WT-9 Dynamic Club S FLIGHT MANUAL Section 5 Page 5-1
SECTION 5
PERFORMANCE
Page
5.1 Introduction 5-1
5.2 Approved data 5-1
5.2.1 Airspeed indicator system calibration 5-1
5.2.2 Stall speed 5-2
5.2.3 Take-off performance 5-2
5.2.4 Landing distance 5-2
5.2.5 Climb performance 5-2
5.3 Additional information 5-3
5.3.1 Endurance 5-3
5.3.2 Balked landing climb 5-4
5.3.3 Effect on flight performance and characteristics 5-4
5.3.4 Demonstrated crosswind performance 5-4
5.3.5 Noise data 5-4
5.1 Introduction
Section 5 provides approved data for airspeed calibration, stall speed and take-off
performance and non-approved additional information. The data in the charts has
been computed for condition of the standard atmosphere from actual flight tests with
the aeroplane at maximum take-off weight and engine in good condition and using
average piloting techniques.
5.2 Approved data
5.2.1 Airspeed indicator system calibration
IAS ( km/h ) 50 65 70 80 90 100
110
120
130
140
160
CAS ( km/h ) 65 76 80 87 92 100
110
118
127
136
156
IAS ( km/h ) 180 200 220 240 260 280
CAS ( km/h ) 175 195 215 233 252 272
IAS = indicated airspeed
CAS = calibrated airspeed
Date: 1.12.2001 „Appr“
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