The Altitude Preselect System APS4A is intended to be used as an interface between Air Data Display or Primary Flight Display (e. g. Thommen AD30- and AD32-Family, Garmin G600, Aspen 1000) with alerter function and a variety of existing autopilot systems to supply altitude preselect- and hold-function. The system is mainly designed for retrofit installation and consists of a small lightweight interface box and an optional altitude preselect indicator/switch. [mehr]
The Fuel Quantity Indication System is a fuel quantity and low fuel level sensing and indicating system.
The system components are:
The HCU200 unit is a control unit for a DC-load like a pitot/static tube heater to prevent aircrew from misleading information of non-working heaters or excessive current draw conditions for a va-riety of aircraft.
The HCU200 is consisting of:
Designed for either single or dual FMS/GPS installation
The LPV-Converter resolves the arising problem with the LPV/VNAV-approach that appears, when an aircraft is equipped with an EFIS system (e.g. Honeywell SPZ5000 in Cessna 525 or Thales system in EC135/145) and a SBAS capable (WAAS/EGNOS) FMS/GPS with an ARINC429 interface. [mehr]