Electrical System
Fuel system
Flight controls
Engine/power plant
Avionics
100
DC capacity of the 172 electrical system

28 volts

100

the usable fuel capacity of the C172S

53 gallons

100

The primary flight controls

Ailerons, Elevator, rudder

100
The Cessna 172S has this specific type of engine

Lycoming IO-360-L2A

100

This takes information from the pitot static system and displays it on the PFD

ADC

200

The number of electrical busses

6

200

The C172S pulls fuel from this area of the fuel tanks

The side

200

the type of ailerons on the C172S

Differential Friese type

200

The amount of spark plugs on the Cessna 172S

8

200

The magnetometer is located in this wing

Left

300

These items are located on the Essential bus

PECANS:

PFD,EIS,COMM1,ADC/AHRS, STBY ind lights

300

The three parts of the system that fuel sumps are pulling from under the cowling

Fuel Selector, Fuel reservoir, Fuel strainer

300

The differential ailerons assist in preventing this during a turn and a C172S

adverse yaw

300

The camshaft is gear driven by this in the engine

Crankshaft

300

This information processed and displayed by the GRS 77 and GMU 44

Attitude, Heading, rate of turn, slip/skid (AHRS)

400

This connects the battery, external power, alternator and ammeter to multiple relays that power the buses

J Box or power distribution module

400

The fuel flows through this directly before entering the strainer

Fuel shutoff valve

400

the type of trim tab on a C172

Servo

400

The rotational speed of the camshaft is this amount less than the crankshaft

1/2

400

The Cessna 172S nav 3 models with the G1000 and incorporated autopilot use this type of autopilot system on our FF and FM tail numbers

GFC 700/two axis

500

The voltage at which the main battery will switch to the standby battery

20 volts

500

The fuel return line from the engine to the reservoir tank has this on it to assist with preventing reverse flow and maintaining proper system pressure

Check valve

500

the type flaps on a C172S

Slotted with fowler characteristics

500

this gear is responsible for engaging the starter motor's pinion gear with the engine's ring gear on the flywheel during engine start-up

the bendix gear

500

These two LRU's are responsible for feeding information from the avionics system to the PFD/MFD in normal operations

The two GIS 63's or Garmin integrated avionics units