AI.IX.C.S6

From the FAA library

• Airplane Flying Handbookp. 10-5
  Chapter 10: Performance Maneuvers › Chandelle

  slip or turn coordinator, and by using appropriate control pressures. At the 90° point, the pilot should begin to smoothly roll out of the bank at a constant rate while maintaining the pitch attitude attained ... rollout is begun at the start of the final 90°. As the rollout continues, the vertical component of lift increases. However, as speed continues to decrease, a slight increase of elevator back pressure is required to keep the pitch attitude…

• Airplane Flying Handbookp. 3-8
  Chapter 3: Basic Flight Maneuvers › Straight-and-Level Flight › Level Flight

  result, the pilot can develop the ability to adjust the change desired in the airplane’s attitude by the amount and direction of pressures applied to the flight controls without the pilot excessively referring to instrument or outside references ... each minor correction. The pitch attitude for level flight is first obtained by the pilot being properly seated, selecting a point toward the airplane’s nose as a reference, and then keeping that reference point in a fixed position relative…

• Airplane Flying Handbookp. 5-11
  Chapter 5: Maintaining Aircraft Control: Upset Prevention and Recovery Training › Slow Flight › Maneuvering in Slow Flight

  airplanes, torque, slipstream effect, and P-factor may produce a strong left yaw, which requires right rudder input to maintain coordinated flight. The closer the airplane is to the 1G stall, the greater the amount of right rudder pressure required ... Figure 5-7. Slow flight—low airspeed, high angle of attack, high power, and constant altitude. Maneuvering in Slow Flight When the desired pitch attitude and airspeed have been established in straight-and-level slow flight, the pilot needs…

• Airplane Flying Handbookp. 18-18
  Chapter 18: Emergency Procedures › Inadvertent VFR Flight Into IMC › Attitude Control

  Attitude Control An airplane is, by design, an inherently stable platform and, except in turbulent air, maintains approximately straight-and-level flight if properly trimmed and left alone. It is designed to maintain a state of equilibrium in pitch, roll ... others. The typical light airplane exhibits a good deal of stability in the yaw axis, slightly less in the pitch axis, and even lesser still in the roll axis. The key to emergency airplane attitude control, therefore, is to: ⦁ Trim…

• 14 CFR Part 61 — Certification: Pilots, Flight Instructors, and Ground InstructorsOpen
  14 CFR Part 61, Appendix A to Part 61—Airman Certification Standards and Practical Test Standards

  Part 61, Appendix A to Part 61—Airman Certification Standards and Practical Test Standards with a Sport Pilot Rating Practical Test Standards for Powered Parachute Category and Weight-Shift-Control Aircraft Category, June 2026. Flight Instructor Certificate with a Sport ... Pilot Rating; Powered Parachute Category Privileges, Weight-Shift-Control Aircraft Category Privileges Instrument Rating—Airplane Instrument Proficiency Check—Airplane | FAA-S-ACS-8C, Instrument Rating—Airplane Airman Certification Standards, November 2023. Instrument Rating—Helicopter Instrument Proficiency Check—Helicopter…