MODIFICATIONS OF Carlisle Interconnect Technologies (157)

ARINC 791 FLIGHTGEAR™ KA/KU UNIVERSAL INSTALLATION

Carlisle Interconnect Technologies, in a partnership with Saint Gobain Performance Plastics, now offers a complete ARINC 791 solution for Ka- and Ku-band SATCOM installations. The complete package contains everything required for either retrofit or forward fit installations on large jet aircraft. Installation fittings are adjustable to cover the complete range of aircraft frame spacing while providing discrete interface loads to the fuselage. The aerodynamic fairing follows ...
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VALIDATION OF FAA STC ST02923CH: EFB INSTALLATION OF ECS EZMOUNTTMMECHANICAL...

Validation of FAA STC ST02923CH: EFB Installation of ECS EZMountTMMechanical Mounting Assemblies
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INSTALLATION OF A ROSEMOUNT AEROSPACE ELECTRONIC FLIGHT BAG(EFB) CLASSIII:- CONFIGURATION...

Installation of a Rosemount Aerospace electronic flight bag(EFB) classIII:- Configuration 1: Installation of Dual SDU electrical power withcrosstalk capabilities between the two units- Configuration 2: Installation of Dual SDU and EFB-IU P1 connectionsonly- Configuration 3: Installation of Dual SDU...
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INSTALLATION OF ELEMENTARY OR ENHANCED SURVEILLANCE MODE S TRANSPONDERSREV. 1:...

Installation of Elementary or Enhanced Surveillance Mode S TranspondersRev. 1: Configurations 5 and 8 addedRev. 2: Configurations 7 and 9 addedRev. 3: Configuration 6 added
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INSTALLATION FOR A ROCKWELL COLLINS SATCOM 2100 SYSTEM:-CONFIGURATION 1: FOR...

Installation for a Rockwell Collins SATCOM 2100 System:-Configuration 1: for Aircraft without existing Boeing SATCOM provisions- Configuration 2: for Aircraft with existing Boeing SATCOM provisionswith partial Boeing SATCOM provisions (HF/SAT panel installed in P6Panel)-Configuration 3: for Aircraft(...
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INSTALLATION OF AN INTERMEDIATE GAIN ANTENNA (IGA) SUBSYSTEM:- CONFIGURATION 1:...

Installation of an Intermediate Gain Antenna (IGA) subsystem:- configuration 1: for aircraft without existing SATCOM antennaprovisions from Boeing- configuration 2: for aircraft with existing SATCOM antenna provisionsfrom Boeing- configuration 3: installation of IGA provisions for aircraft withoutex...
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INSTALLATION OF ECS EZMOUNT MECHANICAL MOUNTING ASSEMBLIESCONFIGURATIONS :-1: MASTER KIT,...

Installation of ECS EZMount Mechanical Mounting AssembliesConfigurations :-1: Master Kit, EZMount® Slider 737-2: MasterKit, EZMount® Pivot 737-3: Master Kit, EZMount® Slider 737 ClassicRevision1: addition of configuration 4 Master Kit, EZMount Pivot for737-300/400/500
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INSTALLATION OF ECS EZMOUNT® TABLET CRADLE ASSEMBLIES ON EXISTINGEZMOUNT® PIVOT...

Installation of ECS EZMount® Tablet Cradle assemblies on existingEZMount® Pivot installations:- configuration 1: Cradle(8.0" X 10.7") provisions- configuration 2: Cradle (8.5" X 11.2") provisions
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VALIDATION OF FAA STC ST02923CH: EFB INSTALLATION OF ECS EZMOUNTTMMECHANICAL...

Validation of FAA STC ST02923CH: EFB Installation of ECS EZMountTMMechanical Mounting Assemblies Limitations: 1) This approval constitutes approval for the EZMountTM MechanicalMounting Assemblies only. The capability of any system attached to theEZMountTM Mechanical Mounting Assembly requires additional EASAapproval. 2) The maximum allowed weight of any device to. Conditions: Prior to installation of this STC it must be determined that theinterrelationship between this modification and any other ...
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INSTALLATION OF A CONNEXION BY BOEING NEXT GENERATION ANTENNA AND...

Installation of a Connexion by Boeing Next Generation Antenna and Satellite Data System.
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INSTALLATION OF CLASS II ELECTRONIC FLIGHT BAG PROVISIONS IN ACCORDANCE...

Installation of Class II Electronic Flight Bag Provisions in accordance with Star Aviation Inc. Master Data List R46-0543, Revision J, Dated October 11, 2011, or later FAA approved revision.
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INSTALLATION OF CONNEXION BY BOEING NEXT GENERATION ANTENNA AND SATELLITE...

