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54 Cards in this Set
- Front
- Back
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V_S0 (Stall speed in LDG configuration)
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34
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V_S1 (Stall speed in CRUISE configuration)
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42
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V_R (Rotate Speed)
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44
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Lift-off airspeed
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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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V_X (flaps T/O) (Best angle of climb)
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60
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V_X (flaps CRUISE) (Best angle of climb)
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65
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V_Y (flaps T/O) (Best rate of climb)
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66
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V_Y (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 (lbs)
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1770
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Max. landing weight (lbs)
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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 (at or below 1653 lbs)
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12.48
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Max. weight in baggage compartment (lbs)
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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 (psi)
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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 temperature (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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Maximum airplane structural temperature (degrees C)
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55
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Propeller approx. minimum 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 req for 10 min. before T/O
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-20
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