• Located at the instrument panel.

• Illuminating when the engine manifested a metal in the oil system.

• Connected to a chip detector plug in the oil drain sump.

When the fuel drops to 9 gallons in either fuel tank, the sensing unit will illuminate the applicable low fuel warning light.

• Both pilots are required a headset to have communication to each other.

• Press to talk are integrated at each control yoke for press to talk function

Pressing toggle switch fore transmit outside the aircraft and aft for the intercom

• Allows selection of fuel from various tanks.

• It contains three positions: LEFT, RIGHT, and BOTH.

Used to cut-off fuel from the tank to the engine.

Strainer removes moisture and other sediments that might be in the system. Since these contaminants are heavier than aviation fuel, they settle in a sump at the bottom of the strainer assembly.

It is driven directly by the engine and its flow rate depends on engine RPM.

• It controls the amount of intake air admitted into the intake manifold and meters the proportionate amount of fuel to the fuel manifold valve.

• Located at the top of the engine assembly fore of fuel manifold valve

The injector nozzle ( one per cylinder ) are air bleed type fuel nozzles which spray fuel directly into intake port of the cylinder. Located at the top of the cylinder beside the spark plugs

IO – 360DB21B

I - _____________

IO – 360DB21B

O - _____________

IO – 360DB21B

360 - _____________

IO – 360DB21B

DB - _____________

IO – 360DB21B

21 - _____________

Located at the front of the engine opposite of the propeller governor and controlled by mixture control.

The injector nozzles are “air bleed” type fuel nozzles which spray fuel directly into the intake port of the cylinders.

The _________ on the IO-360 is a six-tube, air distribution system mounted atop the engine.

Produces oil pressure to increase blade pitch

Instrument that indicates the speed of the crankshaft of a reciprocating engine. Connected to the engine by a flexible drive shaft and geared to the engine so that when the engine turns, so does the shaft.

Indicates the pressure of the air in the engine’s induction manifold. Indication of the power develop in the engine (the higher the pressure of fuel air mixture in the engine, the more power it can produce)

Indicates the approximate gallons per hour being metered to the engine.

A bourdon tube type or electrically operated indicator. The gauge is connected by a single wire to sending unit located in the engine oil passage above the oil cooler.

The most important instrument used by the pilot to perceive the health of an engine

The _________ is connected to a thermocouple on the engine cylinder. All cylinder has provision of the installation

Differential pressure gauge that compares ram air pressure (picked up by pitot on the leading edge of the left wing) and static pressure (from the static ports)

Used to indicate the height of the aircraft above a predetermined level, such as sea level or terrain beneath the aircraft.

Indicates the actual climb or descent rate of the aircraft. Calibrated in feet per minute

Give the pilot pitch and roll information. Operated by a vacuum system

Shows the correct execution of a turn while banking the aircraft and indicates movement about the vertical axis of the aircraft.

The turn-and-slip indicator is actually two separate devices built into the same instrument housing (a turn indicator pointer and slip indicator ball)

Furnishes the pilot a constant directional reference with relation to the north pole of the earth. Synchronized with standby compass

Measures and indicates the alternator output voltage of the electrical system

Part of Vacuum system that indicate inches of mercury (in Hg). Green markings indicate 4.6 to 5.4 inches of mercury which is the operating range for the gyro instrument. 5.3 in Hg is desirable at full power.

[AC ELECTRICAL SYSTEM]

-Use for cold weather starting or when lengthy electrical maintenance

[AC ELECTRICAL SYSTEM]

gear driven, flange mounted on the engine & is rated at 28 volts, 38 ampere

[AC ELECTRICAL SYSTEM]

Regulates the alternator field current

[AC ELECTRICAL SYSTEM]

Open the over voltage warning light when the voltage reading is 32 Volts and simultaneously shuts off the alternator

[AC ELECTRICAL SYSTEM]

Illuminate anytime electrical system voltage exceeds approximately 32 volts.

[AC ELECTRICAL SYSTEM]

Indicates a charging or discharging condition.