Installation of Connexion by Boeing Next Generation Antenna and Satellite Data System in accordance with Star Aviation Inc. Master Data List R44-0163, Revision CP, Dated May 12, 2011, or later FAA approved revision.
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INSTALLATION OF EMS TECHNOLOGIES AERONAUTICAL DATA TERMINAL SYSTEM.

Installation of EMS Technologies Aeronautical Data Terminal System.
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INSTALLATION OF EZMOUNT (TM) ARM MECHANICAL MOUNTING ASSEMBLIES ON LOWERFRAME...

Installation of EZMount (TM) Arm mechanical mounting assemblies on lowerframe of cockpit sliding window in accordance with Electronic CableSpecialists Master Data List ECS-207476 Rev. A, dated March 4, 2009, orlater FAA approved revisions.Validation of FAA STC ST02708CH Limitations: AFM Supplement as listed in Appendix A of ECS Master Data ListECS-207476 Rev. A Conditions: AFM Supplement as listed in Appendix A of Electronic Cable SpecialistsMaster Data List ...
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VALIDATION OF FAA STC ST03007CHLINEFIT INSTALLATION OF A DUAL CMC...

Validation of FAA STC ST03007CHLinefit installation of a Dual CMC Electronics Class 3 Electronic FlightBag (EFB) System. Limitations: - Certification Plan, ECS-208298, Revision G, dated 11 January 2012- Project Compliance Report, ECS 208299, Revision B, dated 19 January2012- EASA Certification Comparison for STCST03007CH, ECS-210256, Initial release, dated 23 May 2012- Master Data L (...) Conditions: 1) The Operating System (OS) for which this Class 3 EFB ...
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INSTALLATION AND ACTIVATION OF AN ASTRONAUTICS CORPORATION OF AMERICAELECTRONICS CLASS...

Installation and activation of an Astronautics Corporation of AmericaElectronics Class 3 Electronic Flight Bag (EFB) System consisting of anElectronic Unit (EU) and a Display Unit(DU). Limitations: ECS-207709, rev. F, Electronic Cable Specialist Master Data List<(>,<)>ECS- 207678, rev A, Project Compliance Report<(>,<)>ECS-207718, rev C, AFM Supplement<(>,<)>ECS-207717, rev A, Instructions for Continued Airworthiness<(>,<)>ECS-210738,rev N/C, EA (...) Conditions: Information displayed on the EFB is not to be used for ...
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RETROFIT INSTALLATION OF A DUAL CMC ELECTRONICS CLASS 3 ELECTRONICFLIGHT...

Retrofit installation of a Dual CMC Electronics Class 3 ElectronicFlight Bag (EFB) System. Limitations: Certification Plan, ECS-209314, Revision E, dated 8 July 2011- Project Compliance Report, ECS 209313, Revision D, dated7 October2011- EASA Certification Comparison for STC ST03006CH, ECS-210121, Initial release, dated 23 May 2012- Master Data List, E (...) Conditions: 1) The Operating System (OS) for which this Class 3 EFB system isintended has not ...
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INSTALLATION OF A ROSEMOUNT AEROSPACE 8700E1 CLASS 3 ELECTRONIC FLIGHTBAG...

Installation of a Rosemount Aerospace 8700E1 Class 3 Electronic FlightBag (EFB) System. - Approved configurations are the following:- Configuration 1: Installation of Dual SDU electrical power withcrosstalkcapabilities between the two units<(>,<)>- (...) Limitations: - Certification Plan, ECS-209047, Revision G, dated 27 April 2011- Project Compliance Report, ECS 209073, Revision D, dated 02 June 2011- EASA Certification Comparison for STC ST02949CH ECS-210104, Revision B, dated 04 January ...
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INSTALLATION OF ECS EZMOUNTTM TILT MECHANICAL MOUNTING ASSEMBLIES ON LOWER...

Installation of ECS EZMountTM Tilt mechanical mounting assemblies on lower frames of cockpit sliding windows.
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VALIDATION OF FAA STC ST02992CH - INSTALLATION OF DUAL ELECTRONIC...

Validation of FAA STC ST02992CH - Installation of dual Electronic FlightBag (EFB) System Provisions. Limitations: 1) The aircraft operator must perform the instructions for continuedairworthiness and comply with the Airworthiness Limitation Items as perthe Instructions for Continued Airworthiness (ICA), ReferenceECS-209337, Revision G, dated 22 August 2012. 2) Additio. Conditions: 1) Prior to installation of this STC it must be determined that theinterrelationship between this STC and ...
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INSTALLATION OF CABIN WIRELESS LOCAL AREA NETWORK (CWLAN) IN ACCORDANCEWITH...

