Weather Information
Operation of systems
Powerplant/ignition
Electrical System
Pitot System
100

the phone number for obtaining a weather brief

1-800-WX-BRIEF

100

The most simple of the four types of flaps

Plain

100

Self contained engine driven unit that supplies electrical current to the spark plugs

Magnetos

100

The amount of volts in our Direct current system

28

100

Measured at the flush port on the side of the airplane where air is not disturbed

Static Pressure

200

The radius a TAF covers around an airport

5 SM

200

The most common high lift devices used on aircraft

Flaps

200

Cylinder arrangement on the Lycoming IO-360

horizontally opposed

200

Monitors the performance of the electrical system

Ammeter

200

The instrument/instruments that the Pitot tube connects to

Airspeed indicator

300

The three types of airmets

Sierra, Tango, Zulu

300

frise-type ailerons combat this

Adverse yaw

300

The four stroke operating cycle

Intake, Compression, Power/Combustion, Exhaust

300

The acronym for the Essential bus and what is on it

PECANS (PFD, EIS, COMM 1, ADC/AHRS, NAV1, STDBY LIGHTS)

300

The error that occurs when the static port is blocked and pitot tube is open

Low in climb and high in descent (reverse altimeter)

400

The speed at which surface winds must exceed for a convective sigmet to be issued

50 knots

400

Type of tab that decreases excessive control forces

Balance tab

400

This part activates the magnetos during normal operation and sends power to the spark plugs

The Crankshaft

400

Feed directly into the Cross Feed Bus

Electrical Bus 1 & 2

400

The amount of gimbals in your attitude indicator

Two (pitch and roll)
500

The altitude range that mid level prognostic charts cover

10,000' MSL - FL450

500

This type of rudders acts as vertical and horizontal stabilizers

V-Tails

500

Increasing airspeed, enriching mixture, and/or reducing power helps lower this

Oil Temperature

500

Where the Alternator Control Unit is housed 

J-Box/Power Distribution Module

500

The spinning disk in the attitude indicator is oriented/mounted 

Horizontally

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