AI.XII.C.K2f

From the FAA library

• Risk Management Handbookp. 3-6
  Chapter 3: Identifying Hazards & Associated Risks › Aircraft Hazards › Equipage

  weight reduces climb performance. • Weight and Balance–Pilots who do not check center of gravity limits may experience difficulty trimming or controlling the aircraft, which could lead to a loss of control in-flight. Equipage The avionics and other equipment ... pilot workload. A pilot flying an aircraft in these conditions might consider aircraft without an autopilot an “A” hazard. • Inoperative Equipment–Inoperative equipment triggers an “A” hazard. For example, an inoperative landing light may make night operation more hazardous, even…

• Airplane Flying Handbookp. 15-1
  Index

  Electrical fires Elementary eights Eights across a road Eights along a road Eights around pylons Eights-on-pylons Elevator trim stall Emergencies Emergency approaches and landings (simulated) Emergency descents Emergency landings Psychological hazards 18-1 Types of emergency landings Ditching ... Engine and propeller Engine failure: After lift-off After takeoff After takeoff (single-engine) During flight Engine fire Engine inoperative approach and landing Engine inoperative flight principles Engines Engine shutdown Engine starting Environmental factors Exhaust gas temperature (EGT) F False…

• Airplane Flying Handbookp. 13-8
  Chapter 13: Transition to Multiengine Airplanes › Operation of Systems › Yaw Damper

  that the command bars are pulled from view. Prior to system engagement, all FD/AP computer and trim checks should be accomplished. Many newer systems cannot be engaged without the completion of a self-test. The pilot should also be familiar ... damper should be off for takeoff and landing. There may be additional restrictions against its use with one engine inoperative. Most yaw dampers can be engaged independently of the autopilot…

• Airplane Flying Handbookp. 13-24
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › ⦁ All propeller controls in the recommended takeoff position throughout VMC determination

  VMC is highest, therefore, when the critical engine propeller is windmilling at…

• Airplane Flying Handbookp. 13-26
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › VMC Demo

  The following description assumes a twin with non-counter-rotating engines, where…

• Airplane Flying Handbookp. 13-35
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Approach and Landing

  With drag from only one windmilling propeller, the airplane tends to float…