Installation of Cabin Wireless Local Area Network (CWLAN) in accordancewith Star Aviation Inc. Master Data List R44-0175, Revision G, datedOctober 13, 2004, or later FAA approved revisions and Provisionalinstallation of a Panasonic Avionics Corporation eXP Limitations: None. Conditions: AFM Supplement R44-0293, Revision A, dated October 18, 2004 shall be onboard the modified aircraftInstructions for Continued Airworthiness Document # R44-0182 Rev. IRdate June 16, 2004, Document # ...
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VALIDATION OF FAA STC ST02961CH - APPROVED CONFIGURATIONS ARE THEFOLLOWING:-...

Validation of FAA STC ST02961CH - Approved configurations are thefollowing:- Configuration 1: Replacement of Honeywell Weather Radar System RDR-4Bwith Honeywell Honeywell Weather Radar RDR- 4000<(>,<)>-Configuration 2: Software upgrade to Honeywell WRS RDR-4 Limitations: None. Conditions: 1) Prior to installation of this STC it must be determined that theinterrelationship between this STC and any other previously installedmodification and / or repair will introduce no adverse effect upon ...
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INSTALLATION OF A ROSEMOUNT AEROSPACE 8700E1 CLASS 3 ELECTRONIC FLIGHT...

Installation of a Rosemount Aerospace, Inc. 8700E1 Class 3 Electronic Flight Bag (EFB) System.
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INSTALLATION OF ECS EZMOUNT MECHANICAL MOUNTING ASSEMBLIES IN ACCORDANCEWITH ELECTRONIC...

Installation of ECS EZMount mechanical mounting assemblies in accordancewith Electronic Cable Specialists, Inc. Master Data List ECS 209135,Revision H, dated November 29, 2011 or later approved revisionValidation of FAA STC ST02907CH Limitations: The equipment for which these provisions are installed has not beencertified. Additional approval is required for the installation of thisequipment and must be evaluated to assure satisfactory compliance withapplicable airworthiness standards.. Conditions: AFM Supplement ...
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INSTALLATION AND ACTIVATION OF AN ASTRONAUTICS ELECTRONIC FLIGHT BAG SYSTEM

Installation and activation of an Astronautics Corporation of America Electronic Flight Bage (EFB) System.
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INSTALLATION OF A LAPTOP STOWAGE/CHARGER ASSEMBLY FOR CLASS I EFB

STC ST01118CH supports installation of a laptop stowage/charger assembly behind the flight crew seats in accordance with Electronic Cable Specialists (ECS) Master Data List ECS-980089.
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INSTALLATION OF A CMC ELECTRONICS CLASS 3 ELECTRONIC FLIGHT BAG...

Installation of a CMC Electronics Class 3 Electronic Flight Bag (EFB) System Activation.
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INSTALLATION OF CONNEXION BY BOEING NEXT GENERATION ANTENNA AND SATELITEDATA...

Installation of Connexion by Boeing Next Generation Antenna and SateliteData System in accordance with Star Aviation Inc. Master Data ListR44-0163, Revision CP, Dated May 12, 2011 or later approved revision Limitations: None. Conditions: Aircraft Flight Manual Supplement R44- 0300 Rev. IR dated October 16,2004 is a required part of this STC.Instruction for Continued Airworthiness Star Aviation Document No #R44-0273, Rev. D, dated June 20, 2011 must ...
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UPGRADE OF AN EXISTING SINGLE HONEYWELL RDR-4B WEATHER RADAR SYSTEM...

Upgrade of an existing single Honeywell RDR-4B Weather Radar System with a more advanced single Honeywell RDR-4000 Weather Radar System. 
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INSTALLATION OF ECS EZMOUNTTM MECHANICAL MOUNTING ASSEMBLIES ON SIDEWALLS..

Installation of ECS EZMountTM mechanical mounting assemblies on sidewalls of cockpit.
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INSTALLATION OF ECS EZMOUNTTM MECHANICAL MOUNTING ASSEMBLIES.

Installation of ECS EZMountTM Mechanical Mounting Assemblies. 
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INSTALLATION OF AN EZMOUNT™ TILT MECHANICAL MOUNTING ASSEMBLYREVISION OF THE...

Installation of an EZMount™ Tilt Mechanical Mounting AssemblyRevision of the EASA STC EASA.IM.A.S.03101 to add Configuration 2 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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INSTALLATION OF UNIVERSAL AVIONICS SYSTEMS CORPORATION MULTI-FUNCTION...

