VAL Avionics NAV 2000 Installationsanleitung Seite 135

  • Herunterladen
  • Zu meinen Handbüchern hinzufügen
  • Drucken
  • Seite
    / 401
  • Inhaltsverzeichnis
  • FEHLERBEHEBUNG
  • LESEZEICHEN
  • Bewertet. / 5. Basierend auf Kundenbewertungen
Seitenansicht 134
SV-EMS-220/221 Installation and Configuration
SkyView System Installation Guide - Revision R 7-27
Pin
EMS 37-pin Harness
Wire Color
Sensor (with Dynon part number if
applicable)
35
Green
Not connected
36
Blue or Unwired
CAN High from 912 iS ECU
37
Green or Unwired
CAN Low from 912 iS ECU
The 912 iS ECU provides the following information to SkyView via a computerized CAN bus
interface:
Engine RPM (tachometer)
Oil Temperature
Oil Pressure
Coolant Temperature
Lane A Bus Voltage
Lane B Bus Voltage
EGT 1-4
Manifold Pressure
Fuel Flow
Engine Time
Additionally, the SV-EMS-221 provides an RPM out signal that can be sent to the aircraft's
propeller controller (if so equipped). The RPM out signal is nominally at 0 volts and steps to 12
volts for 0.1 milliseconds. The RPM out signal pulses once per engine revolution. The installer
must verify compatibility between the RPM out signal and the RPM input requirements of the
aircraft's propeller controller. The following diagram details all of the connections that need to
be made between the Rotax 912 iS and the SV-EMS-221, as well as the optional RPM signal
output to a propeller controller:
Figure 30 - SV-EMS-221 / Rotax 912 iS Connections
Seitenansicht 134
1 2 ... 130 131 132 133 134 135 136 137 138 139 140 ... 400 401

Kommentare zu diesen Handbüchern

Keine Kommentare