MODIFICATIONS OF Scandinavian Avionics Design ApS (132)

ADS-B OUT CS23 AIRCRAFTS

ADS-B out Replacement / Upgrade of the existing single or dual transponder to include ADS-B functionality according to Minimum Operational Performance Standards.
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UPGRADE TO ROCKWELL COLLINS TCAS VERSION 7.1 (ACAS II)

Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II)
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AVIATOR 350 SATELLITE COMMUNICATION SYSTEM

Aviator 350 Satellite Communication System With Wireless Local AreaNetwork (WLAN) Including 3G/4G Network Functionalityfor On Ground Only.
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INSTALLATION OF SANDEL AVIONICS ST3400H HTAWS.

Installation of Sandel Avionics ST3400H HTAWS.
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UNIVERSAL FMS UNS-1LW INSTALLATION

Universal FMS UNS-1Lw installation
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P-RNAV APPROVAL OF EXISTING DUAL HONEYWELL GNS-XLS FMS SYSTEM

P-RNAV approval of existing Dual Honeywell GNS-XLS FMS System
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IRIDIUM ANTENNA INSTALLATION ON BAE 125-1000A, BAE 125-1000B & HAWKER1000

Iridium Antenna Installation on BAe 125-1000A, BAe 125-1000B & Hawker1000
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SINGLE TRANSPONDER SYSTEM UPGRADE TO MODE S ELS/EHS/ADS-B

Single transponder system upgrade to MODE S ELS/EHS/ADS-B
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PROVISION FOR DUAL PORTABLE ELECTRONIC FLIGHT BAG (EFB) IN A...

Provision For Dual Portable Electronic Flight Bag (EFB) in a Boeing 757Series Aircraft
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ROCKWELL COLLINS TCAS VERSION 7.1 (ACAS II) UPGRADE OF PRIOR...

ROCKWELL COLLINS TCAS VERSION 7.1 (ACAS II) UPGRADE OF PRIOR EXISTINGTCAS VERSION 7.0 IN PART 25 AIRCRAFTS as per AML STC
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EFB TABLET DISPLAY MOUNT PROVISION

EFB Tablet Display Mount Provision
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REPLACEMENT OF EXISTING TCAS 7.0 BY TCAS 7.1 IN ACCORDANCE...

Replacement of existing TCAS 7.0 by TCAS 7.1 in accordance withScandinavia Avionics Design document 2097492 DOC, at issue 1, dated October 9, 2015;
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P-RNAV UPGRADE OF GNS430

P-RNAV Upgrade of GNS430
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TCAS 7.1 (ACAS II) UPGRADE OF PRIOR EXISTING TCAS 7.0...

TCAS 7.1 (ACAS II) UPGRADE OF PRIOR EXISTING TCAS 7.0 IN PART 25AIRCRAFTS as per AML STC
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ATP AIRCRAFT - PROVISION OF DUAL PORTABLE ELECTRONIC FLIGHTBAG (EFB)THE...

ATP aircraft - Provision of dual portable Electronic FlightBag (EFB)The installation of the EFB provision comprises of2 window mountsconsisting of a swivel and a tablet holder, 2 EFB control panels, onedata integration centre and 2 C/B’sfor 28VDC to the EFB systems.
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ATR AIRCRAFT – INSTALLATION OF PROVISION FOR PORTABLE ELECTRONIC FLIGHTBAG...

ATR aircraft – Installation of provision for portable Electronic FlightBag (EFB) with wireless connectivity and optional surveillance camerasystemThe installation provides, as a baseline, the provision for Portable EFBTablet Displays in the cockpit on both pilot sides, including two windowmounts, on...
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UPGRADE FROM TCAS II VERSION 7.0 TO TCAS II VERSION...

Upgrade from TCAS II Version 7.0 to TCAS II Version 7.1 on Learjet24/25/31/35/36/55/60 Series Aircraft.
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INSTALLATION OF A FIVE PANEL UNIVERSAL EFI-890R EFIS TO BAESYSTEMS...

Installation of a Five Panel Universal EFI-890R EFIS to BAESystems ATPSerial Number 2033.
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UPGRADE FROM TCAS II VERSION 7.0 TO TCAS II VERSION...

Upgrade from TCAS II Version 7.0 to TCAS II Version 7.1 on CessnaCitation Aircraft
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INSTALLATION OF DUAL UNIVERSAL EFI-890R SYSTEM INTERFACED WITH DUALGARMIN GTN-750...

Installation of Dual Universal EFI-890R system interfaced with DualGarmin GTN-750 as primary navigation source (SAD Project No. 2086597)
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APPROVAL OF INSTALLATION OF A UNIVERSAL LPV MONITOR IN ACCORDANCE...

Approval of Installation of a Universal LPV Monitor in accordance withScandinavian Avionics Modification 2092019 Issue 1 dated 27 February2015.
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INSTALLATION OF UNIFIS 3000 FLIGHT INSPECTION SYSTEM.

Installation of UNIFIS 3000 Flight Inspection System.
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SOFTWARE UPGRADE FOR TCAS 7.1 COMPLIANCE ON:-,,ACSS T2CAS TCAS COMPUTER-,,HONEYWELL...

Software upgrade for TCAS 7.1 compliance on:-,,ACSS T2CAS TCAS computer-,,Honeywell TPA-100A TCAS computer
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INSTALLATION OF PROVISIONS FOR THE USE OF DUAL NAVAERO T.BAGC2...

Installation of provisions for the use of dual NAVAERO t.BagC2 EFBSystem on Embraer ERJ 170 aircraft.
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HONEYWELL FMZ-2000 FLIGHT MANAGEMENT SYSTEM.P-RNAV APPROVAL FOR EXISTING HONEYWELL FMZ-2000THIS...

Honeywell FMZ-2000 Flight Management System.P-RNAV approval for existing Honeywell FMZ-2000This REV. 1 was issued to correct a mistake in the name and address ofthe STC holder.
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UPGRADE OF EXISTING DUAL DIVERSITY TRANSPONDERS MODE S ELEMENTARY SURVEILLANCE...

Upgrade of existing dual diversity Transponders Mode S Elementary Surveillance (ELS) and Enhanced Surveillance (EHS)
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INSTALLATION OF GARMIN DUAL GTN-750 SYSTEMREVISION 1 ADDS THE TAWS...