Installation of a Universal Avionics Systems Corporation Multi-Function Displays.
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MODIFICATION OF THE WIRING INTERFACE BETWEEN THE FLIGHT MANAGEMENT COMPUTER...

Modification of the wiring interface between the Flight Management Computer System (FMCS) and the ACARS Communications Management Unit (CMU-900).
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UPGRADE OF THE INTERNAL CORE SOFTWARE OF THE ACARS COMMUNICATIONS...

Upgrade of the internal core software of the ACARS Communications Management Unit (CMU-900).
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UPGRADE OF THE INTERNAL CORE SOFTWARE OF THE ACARS DATA...

Upgrade of the internal core software of the ACARS Data Link Management Unit (DLM-900).
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INSTALLATION OF A UNIVERSAL AVIONICS SYSTEMS CORPORATION (UASC) TERRAIN AWARENESS...

Installation of a Universal Avionics Systems Corporation (UASC) Terrain Awareness and Warning System (TAWS) and UASC UNS-1F Flight Management System (FMS) as a position source for TAWS or installation of a UASC TAWS and triple UASC FMS.
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UPGRADE OF THE INTERNAL CORE SOFTWARE OF THE ACARS DATA...

Upgrade of the internal core software of the ACARS Data Link Management Unit (DLM-900).
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UPGRADE OF THE INTERNAL CORE SOFTWARE OF THE ACARS COMMUNICATIONS...

Upgrade of the internal core software of the ACARS Communications Management Unit (CMU-900).
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UPGRADE OF THE INTERNAL CORE SOFTWARE OF THE ACARS DATA...

Upgrade of the internal core software of the ACARS Data Link Management Unit (DLM-900).
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INSTALLATION OF MOUNTING BRACKETS AS PROVISIONS FOR FUTURE MECHANICAL INSTALLATION...

Installation of mounting brackets as provisions for future mechanical installation of Electronic Flight Bag Display Units (DUs) and Remote Processing Units (RPUs).
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INSTALLATION OF A GLOBAL MOBILE SATELLITE TELEVISION AND DATA SYSTEM....

Installation of a global mobile satellite television and data system. Limited to installation on Boeing model 737-7AH IGW, serial number 29749 ONLY.
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INSTALLATION OF ECS EZMOUNT (TM) MECHANICAL MOUNTING ASSEMBLIES LIMITATIONS: SEE...

Installation of ECS EZMount (TM) mechanical mounting assemblies Limitations: see limitations and conditions on STC FAA ST02637CH. 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 EZMOUNT (TM) TILT MECHANICAL MOUNTING ASSEMBLY ONSIDEWALLS OF...

Installation of EZMount (TM) Tilt mechanical mounting assembly onsidewalls of cockpit in accordance with Electronic Cable SpecialistsMaster Data List ECS-207476 Rev. A, dated March 4, 2009, or later FAAapproved revisions.Validation of FAA STC ST02708CH Limitations: AFM Supplement as listed in Appendix A of Electronic Cable SpecialistsMaster Data List ECS-207476, Rev. A, dated March 4, 2009 or later FAAapproved revision, is required on board the modified aircraftThe ...
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·,,ELECTRONIC CABLE SPECIALISTS MASTER DATA LIST, REF. DOC. ECS-206919,REVISION E,...

·,,Electronic Cable Specialists Master Data List, ref. doc. ECS-206919,Revision E, dated 9th September 2008 (*)·,,Airplane Flight Manual Supplement, ref. doc. ECS-206922, RevisionN/C, dated 29th September 2008 (*)·,,Instructions for Continued Airworthiness Limitations: None. Conditions: 1.,,Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.2.,,The ins
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INSTALLATION OF AD AEROSPACE COCKPIT DOOR MONITORING SYSTEM LIMITATIONS: 1....

Installation of AD Aerospace Cockpit Door Monitoring System Limitations: 1. Prior to installation of this modification the installer must determine that the interrelationship between this modificationand any other previously installed modification will introduce no adverse effect upon the airworthiness of the produc. Conditions: n/a
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INSTALLATION OF ELECTRICAL AND MECHANICAL PROVISIONS FOR GLOBAL SYSTEM MOBILE...

Installation of electrical and mechanical provisions for Global System Mobile (GSM) equipment.
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INSTALLATION OF EZMOUNTTM ARM MECHANICAL MOUNTING ASSEMBLIES ON LOWER FRAME...

