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3.1.1 Introduction
Chapter 3.1 contains procedures for normal aircraft operation.
3.1.2 Outfit and Equipment
It includes a basic set of instruments to monitor flight and power unit
parameters. Further equipment is offered as optional.
It holds the following as minimum: airspeed indicator, altimeter, vertical speed
indicator, slip indicator, engine RPM, CHT, oiltemperature, oil pressure.
II. INSTRUMENTS
Type Serial No.
Airspeed indicator
Altimeter
Vertical speed indicator
Slip indicator
Compass
Engine RPM
CHT
EGT
Water temperature
Oil temperature indicator
Oil pressure indicator
Charge indicator lamp
Intercom
Radio
Transponder
Engine ROTAX 912 UL-ULS
Propeller dm-prop dmp – 3/3 1700 mm
III. STORAGE BATTERY
Type
Voltage 12 V
Capacity 8 Ah