Scanner Course #2
Aircraft Familiarization – –
Aircraft Controls Aircraft Instruments
Weight and Balance
Minnesota Wing Aircrew Training: Tasks P-2016, P-2017, P-2018
Scanner Course #2
Aircraft Structure and Controls
Scanner Course #2
Aircraft Familiarization
Why do I need to know this stuff anyway? Terminology Structure Control surfaces Instrumentation Limitations
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The Airplane
CAP typically uses C172 and C182.
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Aircraft Terminology Right Aileron
Vertical Stabilizer Empennage Right Flap
Rudder
Trim Tabs Right Wing
Elevator Left Flap Left Aileron
Propeller
Nose Gear
Main Gear
Landing Light Left Wing
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Ailerons provide roll control
Right wing goes down
Right Aileron UP
Left Aileron DOWN
Left wing goes up
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Elevators provide pitch control
Center of Gravity
Center of Gravity
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The rudder controls yaw
CENTER of GRAVITY RIGHT RUDDER PEDAL
LEFT RUDDER PEDAL
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Trim tabs neutralize control pressures
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Aircraft Instruments
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Instrument Panel
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Flight Instruments
Magnetic Compass – – – –
Primarily a backup Doesn’t require any power Installation problems Bank angles and speed changes can cause a compass to show the wrong heading
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Flight Instruments
Heading Indicator (Directional Gyro) – – – – –
Gyro-driven heading indicator Quick response to turns Stable indications Electrical or vacuum-driven Will drift, requires periodic realignment
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Flight Instruments
Altimeter –
–
Usually set to show pressure altitude above Mean Sea Level (MSL) Accurate altitude is dependent on the altimeter setting.
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Flight Instruments
Turn Coordinator –
–
–
Really two instruments Miniature aircraft shows turn rate only does not show bank angle Inclinometer shows quality of turn Coordinated, slip, skid
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Flight Instruments
Attitude Indicator – –
Provides a horizon reference Hash marks indicate bank angle
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Flight Instruments
Airspeed –
– –
Knots or MPH Colored markings Shows aircraft performance
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Flight Instruments
Vertical Speed – – –
Climb or descent rate Has a lag due to design Use with altimeter
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Engine Instruments
Tachometer – –
Markings — green arc Indicates power
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Other Engine Instruments
Gauges – – – – –
Fuel (accurate at empty) Oil Temperature and Pressure Vacuum and Generator Exhaust Gas Temperature Instruments vary from aircraft to aircraft
Scanner Course #2 Comm, VOR and DME radios Navigation/Communication Radio
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Primary and Standby Frequencies
DME
Comm 1 Communications
Comm 2
Nav 1 Navigation
Nav 2
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Comm Antennas
– –
Normally mounted on top One for each radio
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Nav Antennas
– –
“Cat whisker” style One for each nav
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Navigation Instruments VOR
VHF Omnidirectional Range (VOR-DME, VORTAC) –
ADF
Indicates direction to/from ground transmitter relative to magnetic North
Automatic Direction Finder (NDB) –
Direction toward ground transmitter relative to airplane nose
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Other Antennas Loop (directional) ADF
Marker Beacon
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UHF Antenna
Blade type (may be spike) Transponder & DME [If mounted up front, may interfere with DF]
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Global Positioning System
Satellite based navigation –
–
Apollo GX55 Can provide search pattern course guidance and lat and long of target
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GPS Antenna
GPS
Line of sight, so mounted at the very top Comm antennas can interfere with the weak signals, so they are tested for interference
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Direction Finding Receiver
Used for electronic ELT searches
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CAP FM Transceiver
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Audio Panel
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Transponder
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Static “wicks”
– –
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Mitigate buildup of static electricity (interferes with comm) Wings, elevators, vertical stabilizer Take care when walking around
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Weight and Balance and Operations
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Weight and Balance Lift
Weight
Force from horizontal tail surface
The wings generate a limited amount of lift Maximum weight for an aircraft is set by the manufacturer Pitch stability is affected by the location of the center of gravity The pilot computes weight and balance and controls it by loading the aircraft correctly -If incorrectly loaded: – the pilot may not be able to raise the nose during take off or – the aircraft may be unstable and difficult or impossible to control in the air
Scanner Course #2
Weight and Balance
Excessive weight adversely impacts performance: – – –
Out of Forward C.G. limits can cause: – –
Longer take off and landing distance Reduced climb performance Reduced ability to withstand turbulence and wind shear forces Reduced up-elevator authority (ability to raise the nose) Can eliminate the ability to flare for landing
Out of Rear C.G. limits can cause: – –
Reduced down-elevator authority (ability to lower the nose) Can make stall recovery difficult or impossible
Scanner Course #2
Mission Aircraft Operations A CAPF84 or CAPF104 must be completed Altimeter settings will be from a source within 50 NM or the closest source available and updated hourly. Airspeed will be no lower than 1.3 times aircraft stall at zero flaps and 30 degrees of bank.
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Mission Aircraft Operations Search altitudes are limited to no lower than 500 feet above the surface (except for counter drug vessel identification). Search aircraft on missions over water must plan to be over a suitable airfield with at least 90 minutes of fuel on board at normal cruise speed.