Airplane Flight
Manual Cessna F150L
Nr. 160
Converted with kit
NS402S with ROTAX 912 S3 and
Page:
5-6b
HOFFMANN HO-V352F/170FQ+10
Revision 1
– Change A
AIRSPEED SYSTEM CALIBRATION
Airspeed, IAS, indicated air speed deviates from the calibrated airspeed CAS as follows (mph)
Landing flaps up
IAS
CAS
50
53
60
60
70
69
80
78
90
87
100
97
110
108
120
118
130
128
140
138
Landing flaps full
IAS
CAS
40
40
50
50
60
61
70
72
80
83
90
94
100
105
Fig. 5 - 2
– Air speed indicator
STALL SPEEDS
Engine on idle, IAS is an approximate.
Weight 726 kg.
.
Flap position
Bank angle
0°
20°
40°
60°
mph
IAS
mph
CAS
mph
IAS
mph
CAS
mph
IAS
mph
CAS
mph
IAS
mph
CAS
Flaps up
Flaps 20°
Flaps 40°
54
49
48
55
49
48
56
50
49
57
51
49
63
56
54
63
56
54
80
70
66
78
70
67
Fig. 5 - 3
–Stall speeds
Summary of Contents for CESSNA 150
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