IR.VII.B.R6
Risk managementConfiguring the aircraft.
From the FAA library
- 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…
- 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…
- Chapter 1: Introduction to Flight Training › Safety Considerations › Stall Awareness
pilot should understand and appreciate factors such as airspeed, pitch attitude, load factor, relative wind, power setting, and aircraft configuration in order to develop a reasonably accurate mental picture of the wing’s AOA at any particular time…
- Chapter 5: Maintaining Aircraft Control: Upset Prevention and Recovery Training › Slow Flight
maintain a selected altitude. It is essential that pilots: 1. understand the aerodynamics associated with slow flight in various aircraft configurations and attitudes, 2. recognize airplane cues in these flight conditions, 3. smoothly manage coordinated flight control inputs while maneuvering…
- 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…
- Chapter 5. DEVELOPING CHECKLISTS › 5.2 Methods for Managing Checklist Accomplishment › 5.2.4 Representative Items
pilots when incorporated in a checklist. 5. A checklist should not be depended upon to initiate a change in aircraft configuration. Operators should key aircraft configuration changes to specific operational events (e.g., direct the landing gear to be extended…