Installation of Garmin Dual GTN-750 SystemRevision 1 adds the TAWS limitation to MSN 550-0672 and revokes theInitial Issue of the approval. Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations -Scandinavian Avionics, AFM Supplement GTN-750, ...
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RDR-1400C WEATHER RADAR INSTALLATION.

RDR-1400C Weather Radar Installation.
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INSTALLATION OF UNIVERSAL UNS FMS SYSTEM.THIS STC INSTALLS A NEW...

Installation of Universal UNS FMS System.This STC installs a new fully integrated navigation and flightmanagement system, identified as Universal UNS-1Lw, interfaced with EFISwithor without Advisory Vertical Guidance displayed on EHSI. Limitations: Master Document list, ref : 2080925-DOC issue 1, dated 19/07/2013;FMS Configuration with advisory VNAV : Aircraft Flight Manual Supplement, ref : 2080925-AM A Issue 2;FMS Configuration without advisory VNAV : Aircraft Flight Manual Supplement, ref ...
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THRANE & THRANE AVIATOR 350 SATELLITE COMMUNICATION SYSTEM WITH WIRELESSLOCAL...

THRANE & THRANE AVIATOR 350 SATELLITE COMMUNICATION SYSTEM WITH WIRELESSLOCAL AREA NETWORKDescription as per AssociatedTechnical Documentation Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations Master Documents List in document ref. 2081137 DOC issue 2,dated24/05/2013.Master ...
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INSTALLATION OF DUAL UNIVERSAL UNS-1E FMS IN LEARJET 35/35A/36/36AMAJOR CHANGE...

Installation of Dual Universal UNS-1E FMS in Learjet 35/35A/36/36AMajor Change to existing STC by additional certification for P- RNAVoperations by showing compliance with JAA TGL-10.Defined in Engineering Order 2032349-EO, issue 5, dated 18 April 20 (...) Certification Basis Certification Basis for the change: CS25, Amdt. 01.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original productareunchanged and remain applicable to ...
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STAND-ALONE AVIATOR 300 SATCOM SYSTEM INSTALLATION AS IDENTIFIED INENGINEERING ORDER...

Stand-alone AVIATOR 300 Satcom system installation as identified inEngineering Order 2072808-EO Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations Scandinavian Avionics, AFM Supplement 2072808-AM, issue 1 dated 06 July2012;Scandinavian Avionics, Continued Airworthiness 2072808-CA, Issue 2,dated ...
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INSTALLATION OF UNIVERSAL UNS-1LW FMS SYSTEM CERTIFICATION BASIS THE CERTIFICATION...

Installation of Universal UNS-1Lw FMS System Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations Scandinavian Avionics, AFM Supplement 2080144-AM A , issue 2 dated 23January 2013Scandinavian Avionics, Continued Airworthiness 2080144-CA A, Issue 1,dated 13 ...
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DUAL NAVAERO EFB CLASS 2 SYSTEM PROVISIONS LIMITATIONS: INSTALLATION MUST...

Dual NAVAERO EFB Class 2 System Provisions Limitations: Installation must be in accordance with Technical Order Doc. 2068119-TO,Issue 3.Operation must be in accordance with AFM Supplement Doc. 2068119-AM A,Issue 3 or Doc. 2068119-AM B,Issue 3.Maintenance must be in accordance with MM Supplement Doc. 2068 (...) Conditions: This STC does not constitute an Operational Approval. IndividualOperational Approvals, including the COTS equipment suitability, must beissued by the competent ...
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REPLACEMENT OF EXISTING SAFT NI-CAD. BATTERY WITH CONCORDE LEAD ACIDBATTERY...

Replacement of existing SAFT Ni-Cad. battery with Concorde lead acidbattery RG-350.Note: this STC is issued for the purpose of transfering STC No. 10028452from Airalpha A/S (DOA 21J.268) to new STC holder Scandinavian AvionicsDesign GmbH (DOA 21J.014)
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INSTALLATION OF L3 FA2100 DIGITAL FDR CERTIFICATION BASIS THE CERTIFICATION...

Installation of L3 FA2100 Digital FDR Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/or emissions levels of the original product areunchanged and remain applicable to this certificate/approval. Limitations According to Engineering Order No. 2068970- EO Issue 1To be operated in accordance with AFM-S Document No. 2068970-AMIssue 1To be maintained i.a.w. CA Document ...
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INSTALLATION OF A DUAL NAVAERO ELECTRONIC AND LOGGING DISPLAY SYSTEM.CHANGE...

Installation of a Dual navAero Electronic and logging display system.Change consisting in installing a dual portable Class 2 EFB's t.BagC2system Limitations: Not Applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and / or repair will introduce no adverse effectupon the airworthiness of the product.
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PROVISION FOR A DUAL NAVAERO T.BAGC2 CLASS 2 ELECTRONIC FLIGHT...

Provision for a Dual NAVAERO t.BagC2 Class 2 Electronic Flight BagSystem Limitations: None. Conditions: This STC for the provision for a dual Class 2 Electronic Flight Bag hasbeen assessed using the guidance in JAA Temporary Guidance Leaflet (TGL)No. 36. As part of that airworthiness assessment a limited evaluationwas made of the proposed EFB installation o
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UPGRADE OF ROCKWELL COLLINS TDR- 94D MODE S TRANSPONDER SYSTEM...

UPGRADE OF ROCKWELL COLLINS TDR- 94D MODE S TRANSPONDER SYSTEM FORENHANCED (EHS) SURVEILLANCE CAPABILITY. Certification Basis The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalCert base as TCDSJAR 25 Change 13Applicant elected to comply CS 25, Amdt. 5,AMC 20-13 a (...) Limitations To be installed in accordance with Engineering Order Doc. ID 2062013- EO,Issue 1 and ...
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GPS / NAVIGATION / COMMUNICATION, DUAL GARMIN GNS 430/530 AWINSTALLATIONTHE...

