Cirrus SR20 Handbuch Seite 171

Abschnitt 7
Beschreibung des Flugzeugs und der Systeme Inhaltsverzeichnis
Variometer (VSI) ........................................................................ 7-60
Höhenmesser ............................................................................ 7-61
Pitot-Heizungsschalter............................................................... 7-61
Pitot-Heizungslampe.................................................................. 7-61
Alternative Statikquelle .............................................................. 7-62
Vakuumsystem ............................................................................. 7-63
Unterdruckanzeige..................................................................... 7-63
Vakuum-Warnlampe .................................................................. 7-65
Zus. Vakuumwarnlampe ............................................................ 7-65
Attitude-Anzeiger ....................................................................... 7-65
Richtungs-Gyro .......................................................................... 7-66
Avionik und Navigation ................................................................. 7-67
Avionikschalter........................................................................... 7-68
Magnetkompass ........................................................................ 7-68
Wendekoordinator ..................................................................... 7-69
Course Deviation Indicator ........................................................ 7-69
Horizontal Situation Indicator (Optional) .................................... 7-70
Autopilot..................................................................................... 7-72
Audio-System ............................................................................ 7-74
Multifunktionsanzeige ................................................................ 7-75
GPS-Navigation ......................................................................... 7-77
Kommunikations-Transceiver (COM) ........................................ 7-78
Navigations-Empfänger (Nav) ................................................... 7-79
Transponder .............................................................................. 7-80
Emergency Locator Transmitter ................................................ 7-80
Betriebsstundenzähler ............................................................... 7-82
Digitaluhr.................................................................................... 7-82
Cirrus Flugzeugfallschirmsystem (CAPS) ..................................... 7-84
Systembeschreibung ................................................................. 7-84
Aktivierungsgriff ......................................................................... 7-85
Aktivierungsmerkmale ............................................................... 7-86
P/N 21561-002
Ursprüngliche
Cirrus Design
SR22
7-3