HI.XI.G.K4

From the FAA library

• Helicopter Flying Handbookp. 13-10
  Chapter 13: Effective Aeronautical Decision-Making › Risk Management › Four Risk Elements

  Figure 13-5. Risk elements to evaluate in decision-making. personal evaluations of the aircraft, such as its powerplant, performance, equipment, fuel state, or airworthiness. A situation to consider: en route to an oil rig an hour’s flight from…

• Pilot's Handbook of Aeronautical Knowledgep. 11-15
  Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Takeoff Performance

  effect on takeoff performance. While subsequent corrections are appropriate for the effect of temperature on certain items of powerplant performance, density altitude defines specific effects on takeoff performance. An increase in density altitude can produce a twofold effect on takeoff…

• Pilot's Handbook of Aeronautical Knowledgep. 11-5
  Chapter 11: Aircraft Performance › Performance › Straight-and-Level Flight

  flight performance involve steady-state flight conditions and equilibrium of the aircraft. For the aircraft to remain in steady, level flight, equilibrium must be obtained by a lift equal to the aircraft weight and a powerplant thrust equal…

• Pilot's Handbook of Aeronautical Knowledgep. 4-9
  Chapter 5: Aerodynamics of Flight

  Chapter Summary Modern general aviation aircraft have what may be considered high performance characteristics. Therefore, it is increasingly necessary that pilots appreciate and understand the principles upon which the art of flying is based. For additional information on the principles ... flight are thrust, drag, lift, and weight. They are defined as follows: • Thrust—the forward force produced by the powerplant/ propeller or rotor. It opposes or overcomes the force of drag. As a general rule, it acts parallel…

• Aviation Instructor's Handbookp. 5-26
  Chapter 5: The Teaching Process › Types of Instructional Aids › Enhanced Training Materials

  learners understand how to perform the maneuver or procedure and also become familiar with the performance criteria. The examiner for the Airframe and Powerplant (A&P) is required to ask four questions in each of the subject areas, which…

• Helicopter Flying Handbookp. 11-18
  Chapter 11: Helicopter Emergencies and Hazards › System Malfunctions › Loss of Tail Rotor Effectiveness (LTE)

  prevent spinning once the helicopter lifts off the ground. A helicopter is heavy, and the powerplant places a high demand on fuel. Weight penalizes performance, but all helicopters must have an antitorque system, which adds weight. Therefore, the tail rotor…