GPS / Navigation / Communication, Dual Garmin GNS 430/530 AWinstallationThe installation includes GPS antenna and single marker beacon receiver(KMR 675 or 51Z6) installation Certification Basis EASA TCDS IM.A.207The Certification Basis for the original product remains applicable tothis certificate/ approvalThe requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product are (...) Limitations ·,,Master Document List "2053445 DOC" Issue 3 from ...
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INSTALLATION OF COLLINS TCAS-94 SYSTEM WITH DUAL COLLINS TDR-94DTRANSPONDERS. LIMITATIONS:...

Installation of Collins TCAS-94 system with dual Collins TDR-94Dtransponders. Limitations: Transponder system NOT approved for ELS or EHS.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF ROCKWELL COLLINS TCAS-94 SYSTEM WITH SINGLE TDR-94DSYSTEM, AS...

Installation of Rockwell Collins TCAS-94 System with Single TDR-94DSystem, as per Scandinavian Avionics Engineering Order 2056096-EO issue1 dated 27th September 2010 or later EASA approved revisions. Limitations: None. Conditions: No additional EWIS ICAS tasks over those already identified by theoriginal TC Holder for the applicable aircraft models are needed asconsequence of the implementation of this STC.Prior to installation of this modification it must be determined thatthe ...
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INSTALLATION OF AN L3 DIGITAL FLIGHT DATA RECORDERREVISION 2 WAS...

Installation of an L3 Digital Flight Data RecorderRevision 2 was raised due to missing technical document references inRevision 1 Certification Basis EASA TCDS IM.A.207The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalJAR 25 at change 15The requirements for environmental protection and (...) Limitations - Master Documents List 2018778-01 DOC issue 8, dated 27 Sept. 2010- Engineering ...
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INSTALLATION OF AN INTERNATIONAL COMMUNICATIONS GROUP INC, ICS-100IRIDIUM SATELLITE TELEPHONE....

Installation of an International Communications Group Inc, ICS-100Iridium Satellite Telephone. Certification Basis The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalElect to Comply with CS-25 Am 4.The requirements for environmental protectionand the as (...) Limitations Installation in accordance with Scandinavian Avionics Design documentref 2056325 STC (STC Document List)Operation in accordance with Scandinavian Avionics Design document ref2056325-AM ...
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INSTALLATION OF PROVISIONS FOR THE USE OF DUAL NAVAERO ELECTRONIC...

Installation of provisions for the use of Dual navAero Electronic FlightBag Class 2 (EFB) System Limitations: Not Applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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SOFTWARE UPGRADE OF INSTALLED HONEYWELL GNS- XL OR GNX-XLS FMS...

Software upgrade of installed Honeywell GNS- XL or GNX-XLS FMS system forP-RNAV operation Certification Basis CS 25 amendment 4The certificated noise and/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval Limitations Engineering Order 2050529-EO Issue 2 from 27 November 2009List of STC documents 2050529 STC" issue 2 from 27 November 2009AFM Supplement 2050529-AM-A issue 2 from 27 November 2009 ...
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INSTALLATION OF HONEYWELL MST 67A DUAL MODE S XPDR TRANSPONDER....

Installation of Honeywell MST 67A Dual Mode S XPDR transponder. Certification Basis Certification Basis as per EASA TCDS IM.A.207 Limitations - Engineering Order 2052922-EO Issue 1 from 10 June 2009- List of Certification Documents 2052922-DOC Issue 2 from 28. August2009- AFM Supplements 2052922-AM A Issue 1 from 03 March 2009, 2052922-AM BIssue 1 from 03 March 2009, 2052922-AM C Issue 1 (...) Conditions None
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GARMIN GPS 400W/500W INSTALLATIONREVISION 1 SUPERSEDES THE PREVIOUS ISSUE OF...

GARMIN GPS 400W/500W installationRevision 1 supersedes the previous issue of this STC to delete the modelS550 from the applicability list for correction. Certification Basis Certification Basis as per EASA TCDS IM.A.207 Issue 2 from 5 March 2009 Limitations Master Document List "2054628 DOC" issue 1 from 17 August 2009Aircraft Flight Manual Supplement "2054628-AM" issue 1 from 11 August2009Instructions for Continued Airworthiness "2054628-CA" issue 1 from 11August ...
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INSTALLATION OF VARIOUS ENTERTAINMENT SYSTEMS ACC.: ENGINEERING ORDERDOC.: 2051195-EO COMPLIANCE...

Installation of various Entertainment Systems acc.: Engineering OrderDoc.: 2051195-EO Compliance Record Doc.: 2051195-COR Certification Basis CS-25 Limitations -AFM Supplement Doc.: 2051195-AM- Instructions for Continuous Airworthiness Doc.: 2051195-CA Conditions None
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INSTALLATION OF A DIGITAL FLIGHT DATA RECORDER. CERTIFICATION BASIS LIMITATIONS...

Installation of a Digital Flight Data Recorder. Certification Basis Limitations Installed in accordance with 2047003-EO Engineering Order Issue 2 or later approved revision.Operated in accordance with 2047003-AM AFM supplement Issue 1 or later approved revision.Maintained in accordance with 2047003-CA Instructions forContinued (...) Conditions 1. Prior to installation of this modification the installermust determine that the interrelationship between this modificationand any other previously installed modification will introduce ...
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DUAL UNIVERSAL UNS-1F FMS INSTALLATION. CERTIFICATION BASIS LIMITATIONS AS NOTED...

Dual Universal UNS-1F FMS Installation. Certification Basis Limitations As noted in Certification Document List 2051373 DOC, issue 1 (or later approved revisions). Conditions # Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. (...)
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INSTALLATION OF HONEYWELL MULTI-FUNCTION RADAR (MFRD) AND AN OPTIONAL HONEYWELL...

Installation of Honeywell Multi-Function Radar (MFRD) and an optional Honeywell Primus Radar System, if the existing radar is incompatible with the MFRD. Certification Basis Limitations Compliance Record 2036716-EO, Issue 2AFM Supplement 2036716-AM, Issue 2Instructions for Continued Airworthiness 2036716-CA, Issue 1or later approved versions. Conditions 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed ...
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UPGRADE OF EXISTING FMS UNIVERSAL UNS- 1CSP TO UNS-1CSP+ TO...

