Instrument Rating – Powered-Lift › VII. Emergency Operations › Task B. Powerplant(s) Inoperative (Simulated) during Straight-and-Level Flight and Turns

IP.VII.B.R6

Risk management

Configuring the aircraft.

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Get a short, cited explanation of this element written from the FAA handbooks: the core idea, the numbers that matter, common test traps, and a quick self-check.

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Pilot's Handbook of Aeronautical Knowledge p. 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 Knowledge p. 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 Handbook p. 4-16
Chapter 4: Aerodynamic Factors › Piper PA-34-200T (Des Moines, Iowa) › Tailplane Stall Symptoms
apply appropriate nose-up elevator pressure; • Increase airspeed appropriately for the reduced flap extension setting; • Apply sufficient power for aircraft configuration and conditions. (High engine power settings may adversely impact response to tailplane stall conditions at high airspeed in some…
Instrument Flying Handbook p. 5-2
Chapter 5: Flight Instruments
around the aircraft. The pitot tube connects to the ASI or an air data computer depending on your aircraft's configuration…
Risk Management Handbook p. 7-2
Chapter 7: Automation & Flight Path Management › Balancing Automated & Manual Flight
Continuing the scenario above, the pilot loads the instrument approach and decides to remain on autopilot. However, after the aircraft passes the initial approach fix, ATC cancels the approach clearance. ATC provides vectors and tells the pilot to expect ... comply with the assignment from ATC. The lower level of automation allows the pilot to program and configure the aircraft for an unexpected change while keeping the flightpath and aircraft state under control. 12295 Pilots may sometimes choose to disengage…
Airplane Flying Handbook p. 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…