IP.VII.C.R4

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 11-10
  Chapter 11: Aircraft Performance › Climb Performance Factors › Range Performance

  condition is obtained at maximum lift/ drag ratio (L/DMAX), and it is important to note that for a given aircraft configuration, the L/DMAX occurs at a particular AOA and lift coefficient and is unaffected by weight or altitude. A variation ... cases, it is not always true as there are different variables to every situation. Each aircraft configuration is different, and there is not a rule of thumb that encompasses all of them as to how to achieve the max range…

• Pilot's Handbook of Aeronautical Knowledgep. 11-17
  Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Landing Performance

  When minimum landing distances are considered, braking friction forces predominate during the landing roll and, for the majority of aircraft configurations, braking friction is the main source of deceleration. The minimum landing distance varies in direct proportion to the gross ... effect of wind on landing distance is large and deserves proper consideration when predicting landing distance. Since the aircraft lands at a particular airspeed independent of the wind, the principal effect of wind on landing distance is the change…

• Instrument Procedures Handbookp. G-11
  Glossary

  intermediate altitude in advance when flying a high performance aircraft, you can plan the power or thrust settings and aircraft configurations that result in the most efficient descent, in terms of time, fuel requirements, and engine wear. Visual Approach…

• Pilot's Handbook of Aeronautical Knowledgep. 8-9
  Chapter 8: Flight Instruments › Airspeed Indicator Markings

  Lower limit of white arc (VS0)—the stalling speed or the minimum steady flight speed in the landing configuration. In small aircraft, this is the power-off stall speed at the maximum landing weight in the landing configuration (gear ... limit of green arc (VS1)—the stalling speed or the minimum steady flight speed obtained in a specified configuration. For most aircraft, this is the power-off stall speed at the maximum takeoff weight in the clean configuration (gear…

• Instrument Flying Handbookp. 10-21
  Chapter 10: IFR Flight › Approach to an Airport With an Operating Tower, With an Approach Control › Missed Approaches

  aircraft at any airport below the authorized MDA or continue an approach below the authorized DA/DH unless: 1. The aircraft is continuously in a position from which a descent to a landing on the intended runway can be made ... approach. When a MAP is initiated, a climb pitch attitude should be established while setting climb power. Configure the aircraft for climb, turn to the appropriate heading, advise ATC that a missed approach is being executed, and request further clearances…

• Airplane Flying Handbookp. 9-6
  Chapter 9: Approaches and Landings › Final Approach › Stabilized Approach Concept

  pilot applies a gust factor, indicated airspeed should not decay below the recommended landing speed. 4. Configuration. The aircraft is in the correct landing configuration with flaps as required; landing gear extended, and is in trim. 5. Descent rate ... rate prior to 300 ft AGL. 6. Power setting. The pilot should use a power setting appropriate for the aircraft configuration and not below the minimum power for approach as defined by the AFM. 7. Briefings and checklists. Completing…