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Chapter 2 – Airplane Systems
Section A Airplanes
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Major parts of an airplane
Fuselage Wing Landing Gear Empennage Powerplant
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Fuselage Open or enclosed truss Stressed skin structure Materials used
Monocoque Semi-monocoque
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Wings Monoplanes Biplanes Ailerons Flaps
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Empennage Vertical stabilizer Horizontal stabilizer Stabilator Rudder
Elevator Stabilator
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Trim devices Trim tabs Anti-servo tab
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Landing gear Main wheels Third wheel Tailwheel Nosewheel
Conventional gear Nosewheel Tricycle gear
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Landing gear Fixed gear Retractable gear Seaplanes Landing gear struts
Floats Amphibians Landing gear struts Spring steel, bungee cord, oleo
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Brakes Toe brakes on rudder pedals Parking brake
Equal or differential braking Steering Parking brake Limit steering with brakes – use rudder pedals then brakes only if needed Don’t ride brakes – overheat Keep heels on floor
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Powerplant Engine Propeller Firewall Cowling
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Pilot’s Operating Handbook (POH)
Airplane Flight Manual (AFM) Pilots Information Manual (PIM)
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Contents of POH, AFM, PIM General Limitations Emergency procedures
Where else can these be found? Emergency procedures Abnormal procedures Normal procedures Performance
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Contents of POH, AFM, PIM Weight and balance
Airplane and systems description Handling, service and maintenance Supplements Safety and operational tips
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Chapter 2 – Airplane Systems
Section B The Powerplant and Related Systems
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Powerplant – Reciprocating
Radial Horizontally opposed
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Powerplant – turbine Turbojet Turboprop
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Reciprocating Engines
Pistons Crankshaft Connecting rods Valves
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Four-stroke operating cycle
Intake Compression Power Exhaust
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Similar for turbine
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Induction systems Air + fuel sent for combustion
Intake port – filter and alternate Controls Throttle Mixture Propeller control
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Carburetor
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Leaning the mixture Higher altitudes – air less dense
Mixture control in full rich position creates excessively rich mixture Reduce amount of fuel by leaning so fuel-to-air ratio remains constant Remember to enrich mixture when descending
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Carburetor ice
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Indications of Carburetor Ice
Fixed pitch propeller – loss of R.P.M. Constant speed propeller – loss of manifold pressure
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Carburetor heat
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Indications when Carb heat is used
Initially – drop in R.P.M. (hot air is less dense) Followed by gradual increase in R.P.M. as ice melts For constant speed prop – indications are reflected in manifold pressure
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Fuel injection systems
Less susceptible to icing More precise Use less fuel More horsepower More expensive Sensitive to contaminants More complex starting procedures – esp. when engine is hot
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Fuel injection system
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Supercharging - Turbocharging
Increases power of engine Sea level performance at higher altitudes Supercharger – engine driven compressor Turbocharger – compressor driven by exhaust Usually fuel injected More finicky
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Turbocharger
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Ignition Two magnetos Spark plugs Wires Ignition switch
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Ignition Two magnetos Two spark plugs in each cylinder
Redundancy = safety Better combustion of fuel/air mixture
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Ignition switch Off R L Both Start
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Abnormal combustion Detonation – explosion instead of smooth burning of fuel Engine overheat Improper grade of fuel Preignition Fuel/air mixture ignites before normal timed ignition Residual hot spot Engine roughness
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Fuel system
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Fuel system Tanks Fuel quantity gauges Fuel selector valve
Fuel strainer
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Refuelling Ground wire Fuel grade – color coded
Refill after last flight of day – reduces condensation
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Oil systems
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Cooling systems
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High engine temps Loss of power High oil consumption
Possible engine damage Reduce temps Enrich the mixture Reduce rate of climb Increase airspeed Reduce power
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Engine cooling Cooling least effective Cowl flaps
Takeoff Go-around Low airspeed/high power Cowl flaps Cylinder head temperature gauge
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Exhaust system Vent burned gases overboard Heats cabin
Defrost windscreen
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Propellers
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Types of propellers Climb props Cruise props Fixed-pitch props
Constant-speed props Propeller control – r.p.m.
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Propellers Hazards
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Electrical systems Alternator Battery Ammeter Master switch
Circuit breakers
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