AI.VII.K.K4

From the FAA library

• Seaplane, Skiplane, and Float/Ski Equipped Helicopter Operations Handbookp. 5-1
  PERFORMANCE CONSIDERATIONS FOR TAKEOFF, CLIMB, CRUISE, AND LANDING › TAKEOFF

  experienced seaplane instructor can assist with choosing an appropriate power setting and demonstrating proper technique. CLIMB AND CRUISE When comparing the performance of an airplane with wheels to the same airplane equipped with floats, the drag and weight penalty ... lower for a particular power setting. This in turn means increased fuel consumption and reduced range. Unless the airplane was originally configured as a seaplane, the performance and flight planning information for a landplane converted to floats will typically…

• Pilot's Handbook of Aeronautical Knowledgep. 6-8
  Chapter 6: Flight Controls › Flight Control Systems › V-Tail

  stabilizer/rudder and creates a sideward lift that moves the tail to the right and yaws the nose of the airplane to the left. Rudder effectiveness increases with speed; therefore, large deflections at low speeds and small deflections at high speeds ... utilizes two slanted tail surfaces to perform the same functions as the surfaces of a conventional elevator and rudder configuration. The fixed surfaces act as both horizontal and vertical stabilizers. [Figure 6-16] The movable surfaces, which are usually called…

• Pilot's Handbook of Aeronautical Knowledgep. G-34
  Glossary › Pilot’s Operating Handbook/Airplane Flight Manual

  vertical speed indicator. VS0. The stalling speed or the minimum steady flight speed in the landing configuration. In small airplanes, this is the power-off stall speed at the maximum landing weight in the landing configuration (gear and flaps down ... limit of the white arc. VS1. The stalling speed or the minimum steady flight speed obtained in a specified configuration. For most airplanes, this is the power-off stall speed at the maximum takeoff weight in the clean configuration (gear…

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

  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 ... type rating is not required by regulation accepts major responsibility for the safety of future passengers. Many newer light airplanes are comparable in performance and complexity to transport airplanes. For these, the flight instructor’s checkout should be at least…

• Pilot's Handbook of Aeronautical Knowledgep. 5-35
  Chapter 5: Aerodynamics of Flight › Load Factors › Load Factors and Stalling Speeds

  imposed on structures by stalling an aircraft at relatively high airspeeds. The following information primarily applies to fixed-wing airplanes. The maximum speed at which an airplane may be stalled safely is now determined for all new designs. This speed ... below which you can move a single flight control, one time, to its full deflection, for one axis of airplane rotation only (pitch, roll or yaw), in smooth air, without risk of damage to the airplane. VA must be entered…

• Pilot's Handbook of Aeronautical Knowledgep. 11-12
  Chapter 11: Aircraft Performance › Climb Performance Factors › Region of Reversed Command

  speed at which the lowest brake horsepower sustains level flight. This is termed the best endurance airspeed. An airplane performing a low airspeed, high pitch attitude power approach for a short-field landing is an example of operating ... pilot to reduce or stop the descent by applying power. But without further use of power, the airplane would probably stall or be incapable of flaring for the landing. Merely lowering the nose of the airplane to regain flying speed…