Tutor Platform
Study note

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.

Sign in to generate a study note

From the FAA library

  • Chapter 7: Ground Reference Maneuvers › Turns Around a Point

    achieve this goal. The following are the most common errors in the performance of turns around a point: 1. Failure to adequately clear the surrounding area for safety hazards, initially and throughout the maneuver. 2. Failure to establish a constant ... level altitude prior to entering the maneuver. 3. Failure to maintain altitude during the maneuver. 4. Failure to properly assess wind direction. 5. Failure to properly execute constant-radius turns. 6. Failure to manipulate the flight controls in a smooth…

  • Chapter 13: Transition to Multiengine Airplanes › Engine Failure During Flight

    Engine Failure During Flight Engine failures well above the ground are handled differently than those occurring at lower speeds and altitudes. Cruise airspeed allows better airplane control and altitude, which may permit time for a possible diagnosis and remedy ... failure. Maintaining airplane control, however, is still paramount. Airplanes have been lost at altitude due to apparent fixation on the engine problem to the detriment of flying the airplane. Not all engine failures or malfunctions are catastrophic in nature (catastrophic…

  • Chapter 18: Emergency Procedures › System Malfunctions › Electrical System

    critical systems, and therefore should not be taken lightly even in day/visual flight rules (VFR) conditions. Most in-flight failures of the electrical system are located in the generator or alternator. Once the generator or alternator system goes off line ... light airplane is a battery. If a warning light or ammeter indicates the probability of an alternator or generator failure in an airplane with only one generating system, however, the pilot may have very little time available from the battery…

  • Chapter 18: Emergency Procedures › System Malfunctions › Pitot-Static System

    regardless of aircraft or manufacturer. By comparing information between the six conventional instruments, pilots are able to diagnose common failure modes. Instrument failure indications of conventional instruments and electronic flight displays may be entirely different, and electronic systems failure indications ... equipment malfunctions of electronic flight instrument displays. Rapidly changing equipment, complex systems, and the difficulty or inability to simulate failure modes and functions can impose training limitations. Pilots still should be able to respond to equipment malfunctions in a timely…

  • Chapter 13: Transition to Multiengine Airplanes › Low Altitude Engine Failure Scenarios › Landing Gear Control Selected Up, Single-Engine Climb Performance Inadequate

    Selected Up, Single-Engine Climb Performance Inadequate When operating near or above the single-engine ceiling and an engine failure is experienced shortly after lift-off, a landing needs to be accomplished on whatever essentially lies ahead. [Figure ... within the performance capability of the airplane to do so. An accident is inevitable. Figure 13-19. Engine failure on takeoff, inadequate climb performance. Analysis of engine failures on takeoff reveals a very high success rate of off-airport engine…

  • Chapter 11: Helicopter Emergencies and Hazards › System Malfunctions › Antitorque System Failure

    following the manufacturer’s recommendations regarding operating limits and procedures and periodic maintenance and inspections, many system and equipment failures can be eliminated. Certain malfunctions or failures can be traced to some error on the part of the pilot; therefore ... appropriate flying techniques and use of threat and error management may help to prevent an emergency Antitorque System Failure Antitorque failure usually falls into one of two categories. One is failure of the power drive portion of the tail rotor…