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Altitude Preselect System APS4A

Altitude Preselect System APS4A

Altitude Preselect System APS4A

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]

 

 

   Data Sheet APS4A

Fuel Quantity and Indication System FQIS

Fuel Quantity and Indication System FQIS

ACP 140mm
SCU

The Fuel Quantity Indication System is a fuel quantity and low fuel level sensing and indicating system.

 

The system components are:

  • Active Capacitance Probe (ACP) with mount
  • High Level Switch (HLS)
  • Low Level Switch (LLS)
  • Sensor Connecting Cables (SCC)
  • Signal Conditioner Unit (SCU)           [mehr] 

 

    

   Data Sheet FQIS

Heater Control Unit 200

Heater Control Unit 200

Heater Control Unit 200

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:

  • A solid state switch
  • A current monitor with flag output
  • Self test circuit
  • Redundant switch drive circuit       [mehr]

  

  

   Data Sheet HCU200

 

LPV Converter

LPV Converter

PLV Converter
LPV Converter

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] 

 

 

 

  

Präsentation LPV Converter