BOMBARDIER LEARJET 35, 36 MODIFICATIONS (290)

Introduction of ADS-B Out as per CS-ACNS

Automatic Dependent Surveillance-Broadcast (ADS-B) is a system broadcasting, without the need for action from the pilot or any request from ATC, that provides an enhanced set of aircraft surveillance data to Air Traffic Management (and potentially to other airplanes)

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Installation of a Bendix/King (Honeywell) ART 2000 Radar Transceiver/Antenna interfaced...

Installation of a Bendix/King (Honeywell) ART 2000 Radar Transceiver/Antenna interfaced with a Bendix/King (Honeywell) KMD-850 Multi-Function Display.

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Installation of a Bendix/King (Honeywell) ART 2000 Radar Transceiver/Antenna interfaced...

Installation of a Bendix/King (Honeywell) ART 2000 Radar Transceiver/Antenna interfaced with a Bendix/King (Honeywell) KMD-850 multi-function display.

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Installation of Collins TCAS-94 TCAS II System

The Collins TCAS-94 Traffic Alert Collision Avoidance System provides the enhanced situational awareness required for operation in the ever increasing air traffic environment.

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Installation of an Allied Signal (Bendix/King) CAS 66A TCAS System

Like our TCAS II/ACAS II systems which account for more than 10,000 installations flying on 325 aircraft types, the compact CAS 66A works by interrogating the ATC transponders of other aircraft in flight. The CAS 66A then processes this information and displays the positions of surrounding aircraft to the pilot.

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Installation of an AlliedSignal Avionics TCAS I CAS 66A Traffic...

Installation of an AlliedSignal Avionics TCAS I CAS 66A Traffic and Collision Avoidance System.

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Install Sundstrand Mark VII Ground Proximity/Windshear Warning System

The EGPWS is a Terrain Awareness and Alerting system providing terrain alerting and display functions with additional features.

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Installation of an Allied Signal CAS 67A Traffic Alert &...

Installation of an Allied Signal CAS 67A Traffic Alert & Collision Avoidance (TCAS II). (STC ST00515WI) Certification Basis Limitations - Duncan Aviation Inc. Document List No. 10048800 Revision B dated March 20, 1997, or later approved revisions.- DuncanAviation Inc. AFM Supplement Document No. 40169100 dated August 9, 2004, or later approved revision. Conditions 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.

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Installation of Universal Avionics TAWS Certification Basis Limitations Duncan Aviation...

Installation of Universal Avionics TAWS Certification Basis Limitations Duncan Aviation Document List 10055100 Revision A dated December 14, 2000 or later approved revision.Duncan Aviation AFM Supplement 40010400 dated December 18, 2000 or later approved revision. Conditions None

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