Private Pilot

Front 1

Oil

Back 1

6-8 quarts never leave with less than 6

Front 2

Propeller

Back 2

Sensenich 2 blade, fixed pitch, metal propeller. 76in max RPM 2700 RPM.

Front 3

Landing gear

Back 3

Fixed tricycle style gear with oleo (air/oil) struts. Nose wheel is controlled by the rudder pedals that turns 20 degrees to each side

Front 4

Brakes

Back 4

Hydraulically actuated disc breaks on the main gear. Toe brakes and parking brakes have separate breaking cylinders

Front 5

Flaps

Back 5

Manually operated flap system with settings of 0, 10, 25, an 40 degrees and are spring loaded to return to 0 degrees

Front 6

Pitot static

Back 6

Located under the left wing and is used for airspeed, altimeter, vertical speed indicator. Alternate source is located under left side of instrument panel

Front 7

Fuel system

Back 7

One engine driven and one electric fuel pump electric is used for all takeoffs and landings and when switching tanks

Front 8

Fuel management

Back 8

Switch tanks every 30 minutes to avoid uneven weight distribution

Front 9

Electrical system

Back 9

The archer has a 28 volt dc electrical system and a 24 volt lead acid battery. Electricity is supplied by a 70 amp engine driven alternator that maintains a constant 28 volt output

Front 10

Garmin g500 glass cockpit

Back 10

Primary flight display, multi-function flight display,attitude heading reference system, air data computer, magnetometer, temperature prob, dual Garmin g430 gps.

Front 11

VSO

Back 11

45 kts

Hint 11

Stall speed in landing config

Front 12

VS

Back 12

50

Hint 12

Stall speed with no flaps

Front 13

VR

Back 13

60 kts

Hint 13

Rotation speed

Front 14

VX

Back 14

64 kts

Hint 14

Best angle of climb

Front 15

VY

Back 15

76

Hint 15

Best rate of climb

Front 16

VG

Back 16

76

Hint 16

Best glide at max weight

Front 17

VFE

Back 17

102

Hint 17

Maximum flap extension speed

Front 18

VNO

Back 18

125

Hint 18

Max structural cruising speed

Front 19

VNE

Back 19

154

Hint 19

Never exceed speed

Front 20

VA at 2,550 LBS

Back 20

113

Front 21

VA at 1,634 LBS

Back 21

89 KTS

Front 22

Engine

Back 22

Lycoming 4 cylinder 0-360 engine. 180 horsepower at 2700 RPM horizontally opposed pistons facing each other. Air cooled normally aspirated. Direct driven

Hint 22

L

H

A

N

D

S

Front 23

P.A.V.E

Back 23

Pilot Aircraft Environment External pressure

Front 24

I.M.S.A.F.E.E

Back 24

Illnesses, Medication, Stress, Alcohol, Fatigue, Eaten, Emotion

Front 25

Alcohol

Back 25

8 hr bottle to throttle

0.04 BAC

Not under influence

Front 26

E,C,A,R,R,O,W

Back 26

External data Plate, Compass Deviation Card, Airworthiness Certificate, Registration, Radio station License, Operating handbook, Weight and balance.

Front 27

A,V,1,A,T,E,E,S

Back 27

Annual-12 months, VOR equipment, 100 HR Inspection, Altimeter, Transponder, ELT Battery, ELT 12 months, Static and Encoder.,

Front 28

A,T,O,M,A,T,O,F,L,A,M,E,S

Back 28

Anti collision light system, Tachometer, Oil pressure gauge, Manifold pressure, Airspeed indicator, Temp gauge, Oil temp gauge, Fuel quantity indicator, Landing gear position indicator, Altimeter, Magnetic compass, Emergency Locator Transmitter, Safety belts.

Front 29

F,L,A,P,S

Back 29

Fuses, Landing Light, Anti collision light, Position indicator lights, Source of electricity.

