0
Q
Vs1
A
52 KIAS
1
Q
Vso
A
49 KIAS
2
Q
Vr
A
59 KIAS
3
Q
Vy takeoff
A
66/ KIAS
4
Q
Cruise Climb
A
73
5
Q
Vfe Takeoff
A
108
6
Q
Vfe Landing
A
91
7
Q
Va (<2284)
A
94 KIAS
8
Q
Va
A
108
9
Q
Vno
A
129 KIAS
10
Q
Vne
A
178 KIAS
11
Q
Vref
A
71
12
Q
Vglide
A
73/76
13
Q
Maximum Demonstrated Crosswind
A
20 KTS
14
Q
MTOW
A
2535
15
Q
MLDW
A
2407
16
Q
Maximum Baggage
A
66 LBS
17
Q
Total Fuel Capacity (useable+unusable)
A
51 Gallons
18
Q
Total Useable Fuel
A
50 Gallons
19
Q
Total Unusable Fuel
A
1 Gal
20
Q
Maximum Gas Tank Differential
A
8 gallons
21
Q
Maximum Oil Capacity
A
8 QTS
22
Q
Minimum Oil Capacity
A
4 QTS
23
Q
Engine Designator
A
Lycoming IO-360-M1-A
24
Number of Cylinders
4 cylinders
25
Fuel injected or carburated?
Fuel Injected
26
Total HP @ Max RPM
180 HP @ 2700 RPM
27
Propeller Diameter
74 inches
28
Propeller Pitch Angles
13.5-30.0
29
Flap Settings
Cruise (0), Takeoff (20), Landing (42)
30
Minimum Autopilot Operating Speed
70 KIAS
31
Minimum Autopliot Altitude
200 FT AGL on Approach, 800 FT all other operations
32
Maximum Autopilot Airspeed
165 KIAS
33
Starter Limitations
Maximum 10 Seconds cranking, followed by 20 Seconds Cooling. Maximum attempts- 6 followed by 30 minute cooling period
34
Magneto Check Limitations
Maximum Drop 175, Maximum Differential 50
35
Maximum RPM Drop on Prop Check
500 RPM
36
Takeoff RPM Limitations
2680 +\- 20 RPM
37
Oil temperature range
165-220 F
38
CHT Temperature Range
150-400 (435 in fast cruise) (500 never exceeded)
39
Maximum CHT cooling speed
50F per Minute
40
Minimum windmilling prop speed
70 KIAS
41
Vx
66
Diamond 40
flashcards
Decks in class (2)
# Cards
