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V
S0
(Stall speed in LDG configuration)
34
V
S1
(Stall speed in CRUISE configuration)
42
V
R
(Rotate Speed)
44
Lift-off airspeed
52
Normal landing final approach airspeed
60
No-Flap landing final approach airspeed
65
V
X
(flaps T/O) (Best angle of climb)
60
V
X
(flaps CRUISE) (Best angle of climb)
65
V
Y
(flaps T/O) (Best rate of climb)
66
V
Y
(flaps CRUISE) (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. idle mixture rise leaned to peak (runup/shutdown)
50
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
70
Min. oil temperature (°F)
75
Min. oil temp for full power operation if oil pressure norm
100°F
Max. oil temperature (°F)
240
Fuel pressure lower limit red line (psi)
3.5
Fuel pressure upper limit red line (psi)
32.5
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. CHT (°F)
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
Author
Anonymous
ID
10892
Card Set
More IFS Ops Limits
Description
IFS Ops Limits
Updated
2010-03-17T03:01:40Z
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