CP.II.C.K3

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 7-30
  Chapter 7: Aircraft Systems › Electrical System

  Associated electrical wiring Engine-driven alternators or generators supply electric current to the electrical system. They also maintain a sufficient electrical charge in the battery. Electrical energy stored in a battery provides a source of electrical power for starting ... engine and a limited supply of electrical power for use in the event the alternator or generator fails. Most DC generators do not produce a sufficient amount of electrical current at low engine rpm to operate the entire electrical system…

• Pilot's Handbook of Aeronautical Knowledgep. 7-15
  Chapter 7: Aircraft Systems › Ignition System

  With RIGHT or LEFT selected, only the associated magneto is activated. The system operates on both magnetos when BOTH is selected. A malfunctioning ignition system can be identified during the pretakeoff check by observing the decrease in rpm that occurs ... engine stops running when switched to one magneto or if the rpm drop exceeds the allowable limit, do not fly the aircraft until the problem is corrected. The cause could be fouled plugs, broken or shorted wires between the magneto…

• Pilot's Handbook of Aeronautical Knowledgep. 7-18
  Chapter 7: Aircraft Systems › Starting System

  starter engages the aircraft flywheel, rotating the engine at a speed that allows the engine to start and maintain operation. Electrical power for starting is usually supplied by an onboard battery, but can also be supplied by external power through ... starter switch draw current from the main bus bar, but the starter will not operate until the starting solenoid is energized by the starter switch being turned to the “start” position. When the starter switch is released from the “start…

• Pilot's Handbook of Aeronautical Knowledgep. 7-23
  Chapter 7: Aircraft Systems › Turbine Engines › Foreign Object Damage (FOD)

  deflectors, may also be 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 ... much fuel entering the combustion chamber or insufficient turbine rpm. Any time an engine has a hot start, refer to the AFM/POH or an appropriate maintenance manual for inspection requirements. If the engine fails to accelerate to the proper speed…

• Pilot's Handbook of Aeronautical Knowledgep. 1-16
  Chapter 1: Introduction To Flying › Pilot Certifications

  depending on the type of certificates sought. [Figure 1-20] Each type of pilot’s certificate has privileges and limitations that are inherent within the certificate itself. However, other privileges and limitations may be applicable based on the aircraft type ... operation being conducted, and the type of certificate. For example, a certain certificate may have privileges and limitations under 14 CFR part 61 and part 91. Figure 1-20. Front side (top) and back side (bottom) of an airman certificate…

• Pilot's Handbook of Aeronautical Knowledgep. 9-3
  Chapter 9: Flight Manuals and Other Documents › Powerplant

  Powerplant The Powerplant Limitations portion describes operating limitations on an aircraft’s reciprocating or turbine engine(s). These include limitations for takeoff power, maximum continuous power, and maximum normal operating power, which is the maximum power the engine can produce ... this area are the minimum and maximum oil and fuel pressures, oil and fuel grades, and propeller operating limits. [Figure 9-3] All reciprocating-engine powered aircraft must have a revolutions per minute (rpm) indicator for each engine. Aircraft equipped…