Cessna

Front 1

Vso

Back 1

Stall speed, landing config (40 knots)

Front 2

Vsi/Vs1

Back 2

Stall speed, clean config (48 knots)

Front 3

Vx

Back 3

Best angle of climb (62 knots)

Front 4

Vy

Back 4

Best rate of climb (74 knots)

Front 5

Vr

Back 5

Normal takeoff speed (roll at 55 knots)

Front 6

Vg

Back 6

Best glide speed (68 knots)

Front 7

Vfe

Back 7

Flaps 20-30 (85 knots), flaps 10 (110 knots)

Front 8

Va

Back 8

Maneuvering speed (1900 lbs-90 knots) (2500 lbs-105 knots)

Front 9

Vno

Back 9

Maximum structural cruising speed (yellow 129 knots)

Front 10

Vne

Back 10

Never exceed speed (red 163 knots)

Front 11

Cruise Checklist

Back 11

Throttled for Airspeed

Engine Instruments

Landing light

Mixture lean as required

Front 12

Clean Flow

Back 12

Fuel Selector Both

Mixture Enriched

No Flaps

Front 13

Landing Flow

Back 13

Fuel Selector Both

Mixture Enriched

Flaps Full Within White Arc

Front 14

S Model and R Model with Cessna 72-01 Engine

Back 14

Produces 180 HP @ 2700 RPM

Front 15

S Model and R Model mod Propeller

Back 15

McCauley 76 inch

Front 16

Vacuum operating range

Back 16

4.5-5.5 inches of mercury

Front 17

Landing gear

Back 17

The landing gear is it fixed, tricycle type gear consisting of tubular string steel providing shock absorption for the main wheels, and an oleo (air/oil) strut providing shock absorption on the nose wheel. The nose wheel can turn 10° each side of center.

Front 18

Pitot tube provides static pressure to the

Back 18

Altimeter, Vertical Speed Indicator, and Airspeed Indicator

Front 19

Stall horn

Back 19

A pneumatic type stall system that consists of an inlet on the left wing. The horn sounds 5 to 10 knots above the stall.

Front 20

Identify the range of usable fuel.

Back 20

53 is usable. K-P is 38 gallons.

Front 21

What type of flaps does the C-172 have?

Back 21

Single slot type flaps driven electrically by a motor in the right wing.

Front 22

Describe the ignition system.

Back 22

Dual magneto system, two purposes are to provide improved engine performance and redundancy. They are self contained, engine driven unit that supplies electrical current to the spark plugs and is completely independent of the electrical system.

Front 23

Engine Failure during takeoff

Back 23

1. Throttle Idle

2. Apply Brakes

Front 24

Engine failure immediately after takeoff

Back 24

70 KIAS Flaps Up

65 KIAS Flaps 10-Full

Front 25

Engine failure during flight (restart)

Back 25

1. Airspeed 68 KIAS

2. Fuel Shutoff ON (push full in)

3. Fuel Selector Both

4. Fuel Pump ON

5. Mixture Rich

Front 26

Fire during start

Back 26

1. Continue Cranking

If not started

2. Throttle Full

3. Mixture Off (pull out)

4. Magnetos Start (continue cranking)

5. Fuel Shutoff Off (pull out)

6. Fuel Pump Off

7. Magnetos Off

8. Standby and Master Off

Front 27

Engine Fire in flight

Back 27

1. Mixture Off

2. Fuel Shutoff Off (pull out)

3. Fuel Pump Off

4. Master Off

Front 28

Electrical fire in flight

Back 28

1. Standby and Master Off

2. Vents/Cabin Air/Heat Closed

3. Fire Extinguisher Activate

Front 29

Cabin fire

Back 29

1. Standby and Master Off

2. Vents/Cabin Air/Heat Closed

3. Fire Extinguisher Activate

Front 30

Wing fire

Back 30

All Lights and Pitot Heat Off

Front 31

Describe the electrical system on your aircraft.

Back 31

Electrical energy is provided by 28 volt, direct current system powered by an engine driven 60 amp alternator and a 24 volt battery.