Approved Data; Airspeed Indicator System Calibration - DG Flugzeugbau DG-1000 Flight Manual

5.2 Approved data

5.2.1

Airspeed indicator system calibration

IAS = indicated airspeed
CAS = calibrated airspeed
Caution: The airspeed indicator is to be connected to the static ports and pitot
probe in the fuselage nose.
270
250
230
210
190
170
150
130
110
90
70
70 90
Issued: March 2002
Flight manual DG-1000S
110 130 150
max. upper tolerance
max. lower tolerance
measurement
IAS=CAS
170 190 210 230 250 270
IAS [km/h]
LBA app.
5.3