UPGRADE of existing FMS Universal UNS- 1Csp to UNS-1Csp+ to comply with P-RNAV requirements. Certification Basis Limitations 2045402-EO Engineering Order Issue 2 or later approved revision.2045402-AM AFM Supplement Issue 1 or later approved revision.2045402-CA Instructions for Continued Airworthiness Issue 1 or later approved revision. Conditions 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously ...
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MODE S ELEMENTARY AND ENHANCED UPGRADE OF EXISTING DUAL TRANSPONDER...

Mode S elementary and enhanced Upgrade of existing dual transponder system. Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install. Conditions: n/a
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MODE S ELS/EHS UPGRADE OF EXISTING TRANSPONDER SYSTEM. CERTIFICATION BASIS...

Mode S ELS/EHS Upgrade of existing transponder system. Certification Basis Limitations Engineering order 2042065-EO issue 2.AFMS 2042065-AM issue 1. Conditions Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.
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DUAL TDR-94D TRANSPONDER INSTALLATION UPGRADE TO PROVIDE BOTH ELEMENTARY AND...

Dual TDR-94D Transponder Installation Upgrade to provide both Elementary and Enhanced Surveillance Transponder Mode S Capabilities. Certification Basis Limitations See Scandinavian Avionics:# 2045142-STC (Certification Documents) issue 2, dated 04 Jun 08.# 2045142-EO Engineering Order issue 2, dated 11 Feb 08.# 2045142-AM-A AFM Supplement for Mode S Transponder Elementary Surveillance Capability, issu (...) Conditions Previous required aircraft configuration:# Aircraft equipped with Dual TDR-94D installation with Mode S ...
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INSTALLATION OF SEVERAL AVIONICS SYSTEM AS DEFINENED INTO ENGINEERING.ORDER NO....

Installation of several avionics system as definened into Engineering.Order No. 2042316 – EO issue 2
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INSTALLATION OF AVIONICS SYSTEM GARMIN GNS 480 / HONEYWELLKY-96A /...

Installation of Avionics System Garmin GNS 480 / HoneywellKY-96A / Garmin GTX 33 as defined in Engineering Order 2042580-EO .
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INSTALLATION OF HONEYWELL ART2100/KMD850 WEATHER RADAR SYSTEM. CERTIFICATION BASIS LIMITATIONS...

Installation of Honeywell ART2100/KMD850 Weather Radar System. Certification Basis Limitations 1. AFM-Supplement: 2044352-AM Issue 1;2. Engineering Order: 2044352-EO Issue 2;3. Continued Airworthiness: 2044352-CA Issue 1. Conditions 1. This STC is exclusively applicable for aircraft whichhave the equipment listed in chapter 4 of the Scandinavian Avionics Engineering Order 2044352-EO Issue 2 already installed;2. Prior to installation of this modification the installer must (...)
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INSTALLATION OF DUAL GTX 330D MODE S TRANSPONDER SYSTEMS.INSTALLATION OF...

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 ...
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INSTALLATION OF A SANDEL ST3400 TAWS SYSTEM (CLASS A) CERTIFICATION...

Installation of a SANDEL ST3400 TAWS System (Class A) Certification Basis Limitations See Scandinavian Avionics:# 2040484 STC (STC Document List)Issue 1, dated 12.2.2008# 2040484-EO Engineering Order Issue 2, dated 30.08.2007# 2040484-AM AFM Supplement Issue 2, dtd. 2.10.2007# 2040484-CA Instructions for Continued Airworthiness Issue 1, dtd.18.06.2007 Conditions Previous required aircraft configuration:All models equipped with:# Compatible Air Data Computers with ARINC 429 interface, and# Analogue Radio Altimeter interface ...
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DUAL TDR-94D TRANSPONDER UPGRADE TO PROVIDE LIMITED ENHANCED SURVEILLANCE TRANSPONDER...

Dual TDR-94D Transponder Upgrade to provide limited Enhanced Surveillance Transponder Mode S capability (Non EHS Capable). Certification Basis Limitations See Scandinavian Avionics:# 2044753 DOC (Certification Documents) issue 1, dated 12-Feb-08.# 2044753-TO TechnicalOrder (for installation instructions) issue 2, dated 11-Feb-08.# 2044753-AM AFM Supplement issue 1, dated 18-Feb -08.# 20447 (...) Conditions Previous required aircraft configuration:# Aircraft equipped with Dual TDR-94D (-007/- 008) and installation compliant with Elementary ...
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INSTALLATION OF A EGPWS MK. VIII SYSTEM IN ACCORDANCE WITH...

Installation of a EGPWS Mk. VIII system in accordance with the Engineering Order Doc.: 2017016-EO-02 Issue 2 or later EASA approvedrevision. Certification Basis Limitations Conditions 1. AFM Supplement Document No. 2017016-AM-02 Issue 2 orlater EASA approved revisions.2. Maintenance Requirements and Instruction for Continuous Airworthiness Doc. 2017016-CA-02.
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INSTALLATION OF HONEYWELL GNS-XLS FMS AND L3 STANDBY HORIZON REFERENCE...

Installation of Honeywell GNS-XLS FMS and L3 Standby horizon Reference System. Certification Basis Limitations Master Document List 2040837 DOC, Issue 1, dated 25/11/2007, or later approved revisions. Conditions
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MODE S UPGRADE OF EXISTING HONEYWELL TRANSPONDER SYSTEM RCZ-833 TO...

Mode S Upgrade of existing Honeywell Transponder System RCZ-833 to comply with ICAO requirements for Mode S ELS and EHS.Minor change to EASA.A.S.03107:AFM Supplements for different Downlinked Aircraft Parameters.Mode S Upgrade of existing Honeywell (...) Certification Basis Limitations Installation in accordance with Scandinavian Avionics Engineering Order ref 2037689-EO Issue 2, dated 2, May 2007, or later approved revisions.Aircraft to be operated in accordance with Scandinavian Avionics ...
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VHF COMM, XPDR, ICS, DIRECTIONAL GYRO AND ATTITUDE INDICATOR.

VHF COMM, XPDR, ICS, Directional Gyro and Attitude Indicator.
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DUAL INSTALLATION OF TRANSPONDER MODE S SYSTEM, MST 67A WITH...

