Operation of Aircraft Systems

Written by Jack on May 31st, 2008
Objectives: To familiarize the student with the operation of various aircraft systems so that the student may have a better understanding of his aircraft.
Content:
  • Powerplant
    • Reciprocating engines
      • Radial, In-line, V-Type, Opposed
      • Liquid or air cooled
      • 4-stroke operating cycle (Intake, Compression, Power, Exhaust)
  • Propeller
    • Angle of incidence – for prop, angle formed by chord line and reference plane containing prop hub
    • Fixed Pitch Propeller (2 types)
    • Climb Propeller
    • Cruise Propeller
    • Tachometer as indicator of engine power
    • Lower density, less power
    • Controllable Pitch Propeller
    • Constant Speed Propeller
      • Acts as fixed pitch prop when pitch stops contacted
      • Manifold pressure as indicator of engine power (MAP)
        • For given RPM there is Manifold pressure that shouldn’t be exceeded (accordance w/ mfcr)
  • Induction Systems (2 types)
    • Carburetor system
      • Float-type and pressure-type
        • Icing most likely @ temps < 70?F (21?C) relative humidity > 80%
        • Carb Heat in float-type
      • Fuel injection system
        • Impact icing
    • Superchargers
      • Increase service ceiling
      • Sea level engine (sea level supercharger)
      • Altitude Engine
      • Turbosuperchargers
        • Critical altitude
        • Turbine and compressor
        • Waste gate
        • Intercooler
        • Overboost
    • Excessively rich mixture causes carbon buildup/spark plug fouling
    • Excessively lean mixture causes detonation
  • Ignition System
      • Dual ignition systems
      • Combustion
      • Detonation
      • Preignition
  • Fuel Systems (figures 5-15, 5-17 PHAN)
    • Gravity-fed
    • Fuel-pump, primer, tanks, gauges, selectors, strainers, sumps, and drains
    • Fuel Grades
    • Refueling procedures
  • Starting System
  • Oil Systems
    • Recip. Engines use wet sump or dry sump oil system
  • Engine Cooling Systems
    • Cowl flaps
    • Cylinder Head Temperature Guage (CHT)
  • Exhaust Systems
    • Exhaust Gas Temperature (EGT) and leaning
  • Electrical Systems
    • 14- or 28-volt direct current system
    • Ground Power Unit (GPU) receptacle
    • Alternator/Generator
    • Ammeter/Loadmeter
    • Voltage regulator
  • Hydraulic Systems
    • Single- or double-acting servos
  • Landing Gear
    • Tricycle (Nosewheel)
      • Steerable or Castering
    • Conventional (Tailwheel)
      • Fixed and Retractable
  • Brakes
  • Autopilot

See aircraft POH

See Pilot’s Handbook of Aeronautical Knowledge, C. 5

See PHAN C. 5 Figures

Completion Standards: The lesson is complete when the instructor determines that the student has adequate knowledge of the aircraft systems by giving an oral or written exam.
 

1 Comments so far ↓

  1. Chris Bryant says:

    This is my first time on your web site (very nice & thanks). I am a recently minted CFI, CFII in central Oregon and need to train a student for a High Performance endorsement. This is my first time giving this training, and was looking for a comprehensive lesson plan specifically for this(so I dont miss anything). I still have not found one. Can you help? I appreciate your resource site and any help if possible. Thanks again. Chris Bryant

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