Airspeed System Calibration; Stall Speeds - Rotax CESSNA 150 Manual

Converted with kit
NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10

AIRSPEED SYSTEM CALIBRATION

Airspeed, IAS, indicated air speed deviates from the calibrated airspeed CAS as follows (mph)
Landing flaps up
IAS 50 60
CAS 53 60
Landing flaps full
IAS 40 50
CAS 40 50
Fig. 5 - 2 – Air speed indicator

STALL SPEEDS

Engine on idle, IAS is an approximate.
Weight 726 kg.
.
Flap position
Flaps up
Flaps 20°
Flaps 40°
Fig. 5 - 3 –Stall speeds
Airplane Flight
Manual Cessna F150L
70 80 90 100
69 78 87
60 70 80 90
61 72 83 94
Bank angle
0°
mph mph mph
IAS CAS
54 55
49 49
48 48
110 120
97 108 118
100
105
20°
mph mph
IAS CAS IAS
56 57 63
50 51 56
49 49 54
Nr. 160
Page:
Revision 1 – Change A
130 140
128 138
40° 60°
mph mph mph
CAS IAS CAS
63 80
56 70
54 66
5-6b
78
70
67