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67 Cards in this Set
- Front
- Back
- 3rd side (hint)
Oil |
6-8 quarts never leave with less than 6 |
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Propeller |
Sensenich 2 blade, fixed pitch, metal propeller. 76in max RPM 2700 RPM. |
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Landing gear |
Fixed tricycle style gear with oleo (air/oil) struts. Nose wheel is controlled by the rudder pedals that turns 20 degrees to each side |
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Brakes |
Hydraulically actuated disc breaks on the main gear. Toe brakes and parking brakes have separate breaking cylinders |
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Flaps |
Manually operated flap system with settings of 0, 10, 25, an 40 degrees and are spring loaded to return to 0 degrees |
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Pitot static |
Located under the left wing and is used for airspeed, altimeter, vertical speed indicator. Alternate source is located under left side of instrument panel |
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Fuel system |
One engine driven and one electric fuel pump electric is used for all takeoffs and landings and when switching tanks |
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Fuel management |
Switch tanks every 30 minutes to avoid uneven weight distribution |
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Electrical system |
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 |
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Garmin g500 glass cockpit |
Primary flight display, multi-function flight display,attitude heading reference system, air data computer, magnetometer, temperature prob, dual Garmin g430 gps. |
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VSO |
45 kts |
Stall speed in landing config |
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VS |
50 |
Stall speed with no flaps |
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VR |
60 kts |
Rotation speed |
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VX |
64 kts |
Best angle of climb |
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VY |
76 |
Best rate of climb |
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VG |
76 |
Best glide at max weight |
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VFE |
102 |
Maximum flap extension speed |
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VNO |
125 |
Max structural cruising speed |
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VNE |
154 |
Never exceed speed |
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VA at 2,550 LBS |
113 |
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VA at 1,634 LBS |
89 KTS |
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Engine |
Lycoming 4 cylinder 0-360 engine. 180 horsepower at 2700 RPM horizontally opposed pistons facing each other. Air cooled normally aspirated. Direct driven |
L H A N D S |
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P.A.V.E |
Pilot Aircraft Environment External pressure |
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I.M.S.A.F.E.E |
Illnesses, Medication, Stress, Alcohol, Fatigue, Eaten, Emotion |
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Alcohol |
8 hr bottle to throttle 0.04 BAC Not under influence |
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E,C,A,R,R,O,W |
External data Plate, Compass Deviation Card, Airworthiness Certificate, Registration, Radio station License, Operating handbook, Weight and balance. |
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A,V,1,A,T,E,E,S |
Annual-12 months, VOR equipment, 100 HR Inspection, Altimeter, Transponder, ELT Battery, ELT 12 months, Static and Encoder., |
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A,T,O,M,A,T,O,F,L,A,M,E,S |
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. |
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F,L,A,P,S |
Fuses, Landing Light, Anti collision light, Position indicator lights, Source of electricity. |
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N,W,K,R,A,F,T |
Notams, Weather, known delays, Runway length, Alternate, Fuel 30min day 45 min night, Take off/ landing distance.
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Airspeed diaphram |
Pitot ram air |
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Airspeed diaphram |
Pitot ram air |
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Airspeed case |
Static air |
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Air speed |
Dynamic air pressue |
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Dynamic air pressure |
Difference between static and actual air pressure (ram air) |
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Error’s for airspeed |
Pitot block, pitot and drain block, static block. |
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Pitot block |
Airspeed to 0 due to diaphragm deflation |
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Pitot and drain |
Airspeed will Chang opposite of how it should due to changes in static pressure. |
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Static block |
Normal but incorrect readings compare to other static instruments |
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What is the Aneroid waffer |
Sealed to a pressure of 29.92. |
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Altimeter pitot static system |
Compared between static air and aneroid waffer |
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Altimeter static error |
Altimeter will lock up and not change |
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Alternate static source used |
Altimeter increases and then normalizes |
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Ailerons |
Differential freeze type (not equal degree of change on each side) |
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Pilotage |
Flying by landmarks |
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Dead reckoning |
Using solely fuel time and compass |
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Properties of combustion |
Suck, squeeze, bang, blow |
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Suck |
Air is pulled into the cylinder via the carburetor |
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Squeeze |
Crank shaft causes the piston to squeeze the fuel air mixture |
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Bang |
Fuel is combusted by two spark plugs for an even burn ran by two magnetos |
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Blow |
Exhaust products are pushed out of the cylinder. |
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VFR minimums for class G more than 1200 AGL at or above 10,000 MSL |
5 stature miles, 1000 feet above 1000 feet below 1 statute mile horizontal |
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VFR MINIMUM Class G more than 1200 AGL less than 10,000 MSL (Day) |
1 stature mike vis, 500 feet below 1000 feet above 2000 feet horizontal |
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VFR MINIMUM Class G more than 1200 AGL less than 10,000 MSL (Night) |
500 below, 1000 feet above, 2000 feet horizontal |
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VFR minimums class G 1200 feet or less AGL (night) |
500 below, 1000 above, 2000 horizontal. |
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VFR minimums class G 1200 feet or less AGL (night) |
500 below, 1000 above, 2000 horizontal. |
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VFR minimums class G 1200 feet or less AGL (day) |
1SM vis, clear of clouds |
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Class E at or above 10,000 MSL |
5sm vis 1000 below, 1000 above, 1SM horizontal |
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Class E VFR minimums less than 10,000 MSL |
3SM vis 500 feet below, 1000 feet above, 2000 feet horizontal |
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Class D VFR minimums |
3SM vis 500 feet below, 1000 feet above, 2000 feet horizontal |
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Class C VFR minimums |
3SM vis 500 feet below, 1000 feet above, 2000 feet horizontal |
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Class B VFR minimums |
3SM vis, Clear of clouds |
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VDMONA |
Variation deviation magnetic dip oscillation northerly turning error acceleration deceleration errors |
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VDMONA |
Variation deviation magnetic dip oscillation northerly turning error acceleration deceleration errors |
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UNOS |
Undershoot north undershoot south |
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ANDS |
Acceleration north deceleration south |
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Types of NOTAMS |
FDC POINTER MILITARY SAA DISTANT |
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