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.

The ProLine 21 Radio System will include dual Com's, Nav's, Marker Beacons, Glideslope's, ADF's, DME's, TXP's and Radio Tuning Units.

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.

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 a Honeywell KMD 850 System and installationof a TCAS ISky

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

Installation of a Honeywell KMD 850 System and installationof a TCAS ISky. Certification Basis Limitations - Flight Manual Supplement 2016515-AM-01, Issue 3, or laterEASAapproved Revisions.- Flight Manual Supplement 2016516-AM-01, Issue 3, or later EASAapproved Revisions. Conditions 1. This STC is approved only for the product configurationas definedin the approved design data referred to in the paragraph Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.