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54 Cards in this Set
- Front
- Back
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Vs0 (stall spd in ldg configuration)
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34
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Vs1 (stall spd in cruise configuration)
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42
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Vr (rotate spd)
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44
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Lift-off air speed
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52
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Normal landing final approach airspeed
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60
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No-flap landing final approach airspeed
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65
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Vx (flaps T/O) (best angle of climb)
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60
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Vx (flaps CRUISE) (best angle of climb)
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65
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Vy (flaps T/O) (best rate of climb)
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66
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Vy (flaps CRUISE) (best rate of climb)
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70
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Positive limit load factor (flaps CRUISE)
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+4.4
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Negative limit load factor (flaps CRUISE)
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-2.2
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Positive limit load factor (flaps T/O or LDG)
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+2.0
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Negative limit load factor (flaps T/O or LDG)
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-0
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Voltmeter lower limit red arc (volts)
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8-11
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Voltmeter caution range yellow arc (volts)
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11-12.5
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Voltmeter upper limit red line (volts)
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16.1
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Approved fuel grade
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100LL
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Fuel tank capacity (US gal)
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24.5
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Max ramp weight
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1770
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Max landing weight
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1764
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Forward CG limit (at or below 1653 lbs)
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7.95
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Forward CG limit (1764 lbs)
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8.07
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Aft CG limit (1764 lbs)
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12.16
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Aft CG limit (1653 lbs)
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12.48
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Max weight in baggage compartment
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44
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Min idle mixture rise leaned to peak (runup/shutdown)
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50
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Min rpm during engine runup idle check
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975
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Min permissible static rpm (full throttle runup)
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2000
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Tachometer normal operating range (rpm)
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700-2800
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Min rpm drop during magneto check
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25
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Max rpm drop during magneto check
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150
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Max rpm drop difference between magnetos
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50
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Max permissible continuous bhp
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125
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Min oil pressure
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10
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Max oil pressure for full power operation if OAT < 0 degrees C
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70
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Min oil temp (degrees F)
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75
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Min oil temp for full power operation if oil pressure norm
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100 degrees F
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Max oil temperature (degrees F)
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240
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Fuel pressure lower limit red line (psi)
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3.5
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Fuel pressure upper limit red line (Psi)
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32.5
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Max time for CHT below 300 degrees F in descent (minutes)
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5
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Min CHT (degrees F) takeoff & descent
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240
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CHT normal operating range (degrees F)
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300-420
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CHT caution range (degrees F)
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420-460
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Max CHT (degrees F)
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460
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Max OAT (degrees C) operation w/ full winterization kit
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0
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Max OAT (degrees C) operation w/ partial winterization kit
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12.5
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Max crosswind component student dual (kts)
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15
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Max airplane structural temp (degrees C)
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55
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Prop approx min ground clearance (inches)
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10
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Main landing gear tire pressure (psi)
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33
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Nose gear tire pressure (psi)
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26
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Min OAT (degrees C) cabin heat not required for 10 min before T/O
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-20
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