Dual installation of Transponder Mode S System, MST 67A with PS 550 or PS 578A Mode S Control Panel, with ELS and EHS capability. Certification Basis Limitations EASA approved Engineering Order, Doc. No. 2041564-EO, Issue2, dated 13-Aug-2007 or later approved issueEASA approved Aircraft Flight Manual Supplement, Doc. No. 2041564 AM-A, Issue 1, dated 13-Aug-2007 or later approved issue for installation with P (...) Conditions This change ...
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INSTALLATION OF HONEYWELL MULTI-FUNCTION RADAR DISPLAY AND ENHANCED GROUND PROXIMITY...

Installation of Honeywell Multi-function Radar Display and Enhanced Ground Proximity Warning System (EGPWS) MK VIII.
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INSTALLATION OF A MULTI FUNCTION RADAR DISPLAY (MFRD) AND EGPWS...

Installation of a Multi Function Radar Display (MFRD) and EGPWS MK VIII in accordance with the Engineering Order Doc 2022874-EO- 01,Issue 2 or later EASA approved revisions Certification Basis Limitations AFM Supplement MFRD Document No 2022874-AM-01A Issue 2 or later EASA approved revisionsAFM Supplement EGPWS MK VIII Document No 2022874-AM-01B Issue 3 or later EASA approved revisionsInstructions for Continued Airworthiness Doc 2022874-CA-01 Conditions
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INSTALLATION OF DUAL GARMIN GNS 430A/530A AND 3RD COMM IN...

Installation of Dual Garmin GNS 430A/530A and 3rd COMM in Cessna Citation I model 500 and Citation II model 550, S550. Certification Basis Limitations # Engineering Order 2027496-EO-01, issue 3, dated 30 May2007, or later approved revision.# AFM Supplement Doc. 2027496- 01A, issue 2, dated 31 May 2007, or later approved revision. Conditions 1. Certification Basis of the Change CS-25 Amdt. 2, additionally:2. AMC 20-4 (Basic ...
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INSTALLATION OF DUAL GARMIN GNS 430A/530A AND 3RD COMM IN...

Installation of Dual Garmin GNS 430A/530A and 3rd COMM in Cessna Citation I model 501 and Citation II model 551. Certification Basis Limitations # Engineering Order 2027496-EO-01, issue 3, dated 30 May2007, or later approved revision.# AFM Supplement Doc. 2027496- 01A, issue 2, dated 31 May 2007, or later approved revision. Conditions 1. Certification basis of the Change CS-23, additionally:2. AMC 20-4 (Basic RNAV), AMC 20-5 ...
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INSTALLATION OF A SINGLE DIVERSITY MODE-S TRANSPONDERGARMINGTX 330D AND A...

Installation of a single diversity Mode-S transponderGarminGTX 330D and a new top antenna. Certification Basis Limitations STC Document List 2036635 STCCompliance Record AMC 2036635- CRAFM Supplement ELS 2036635-AM- AAFM SupplementEHS 2036635-AM-B Conditions According to EUROCONTROL definition this equipment with approval EASA.A.S.03036 is non-EHS compliant.Prior to installation of this modification the installer must determine that the interrelationship between this modification and any otherpreviously (...)
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INSTALLATION OF HONEYWELL TRA-45A TERRAIN DISPLAY/ RADIO ALTIMETER INDICATOR.

Installation of Honeywell TRA-45A Terrain Display/ Radio Altimeter Indicator.
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INSTALLATION OF HONEYWELL TRA-45A TERRAIN DISPLAY/ RADIO ALTIMETER INDICATOR. CERTIFICATION...

Installation of Honeywell TRA-45A Terrain Display/ Radio Altimeter Indicator. Certification Basis Limitations Installation in accordance with Scandinavian Avionics Engineering Order Reference 2037690-EO Issue 2, dated 20 April 2007, or laterapproved revisions.Aircraft to be operated in accordance with Scandinavian Avionics Flight Manual SupplementReference (...) Conditions Aircraft Serial No. 650-0037 with FOCA STC Z34-44-05 installed as defined in Scandinavian Avionics Modification Reference 2037690.
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INSTALLATION OF UNIVERSAL UNS-1L/K+, FMS- SYSTEM. LIMITATIONS: N/A. CONDITIONS: N/A

Installation of Universal UNS-1L/K+, FMS- system. Limitations: N/A. Conditions: n/a
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INSTALLATION OF SANDEL ST3400 TAWS SYSTEM. CERTIFICATION BASIS LIMITATIONS ENGINEERING...

Installation of Sandel ST3400 TAWS System. Certification Basis Limitations Engineering Order, Doc. No. 2037448-EO, Issue 2, dated 07-March-2007 or later approved issue.EASA approved Aircraft Flight Manual Supplement, Doc. No. 2037448-AM-( ), Issue 2, dated 28 March 2007, or later approved revisions.STC Document List, Doc. (...) Conditions
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INSTALLATION OF A HONEYWELL CAS 67A ACAS II SYSTEM AND...

Installation of a Honeywell CAS 67A ACAS II System and a Dual MST 67A Mode S Transponder System Certification Basis Limitations Engineering Order, Doc. No. 2038224-EO, Issue 2, dated 21-Mar-2007 or later approved issueEASA approved Aircraft FlightManual Supplement, Doc. No. 2038224-AM-A, Issue 1, dated 16-Mar-2007 or later approved issueand one of the following: * EASA approved Aircraft Flight Manual Supplement, Doc. No. Conditions This change is ...
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MODE-S UPGRADE FOR EXISTING HONEYWELL MST 67A TRANSPONDER SYSTEM. CERTIFICATION...

Mode-S upgrade for existing Honeywell MST 67A transponder system. Certification Basis Limitations Means of Compliance list 2036715 MOC.AFM Supplements -2036715-AM A for aircraft without Primus 1000 EFIS;2036715- AM B for aircraft with Primus 1000 EFIS.2036715-AM C for aircraft with Primus 1000 EFIS.System Description 2036715- DE,Engineering Order (...) Conditions N/A
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INSTALLATION OF AN IN-FLIGHT ENTERTAINMENT SYSTEM CERTIFICATION BASIS LIMITATIONS ENGINEERING...

