 2.2.3 Proficiency in Manual Aircraft Control
Proficiency in Manual Aircraft Control. Pilots should be proficient in manual aircraft control and should be able to operate the aircraft without the use of the aircraft’s automation. Advanced avionics and flight automation offer many levels of automation. Pilots ... understand that no one level of automation is appropriate for all flight situations. If a flight automation system failure occurs, in whole or in part, the pilot should possess the knowledge to address the situation. This may include isolating…