The flashcards below were created by user
cdavies87
on FreezingBlue Flashcards.
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VS0 (Stall speed in LDG configuration, kts)
34
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VS1 (Stall speed in CRUISE configuration, kts)
42
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VG (Rotate Speed, kts)
44
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Lift-off airspeed (kts)
52
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Normal landing final approach airspeed (kts)
60
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No-Flap landing final approach airspeed (kts)
65
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VX (flaps T/O, kts) (Best angle of climb)
60
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VX (flaps CRUISE, kts) (Best angle of climb)
65
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Vy (flaps T/O, kts) (Best rate of climb)
66
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Vy (flaps CRUISE, kts) (Best rate of climb)
70
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Positive limit load factor (flaps CRUISE)
+4.4
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Negative limit load factor (flaps CRUISE)
-2.2
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Positive limit load factor (flaps T/O or LDG)
+2.0
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Negative limit load factor (flaps T/O or LDG)
0
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Voltmeter lower limit red arc (volts)
8-11
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Voltmeter caution range yellow arc (volts)
11-12.5
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Voltmeter upper limit red line (volts)
16.1
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Approved fuel grade
100LL
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Fuel tank capacity (US gal.)
24.5
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Max. ramp weight (lbs)
1770
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Max. landing weight (lbs)
1764
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Forward CG limit (at or below 1653 lbs)
7.95
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Forward CG limit (1764 lbs)
8.07
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Aft CG limit (1764 lbs)
12.16
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Aft CG limit (at or below 1653 lbs)
12.48
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Max weight in baggage compartment (lbs)
44
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Min. rpm during engine runup idle check
975
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Min. permissible static rpm (full throttle runup)
2000
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Tachometer normal operating range (rpm)
700-2800
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Min. rpm drop during magneto check
25
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Max. rpm drop during magneto check
150
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Max. rpm drop difference between magnetos
50
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Max. permissible continuous bhp
125
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Min. oil pressure (psi)
10
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Max. oil pressure for full power operation if OAT <0°C (psi)
70
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Min. oil temperature (°F)
75
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Min. oil temp for full power operation if oil pressure norm (°F)
100
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Max. oil temperature (°F)
240
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Fuel pressure lower limit red line (psi)
3.5
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Fuel pressure upper limit red line (psi)
16.5
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Max. time for CHT below 300°F in descent (minutes)
5
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Min. CHT (°F) takeoff & descent
240
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CHT normal operating range (°F)
300-420
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CHT caution range (°F)
420-460
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Max. OAT (°C) operation w/ full winterization kit
0
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Max. OAT (°C) operation w/ partial winterization kit
12.5
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Max. crosswind component student dual (kts)
15
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Maximum airplane structural temperature (°C)
55
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Propeller approx. minimum ground clearance (inches)
10
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Main landing gear tire pressure (psi)
33
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Nose gear tire pressure (psi)
26
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Min. OAT (°C) cabin heat not req for 10 min. before T/O
-20
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