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  • Chapter 7: Aircraft Systems › Turbine Engines › Foreign Object Damage (FOD)

    utilized. Preflight procedures include a visual inspection for any sign of FOD. Turbine Engine Hot/Hung Start When the EGT exceeds the safe limit of an aircraft, it experiences a “hot start.” This is caused by too much fuel entering…

  • Chapter 13: Effective Aeronautical Decision-Making › Aeronautical Decision-Making (ADM) › Scenario

    shift when he receives a request for a patient pickup at a roadside vehicle accident. The pilot has started to feel the onset of a cold; his thoughts are on getting home and getting a good night’s sleep. After ... thunderstorms are approaching, the flight can be completed prior to their arrival. Figure 13-1. The pilot has a limited capacity of doing work and handling tasks, meaning there is a point at which the tasking exceeds the pilot…

  • Chapter 2: Personal Minimums › Personal Minimums › Step 5—Adjust for Specific Conditions

    additional safety margins [Figure 2-9] only provide a starting point. Pilots may develop their own adjustment factors based on experience, aircraft capabilities, and operation. If flying experience is limited or infrequent, the adjustment magnitude could increase. If multiple special…

  • Chapter 5. Air Traffic Procedures › Section 4. Arrival Procedures › 5-4-11. Radar Approaches

    runway. They are told to anticipate glidepath interception approximately 10 to 30 seconds before it occurs and when to start descent. The published Decision Altitude (DA) will be given only if the pilot requests it. If the aircraft is observed ... least once each mile. If an aircraft is observed by the controller to proceed outside of specified safety zone limits in azimuth and/or elevation and continue to operate outside these prescribed limits, the pilot will be directed to execute…

  • Chapter 5. Air Traffic Procedures › Section 3. En Route Procedures › 5-3-8. Holding

    When an aircraft is 3 minutes or less from a clearance limit and a clearance beyond the fix has not been received, the pilot is expected to start a speed reduction so that the aircraft will cross the fix, initially ... soon as possible and, whenever possible, at least 5 minutes before the aircraft reaches the clearance limit. f. Pilots should report to ATC the time and altitude/flight level at which the aircraft reaches the clearance limit and report leaving…

  • Chapter 7: Aircraft Systems › Electrical System

    charge in the battery. Electrical energy stored in a battery provides a source of electrical power for starting the engine and a limited supply of electrical power for use in the event the alternator or generator fails. Most DC generators ... aircraft have receptacles to which an external ground power unit (GPU) may be connected to provide electrical energy for starting. These are very useful, especially during cold weather starting. Follow the manufacturer’s recommendations for engine starting using…