Installation of an In-flight Entertainment System Certification Basis Limitations Engineering Order, Doc. No. 2031919-EO- 01, issue 2, dated 16-May-2006, or later approved issueEASA approved Aircraft Flight Manual Supplement, Doc. No. 2031919-AM- 01, Issue 3, dated 08-Feb-2007, or later approved IssueInstructions for Continued Airw (...) Conditions This change is limited to airplanes equipped with ARINC 429Interface to GPS / FMS
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MODE S TRANSPONDER UPGRADE FOR EXISTING COLLINS TRANSPONDERSYSTEM. CERTIFICATION BASIS...

Mode S Transponder Upgrade for existing Collins transpondersystem. Certification Basis Limitations Upgrade of existing Collins transponder system in accordance with:Document List 2036079 DOC andEngineering Order 2036079-EO.Operation in accordance with :Flight Manual Suppl. 2036079-AM- AFlight Manual Suppl. 2036079-AM- BContinuing Airworthiness 2036079-CA . Conditions 1. This STC approves only the installation of the parts contained in the above section #Description of Type Design Change#. This STC grants no ...
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HONEYWELL EGPWS MK VIII INSTALLATION CERTIFICATION BASIS LIMITATIONS ENGINEERING ORDER...

Honeywell EGPWS MK VIII Installation Certification Basis Limitations Engineering Order 2035914-EO Issue 2, dated 10-01-2007 or later approved revisions.Aircraft Flight Manual Supplement 2035914-AM Issue 1, dated January 2007 or later approved revisions. Conditions Certification Basis of the Change: CS 25 Amendment 2, additionally JAA Leaflet No. 12 (TAWS).
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INSTALLATION OF UNIVERSAL UNS-1L (-1K+) FMS

Installation of Universal UNS-1L (-1K+) FMS
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HONEYWELL EGPWS MK VIII INSTALLATION

Honeywell EGPWS MK VIII Installation
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UPGRADE OF EXISTING MST-67A TRANSPONDER SYSTEM CERTIFICATION BASIS LIMITATIONS INSTALLATION...

Upgrade of existing MST-67A Transponder System Certification Basis Limitations Installation in accordance with Scandinavian Avionics Engineering Order ref 2036080-EO Issue 1, dated 22 December 2006,or later approved revisions.Aircraft to be operated in accordance with Scandinavian Avionics Flight Manual Supplement ref 2036080- (...) Conditions As defined in Scandinavian Avionics Modification ref 2036080.
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INSTALLATION OF A UNIVERSAL UNS-1F AND / OR UNS-1L FLIGHT...

Installation of a Universal UNS-1F and / or UNS-1L Flight Management System for Basic RNAV, Precision RNAV Operations and Non- precision Approaches and also as a primary means of navigation for oceanic/remote operations. Certification Basis Limitations Technical Order, Doc. No. 2035499-TO, issue 2, dated 04-Jan-2007, or later approved issueEASA approved Aircraft Flight Manual Supplement, Doc. No. 2035499-AM-A, Issue 1, dated October 2006, or later approved Issue, ...
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INSTALLATION OF A UNIVERSAL TERRAIN AWARENESS WARNING SYSTEM (TAWS). CERTIFICATION...

Installation of a Universal Terrain Awareness Warning System (TAWS). Certification Basis Limitations - Technical Order, Doc. No. 2035674-TO, issue 3, dated 03-Jan-2007, or later approved issue- EASA approved Aircraft Flight Manual Supplement, Doc. No. 2035674-AM-A, Issue 1, datedSeptember 2006, or later approved Issue for operation with FMS display (...) Conditions 1. This change is limited to following configuration of theaircraft / equipment type:all airplanes equipped with* ...
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TRANSPONDER S MODE ELEMENTARY AND ENHANCED SURVEILLANCE / UPGRADE OF...

Transponder S Mode Elementary and Enhanced Surveillance / Upgrade of existing dual diversity Transponder Mode S Installation Limitations: Certification Basis of the change: CS 25 Amdt. 2, additionally JAA TGL 13 Rev. 1 (Mode S ELS), JAA TGL 18 (Mode S EHS, compliance to JAA NPA 20-12a shown voluntarily.This STC is approved only for the product configuration as defined in the approved design. Conditions: n/a
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INSTALLATION OF A HONEYWELL CLASS A ENHANCED GROUND PROXIMITY WARNING...

Installation of a Honeywell Class A Enhanced Ground Proximity Warning System EGPWS/TWAS for aircrafts equipped with a compatible MFD or weather radar display. Certification Basis Limitations # Technical Order, Doc. No. 2036070-TO, issue 1, dated 13-Dec-2006, or later approved issue.# EASA approved Aircraft Flight Manual Supplement, Doc. No. 2036070 AM, Issue 2, dated December 2006, or later approved Issue.# Instructions for Con (...) Conditions 1. This ...
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HONEYWELL EGPWS MK VIII INSTALLATION CERTIFICATION BASIS LIMITATIONS ENGINEERING ORDER...

Honeywell EGPWS MK VIII Installation Certification Basis Limitations Engineering Order 2035111-EO Issue 1, dated 16/08/2006 or alter approved revisionAircraft Flight Manual Supplement 2035111-AM Issue 1, dated August 2006 or later approved revision Conditions Certification Basis of the Change: CS 25 Amanedment 1m, aditionally JAA Leaflet No. 12 (TAWS)
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INSTALLATION OF HONEYWELL MULTI-FUNCTION RADAR DISPLAY (MFRD) AND AS AN...

Installation of Honeywell Multi-Function Radar Display (MFRD) and as an option a Honeywell Primus 400 Radar system. Certification Basis Limitations Installation in accordance with Scandinavian Avionics Engineering Order ref 2034305-EO Issue 2, dated 29.6.2006, or later approved revisions.Operation in accordance with Scandinavian Avionics Flight Manual Supplement ref 2034305-AM Issue 1, dated Au (...) Conditions This STC is only applicable to Aircraft without EFIS systemand integrated MFD.
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INSTALLATION OF A #FLIGHT DISPLAY SYSTEMS# ENTERTAINMENT SYSTEM: DVD PLAYER,...

