AI.II.F.K2c

From the FAA library

• Airplane Flying Handbookp. G-19
  Index

  twin-engine airplane with one engine inoperative that involves a small amount of bank and slightly uncoordinated flight to align the fuselage with the direction of travel and minimize drag. Zero thrust (simulated feather). An engine configuration with ... distance Accelerate-stop distance After-landing After-landing roll Aircraft energy management Airframe and systems Airplane-based UPRT Airplane configuration Airplane equipment and lighting Airport and navigation lighting aids Airport traffic patterns and operations All-attitude/all-envelope flight training methods…

• Airplane Flying Handbookp. 18-4
  Chapter 18: Emergency Procedures › Basic Safety Concepts › Airplane Configuration

  Airplane Configuration Since flaps improve maneuverability at slow speed, and lower the stalling speed, their use during final approach is recommended when time and circumstances permit. However, the associated increase in drag and decrease in gliding distance call for caution ... available, a gear-up landing on level, but soft terrain or across a plowed field may result in less airplane damage than a gear-down landing. [Figure 18-3] Deactivation of the airplane’s electrical system before touchdown reduces…

• Airplane Flying Handbookp. 6-1
  Chapter 6: Takeoffs and Departure Climbs › Introduction

  airplanes (tail-wheel) are discussed in Chapter 14: Transition to Tailwheel Airplanes. The manufacturer’s recommended procedures pertaining to airplane configuration, airspeeds, and other information relevant to takeoffs and departure climbs in a specific make and model airplane are contained…

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

  desired configuration (i.e., approximately 5–10 knots above the stall speed for that flight condition), additional power will be needed to maintain altitude. During these changing flight conditions, the pilot should trim the airplane to compensate for changes in control ... extended to the landing position, as applicable. It is recommended the prescribed before-landing checks be completed to configure the airplane. The extension of gear and flaps typically occurs once cruise power has been reduced and at appropriate airspeeds…

• Pilot's Handbook of Aeronautical Knowledgep. 5-21
  Chapter 5: Aerodynamics of Flight › Effect of Wing Planform

  combined with low aspect ratio, it results in flying qualities very different from a more conventional high aspect ratio airplane configuration. Such airplanes require very precise and professional flying techniques, especially at slow speeds, while airplanes with a high aspect…

• 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 ... 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 up, if retractable…