“AERO” Sp. z o.o.
SECTION 5
AT-3 R100
PERFORMANCE
SEPTEMBER, 2004
Page 5-3
AEROPLANE FLIGHT MANUAL
5.2. Approved data
5.2.1. Calibration of the airspeed indicator system
The diagram is based on test flight data.
CAS = IAS +
δδδδ
V
δ
V – aerodynamic correction
CLIMB, LEVEL FLIGHT, DESCENT
WING FLAPS: retracted, for take-off and for landing
[mph]
149
137
124
99
112
87
75
62
50
[mph]
62
75
87
99
112
124
137
149
[kts]
43
54
65
76
86
97
108
118
130
130
118
108
86
97
76
65
54
43
[kts]