Installation of a #Flight Display Systems# Entertainment System: DVD player, Map computer and 2 LCD displays Certification Basis Limitations System Description 2029710-DE,Drawing List 2029710-DL,MoC list 2029710- MOC,Engineering Order 2029710-EO,AFM Supplement 2029710-AM Conditions The IFE sound shall be overrided by the PA system
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INSTALLATION OF A GARMIN GNS 530A AND A HONEYWELL MARKER...

Installation of a Garmin GNS 530A and a Honeywell Marker Beacon KR21, for EU basic RNAV operations Certification Basis Limitations System Description 2032044-DE Iss. 2,Drawing List 2032044-DL Iss. 2,MoC list 2032044,AFM Supplements 2032044-AM-A Iss. 3 and 2032044AM-B Iss. 2 Conditions None
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INSTALLATION OF BENDIX/KING RADAR ALTIMETER SYSTEM KRA 405/405B

Installation of Bendix/King Radar Altimeter System KRA 405/405B
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SANDEL ST3400 TAWS INSTALLATION LEFT HAND AND RIGHT HAND CERTIFICATION...

Sandel ST3400 TAWS Installation left hand and right hand Certification Basis Limitations Engineering Order 2031680-EO-01 Issue 1 or later approved RevisionsAircraft Flight Manual Supplement 2031680-AM-01 A Issue 4 or later approved RevisionsAircraft Flight Manual Supplement 2031680-AM-01 B Issue 1 or later approved Revisions Conditions Certifications Basis of the Change: CS 25, additionally JAALeaflet No. 12 (TAWS)
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INSTALLATION OF ELT TYPE KANNAD 406 AF / AF- H....

Installation of ELT type Kannad 406 AF / AF- H. Reuse or exchange ofantenna
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INSTALLATION OF GPS400 IN CENTER PANEL WITH GAD 42 ADAPTER...

Installation of GPS400 in center panel with GAD 42 adapter for roll steering Certification Basis Limitations Approved Aircraft Flight Manual Supplement for Garmin GPS 400 GPS System Doc. No. 2027746-AM-02 issue 2, dated August 2005 or laterapproved revision Conditions
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INSTALLATION OF HONEYWELL CAS 67A ACAS SYSTEM INCLUDING DUAL MST...

Installation of Honeywell CAS 67A ACAS System including Dual MST 67AMode-S Transponders
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INSTALLATION OF HONEYWELL KMH 880 MULTI- HAZARD AWARENESS SYSTEM CERTIFICATION...

Installation of Honeywell KMH 880 Multi- Hazard Awareness System Certification Basis Limitations Airplane Flight Manual Supplement fo rInstallation of Honeywell KMH 880 Multi- Hazard Awareness System Doc No 2027746 AM-01 Issue 1,dated May 2005 or later approved revision Conditions 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/engineconfigurations shall ...
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INSTALLATION OF A L3 DIGITAL FDR AND TELEDYNE FDAU CERTIFICATION...

Installation of a L3 Digital FDR and Teledyne FDAU Certification Basis Limitations 1) Engineering Order Doc. No.2029534-AM- 01 Issue 2 or laterEASA approved Revisions.2) Airplane Flight Manual Supplement, Doc. No.2029534-AM-01 Issue 2 or later EASA approved Revisions.3) Instruction for Continuous Airworthiness Doc. No.2029534-CA-01. Conditions
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IINSTALLATION OF A ROCKWELL COLLINS TCAS 4000 WITH DUAL TDR-94D...

IInstallation of a Rockwell Collins TCAS 4000 with dual TDR-94D Transponder Certification Basis Limitations Engineering Order Doc. No. 2027113-EO-01 Issue 1 or later EASA approved revisions.Airplane Flight Manual Supplement Rockwell Collins TCAS 4000 Doc. No. 2027113-AM-01A Issue 2 or later EASA approved Revisions.Airplane Flight Manual Supplement Rockwel (...) Conditions
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INSTALLATION OF FREEFLIGHT 2101 I/O APPROACH PLUS GPS NAVIGATION SYSTEM...

Installation of FreeFlight 2101 I/O APPROACH PLUS GPS Navigation System Certification Basis Limitations - Scandinavian Avionics Engineering Order No. 2019034-EO-03, Issue No. 2, dated August 3, 2005- Approved AirplaneFlight Manual Supplement for FreeFlight 2101 I/O APPROACH PLUS GPS Navigation System Conditions -
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INSTALLATION OF HONEYWELL CAS 67A TCAS II SYSTEM, INCLUDINGDUAL MST...

Installation of Honeywell CAS 67A TCAS II System, includingDual MST 67A Mode S Transponders Certification Basis Limitations - Scandinavian Avionics Engineering Order No. 2015055-EO-01, Issue 1, dated October 8, 2004- Approved Airplane Flight Manual Supplement for HONEYWELL MST 67A MODE - S Transponder with PS550 Control, Doc. No. 2015055-AM-01B- Approved Airplan (...) Conditions -
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INSTALLATION OF A ROCKWELL COLLINS TCAS 4000 WITH DUAL TDR-94D...

Installation of a Rockwell Collins TCAS 4000 with dual TDR-94D Mode S Transponder Certification Basis Limitations -Engineering Order Doc No 2025716-EO-01 dated 09.03.2005 Issue 1 or later EASA approved revisions-Airplane Flight Manual Supplement/TCAS 4000 Doc No 2025716- AM-01A issue 2 or later EASA approved revisions-Airplane Flight Manual Supplement/Dual TDR Conditions
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INSTALLATION OF A HONEYWELL KMD 850 SYSTEM AND INSTALLATIONOF A...

Installation of a Honeywell KMD 850 System and installationof a TCAS ISky
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INSTALLATION OF A HONEYWELL KMD 850 SYSTEM AND INSTALLATIONOF A...

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.
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INSTALLATION OF AN ADF 2 BENDIX KING KDF 806 SYSTEM....

Installation of an ADF 2 Bendix King KDF 806 System. Limitations: 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.. Conditions: n/a
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INSTALLATION OF HONYWELL CAS 67A ACAS/TCAS II WITH DUAL MST-67A...