Front 30

N,W,K,R,A,F,T

Back 30

Notams, Weather, known delays, Runway length, Alternate, Fuel 30min day 45 min night, Take off/ landing distance.

Front 31

Airspeed diaphram

Back 31

Pitot ram air

Front 32

Airspeed diaphram

Back 32

Pitot ram air

Front 33

Airspeed case

Back 33

Static air

Front 34

Air speed

Back 34

Dynamic air pressue

Front 35

Dynamic air pressure

Back 35

Difference between static and actual air pressure (ram air)

Front 36

Error’s for airspeed

Back 36

Pitot block, pitot and drain block, static block.

Front 37

Pitot block

Back 37

Airspeed to 0 due to diaphragm deflation

Front 38

Pitot and drain

Back 38

Airspeed will Chang opposite of how it should due to changes in static pressure.

Front 39

Static block

Back 39

Normal but incorrect readings compare to other static instruments

Front 40

What is the Aneroid waffer

Back 40

Sealed to a pressure of 29.92.

Front 41

Altimeter pitot static system

Back 41

Compared between static air and aneroid waffer

Front 42

Altimeter static error

Back 42

Altimeter will lock up and not change

Front 43

Alternate static source used

Back 43

Altimeter increases and then normalizes

Front 44

Ailerons

Back 44

Differential freeze type (not equal degree of change on each side)

Front 45

Pilotage

Back 45

Flying by landmarks

Front 46

Dead reckoning

Back 46

Using solely fuel time and compass

Front 47

Properties of combustion

Back 47

Suck, squeeze, bang, blow

Front 48

Suck

Back 48

Air is pulled into the cylinder via the carburetor

Front 49

Squeeze

Back 49

Crank shaft causes the piston to squeeze the fuel air mixture

Front 50

Bang

Back 50

Fuel is combusted by two spark plugs for an even burn ran by two magnetos

Front 51

Blow

Back 51

Exhaust products are pushed out of the cylinder.

Front 52

VFR minimums for class G more than 1200 AGL at or above 10,000 MSL

Back 52

5 stature miles, 1000 feet above 1000 feet below 1 statute mile horizontal

Front 53

VFR MINIMUM Class G more than 1200 AGL less than 10,000 MSL (Day)

Back 53

1 stature mike vis, 500 feet below 1000 feet above 2000 feet horizontal

Front 54

VFR MINIMUM Class G more than 1200 AGL less than 10,000 MSL (Night)

Back 54

500 below, 1000 feet above, 2000 feet horizontal

Front 55

VFR minimums class G 1200 feet or less AGL (night)

Back 55

500 below, 1000 above, 2000 horizontal.

Front 56

VFR minimums class G 1200 feet or less AGL (night)

Back 56

500 below, 1000 above, 2000 horizontal.

Front 57

VFR minimums class G 1200 feet or less AGL (day)

Back 57

1SM vis, clear of clouds

Front 58

Class E at or above 10,000 MSL

Back 58

5sm vis 1000 below, 1000 above, 1SM horizontal

Front 59

Class E VFR minimums less than 10,000 MSL

Back 59

3SM vis 500 feet below, 1000 feet above, 2000 feet horizontal

Front 60

Class D VFR minimums

Back 60

3SM vis 500 feet below, 1000 feet above, 2000 feet horizontal

Front 61

Class C VFR minimums

Back 61

3SM vis 500 feet below, 1000 feet above, 2000 feet horizontal

Front 62

Class B VFR minimums

Back 62

3SM vis, Clear of clouds

Front 63

VDMONA

Back 63

Variation deviation magnetic dip oscillation northerly turning error acceleration deceleration errors

Front 64

VDMONA

Back 64

Variation deviation magnetic dip oscillation northerly turning error acceleration deceleration errors

Front 65

UNOS

Back 65

Undershoot north undershoot south

Front 66

ANDS

Back 66

Acceleration north deceleration south

Front 67

Types of NOTAMS

Back 67

FDC POINTER MILITARY SAA DISTANT