ADS-B Out Primus II Solution

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ADS-B Out Solution for Primus II Equipped Aircraft

details:

STC Referenced:ST00361BO - Installation of Honeywell Primus II (XS-852) ADS-B Out System (FAA)
STC Holder:Pro Star Aviation, LLC
Approval Date:July 2016
Amended Date:October 2017
Reissue Date:October 2017

 

Pro Star Aviation teamed up with Honeywell Aerospace to create a complete STC solution for Primus II equipped aircraft that is both; compliant with current FAA & EASA ADS-B Out mandates, DO-206B standards, and offers owners & operators options in equipment upgrades and system configurations.

 
 
honeywell_logo_2016

APPLICABLE AIRCRAFT:

STC AML addresses the most popular business and corporate aircraft known to be equipped with a Primus II system:

Beechcraft BAe.125 Series
800A | 800B | 1000A | 1000B

Challenger 601

Citation 550 | 560 | 560XL | 650 | 750

Dornier 328-100 | 328-300

Embraer 145 Series | 135 Series

Global Express

Hawker 800 | 800XP | 1000

Learjet 40 | 45

STC Package contents:

Installation instructions
Flight Manual amendments
Supplemental paperwork
FAA Approved ADS-B Certification for the entire system
Support from the original engineers behind the STC's design & development

STC SPECIFICS:

STC solution is:

  • Specific to Primus II equipped aircraft
  • Compliant with 2020 ADS-B Mandates & DO-260B Standards (required for flight above FL18)

STC solution provides:

  • Four (4) configuration choices for interfacing GPS's to RCZ unit(s)
  • Flexibility when interfacing GPS units with a WAAS GPS sensor
  • Replacement of RM-850's with RM-855's for ADS-B Out compliance
  • Supports GPS's that provide SA (selective availability) to meet DO-260B compliance standards.
    • GPS's with "Selective Availability Aware" (GPS SA) capable sensors provide Mode S Transponders with position, velocity, altitude, figure of merit, and integrity limit data.
  • Upgrade of existing RCZ-8xx units

STC prerequisites:

  • An existing FAA Approved installation of one of the following Position Sources:
    • KGS-200 GNS (single)
    • HG201 MK II GNSSU (single/dual)
    • UNS-1( )w GNSS (single/dual)
  • An existing RCZ-8XXX ICU
  • An existing RM-855
  • An existing Transponder antenna of class (need one):
    • TSO-C166b
    • TSO-C154c A1S
    • TSO-C154c B1S

Equipment Locations:

RMU GPS ICU TRANSPONDER ANTENNA
(Remote Monitoring Unit) (Global Positioning System) (Integrated Communications Unit) (Class Specific)
RM-855 KGS-200 GNSS RCZ-8XX(L)(M) TSO-C166
HG2021 MK II GNSSU TSO-C154c A1S
UNS-1( )w GNSS TSO-154c B1S
 

installation requirements:

Minimal Equipment: Honeywell Strap Bus Kit model #IK-837 or #IK-839

Wiring modifications between the GNSSU/KGS-200 and the RCZ units (at a minimum) will be required to complete the ADS-B out installation.

When upgrading to a GNSSU -GD06 or KGS-200 an active antenna will also be required

Active antenna's integrate...

 

BROCHURES:

ADS-B Out
Primus II Solution

STC

STC AML