The LPV Converter was developed for all Cessna Citation Jets which are either equipped with the legacy Honeywell SPZ5000 System or with Proline21 without the capability to display glideslope information on the Electronic Flight Instrument System (EFIS) (EHSI/PFD) and consequently where LPV approaches are not possible.

Installation of an Aircell High Speed Internet System (AHSI) with Wireless Local Area Network (WLAN) and Axxess II Iridium Phone System in Cessna 525A airplanes and activation of Wireless Local Area Network on Cessna 525B airplanes.

Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I).

Installation of Rockwell Collins ProLine 21 Communication, Navigation, and Surveillance (CNS) System.

Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.

This module is extremely versatile and has numerous STCs in fixed and rotor wing aircraft. This system is lightweight, compact and fits smaller aircraft, yet has critical care capabilities for larger aircraft as well. 

Installation Air Ambulance Conversion Cessna 525, 525a, 525B and 525C

Spectrum Aeromed is recognized as a world leader in creating customized and durable, highly functional air medical transport equipment that complies with aviation regulations. All engineering and design of our air ambulance life support systems comes from working hand-in-hand with air medical personnel worldwide.

WX-950 Stormscope installation. Certification Basis CS 23 Amdt: 40The Certification Basis for the original product remains applicable tothis certificate/ approval.Derogation to latest amendment (Part 21A.101):Do not materially contribute to safety.The certificated noise and/ or emissions levels of th (...) Limitations - Master Data List, Doc. No. 2016-6-16, Rev. IR, dated 12.12.2012;- AFMS, Doc. No. 2016 6-8, Rev. A, dated 25.10.2012;-ICA, Doc. No. 2016-6-10, Rev. IR, dated 27.11.2012;or laterrevisions of the above listed documents approved by EASA. Conditions None. -

The existing Honeywell CAS-66A will be upgraded to a CAS-67A system to meet the ACAS II standard as per latest regulation requirements.

Installation of dual GTX 330D Mode S Transponder systems.Installation of dual GTX 330D Mode S Transponder systems. Certification Basis Limitations - EASA approved Engineering Order, Doc. No. 2019974-EO-05, Issue 4, or later approved Issue- for ELS-mode operation of XPDR system:EASA approved Airplane Flight Manual Supplement, Doc. No. 2019974-AM- 05A, Issue 1, or later approved Issue- i (...) Conditions 1. According to Engineering Order 2019974- EO-05, Issue 41. According to Engineering Order 2019974-EO-05, Issue 4