Installation of Honywell CAS 67A ACAS/TCAS II with dual MST-67A Mode S Transponder Certification Basis Limitations -Certification Documents List 2020220-02, 19.04.2005-AFMS 2020220-AM-02A, Issue 2, or later EASA approved issues-AFMS 2020220-AM-02B, Issue 2, or later EASA approved issues Conditions Certification Basis: applicable requirements of CS25 plus JAA TGLs No 8 and 13 1.
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INSTALLATION OF ROCKWELL COLLINS TCAS-4000 INCL. DUAL MODE S TRANSPONDER...

Installation of Rockwell Collins TCAS-4000 incl. Dual Mode S Transponder TDR-94D in accordance with the Engineering Order Doc 2022256-EO-01 Issue 2 or later EASA approved revisions Certification Basis Limitations AFM Supplement ACAS Document No 2022256-AM-01A issue 2 or later EASA approved revisionsAFM Supplement Mode S Document No 2022256-AM-01B Issue 2 or later EASA approved revisionsInstructions for Continued Airworthiness Doc 2022256-CA-01 Conditions
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INSTALLATION OF A KANNAD 406 ELT IN ACCORDANCE WITH ENGINEERING...

Installation of a Kannad 406 ELT in accordance with Engineering Order Doc 2022256-EO-03, Issue 1 or later EASA approvedrevisions Certification Basis Limitations AFM Supplement Document No 2022256-AM 03 Issue 2 or later EASA aproved revision Instructions for Continued Airworthiness Doc 2022256-CA-03 Conditions -
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INSTALLATION OF BENDIX/KING KRA 405B RADAR ALTIMETER

Installation of Bendix/King KRA 405B Radar Altimeter
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INSTALLATION OF BENDIX/KING KLN 94 GPS SYSTEM. CERTIFICATION BASIS LIMITATIONS...

Installation of Bendix/King KLN 94 GPS System. Certification Basis Limitations EASA-approved Flight Manual Supplement 2019974-AM-03, issue2, or later EASA- approved issue. Conditions
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INSTALLATION OF HONEYWELL KMH 980 MULTI- HAZARD AWARENESS SYSTEM INCLUDING...

Installation of Honeywell KMH 980 Multi- Hazard Awareness System including TCAS I and EGPWS (Class B). Certification Basis Limitations EASA-approved Flight Manual Supplement 2019974-AM-01, issue2, or later EASA- approved issue. Conditions
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INSTALLATION OF WX-500 STORMSCOPE SYSTEM CERTIFICATION BASIS LIMITATIONS EASA-APPROVED FLIGHT...

Installation of WX-500 Stormscope System Certification Basis Limitations EASA-approved Flight Manual Supplement 2019974-AM-02, issue2, or later EASA- approved revision. Conditions
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INSTALLATION OF KANNAD 406 AF ELT CERTIFICATION BASIS LIMITATIONS -ENGINEERING...

Installation of Kannad 406 AF ELT Certification Basis Limitations -Engineering Order 2022014 - EO - 02.-AFM Supplement, Doc. No 2022014 - AM - 02.- Continued Airworthiness Report Doc. No2022014 - CA - 02. 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 ...
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INSTALLATION OF A ROCKWELL COLLINS ACAS (TCASII) 4000 WITH DUAL...

Installation of a Rockwell Collins ACAS (TCASII) 4000 with dual Mode S Transponders Certification Basis Limitations -Engineering Order 2019360-EO-01, Issue 3- Certification Documents List, 24.1.2005- AFMS Issue 2, January 2005 Conditions 1. Certification Basis for this STC is CS 25 plus JAA TGL No 8 and JAA TGL No 13
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INSTALLATION OF A HONEYWELL EGPWS MARK VIII (TAWS) CERTIFICATION BASIS...

Installation of a Honeywell EGPWS mark VIII (TAWS) Certification Basis Limitations -Engineering Order 2019360-EO-03, Rev. 2- Certification Documents List, 24.01.2005- AFMS Issue 1, November 2004 Conditions Certification Basis for this STC is CS 25 plus JAA TGL No 12 "TAWS"
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INSTALLATION OF A L3 DIGITAL FLIGHT DATA RECORDER CERTIFICATION BASIS...

Installation of a L3 Digital Flight Data Recorder Certification Basis Limitations -Engineering Order 2019360-EO-02, Issue 1- Certification Documents List, 30.12.2004- AFMS Issue 1, October 2004 Conditions Certification Basis for this STC is CS 25
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INSTALLATION OF AN UNIVERSAL CVR-30B COCKPIT VOICE RECORDERIN ACCORDANCE WITH...

Installation of an Universal CVR-30B Cockpit Voice Recorderin accordance with the Engineering Order Doc: 2022468-EO-01, Issue 1 orlater EASA-approved Revisions. AFM Supplement Document No 2022468-AM- 01 Issue 1 or later EASA-approved Revisions. Maint (...) Certification Basis Limitations 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 ...
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INSTALLATION OF A KANNAD 406 AF ELT IN ACCORDANCE WITH...

Installation of a Kannad 406 AF ELT in accordance with the EngineeringOrder Doc.: 2021390-EO-01, Issue 2 or later EASA approved revisionsAFM Supplement Document No. 2021390-AM-02,Issue 2 or later EASAapproved revisionsMaintenance Requirements and Instructions for Airworthiness Doc.:2021390-CA-01
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INSTALLATION OF AN L3 DIGITAL FDR F-1000 IN ACCORDANCE WITHTHEENGINEERING...

Installation of an L3 digital FDR F-1000 in accordance withtheEngineering Order Doc.: 2021094-EO-01, Issue 2 or later EASA approved Revisions.AFM Supplement Document No 2021094-AM-02 Issue 2 or later EASA approvedRevisions.Maintenance Requirements and Instructions for Continuous AirworthinessDoc. 20...
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INSTALLATION OF A ROCKWELL COLLINS TCAS-4000INCL. DUAL COLLINS MODE- STRANSPONDER...

Installation of a Rockwell Collins TCAS-4000incl. Dual Collins Mode- STransponder TDR-94 D in accordance with Engineering Order Doc.:2017016-EO-13, issue 2 or later EASA approved Revisions.
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INSTALLATION OF AN ARTEX ELT 406 IN ACCORDANCE WITH ENGINEERING...

Installation of an Artex ELT 406 in accordance with Engineering OrderDoc.: 20176016-EO-01 Issue 2 or later EASA approved revision.
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