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