Installation of EZMountTM Arm mechanical mounting assemblies on lower frame of cockpit sliding windows.
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INSTALLATION OF ELECTRONIC FLIGHT BAG DATA AND POWER CONNECTORS WITH...

Installation of Electronic Flight Bag data and power connectors with associated aircraft wiring interface.
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INSTALLATION OF SATELLITE WEATHER ANTENNA STRUCTURAL PROVISIONS, COVER PLATE, AND...

Installation of satellite weather antenna structural provisions, cover plate, and coax cable provisions.
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INSTALLATION OF ELEMENTARY OR ENHANCED SURVEILLANCE MODE S TRANSPONDER IAW...

Installation of Elementary or Enhanced Surveillance Mode S Transponder iaw Electronic Cable Specialists Master Data List ECS-202128, rev. AB, 7 January 2008 or later approved revision. 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.. Conditions: n/a
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INSTALLATION OF ELEMENTARY OR ENHANCED SURVEILLANCE MODE S TRANSPONDERS. LIMITATIONS:...

Installation of elementary or Enhanced surveillance Mode S transponders. Limitations: 1. Only configurations 1, 2, 4, 5, 7, 8 and 9 as listed in the Master Data List ECS-203150, Revision P, are deemed to be approved; 2. The AFM Supplement as listed in Appendix A of Electronic Cable Specialists Master Data List ECS-203150, Revision P,. Conditions: n/a
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INSTALLATION OF A SMITHS INDUSTRIES FLIGHT MANAGEMENT SYSTEM DATA BUS...

Installation of a Smiths Industries Flight Management System Data Bus Portable Computing Device Recorder. 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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INSTALLATION OF A HONEYWELL KMH 880 MULTI- HAZARD AWARENESS SYSTEM...

Installation of a Honeywell KMH 880 Multi- Hazard Awareness System or a Honeywell KTA 870 Traffic Advisory System.
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INSTALLATION OF ELEMENTARY AND ENHANCED SURVEILLANCE MODE S TRANSPONDERS IN...

Installation of elementary and enhanced surveillance Mode S transponders In MD-11; MD-11F; DC-10-10; DC-10-15; DC10-30; DC 10-40; DC-10-10F; DC–10-30F; DC-10-40F in accordance with “Electronic Cables Specialists Master Data List ECS-203475”. Limitations: 1. ECS-203482 Rev. N/C AFM Supplement for McDonnell Douglas MD11 Series with Enhanced Mode-S Transponder Upgrade with Flight ID from Transponder Control Panel.2. ECS 204353 Rev N/C AFM Supplement for Douglas DC-10 Series Airplane with ...
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INSTALLATION OF SMITHS INDUSTRIES FLIGHT MANAGEMENT SYSTEM DATA BUS PORTABLE...

Installation of Smiths Industries Flight Management System Data Bus Portable Computing Device Recorder.
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INSTALLATION OF CONNEXION BY BOEING NEXT GENERATION ANTENNA AND SATELLITE...

Installation of Connexion by Boeing Next Generation Antenna and Satellite Data SystemNote: This Revision reflects the transfer of this STC from Flight Structures, Inc. to Star Aviation, Inc. Limitations: 11. Airworthiness Limitations Section of the Instruction for Continuous Airworthiness, document numbers R44-0403, revision B, dated 22nd July 2005 for -200 series, R44- 0218, revsion B, dated 20th October 2004 for - 300 series, or later FAA ...
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INSTALLATION OF ENHANCED MODE-S TRANSPONDER. LIMITATIONS: THE AIRPLANE FLIGHT MANUAL...

Installation of Enhanced Mode-S Transponder. Limitations: The Airplane Flight Manual Supplement as listed in Appendix A of Electronic Cable Specialists Master Data List, Document No. ECS-202463, Revision F, dated June 27, 2006, or later approved revision is required on board the modified aircraft.. Conditions: n/a
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INSTALLATION OF DUAL HONEYWELL HT9100 GNSS GPS NAVIGATION SYSTEM. LIMITATIONS:...

Installation of Dual Honeywell HT9100 GNSS GPS Navigation System. Limitations: 1. Limited to configuration III and IV.2. Compatibility of this design change with previously approved modifications must be determined by the installer.3. This STC is approved only for the product configuration as defined in the approved design d. Conditions: n/a
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INSTALLATION OF HONEYWELL MCS-6000 SATCOM SYSTEM LIMITATIONS: THIS INSTALLATION MUST...

Installation of Honeywell MCS-6000 SATCOM System Limitations: This installation must be installed in conjunction with Honeywell STC EASA.IM.A.S.02276 for the installation of the SATCOM High-Gain Antenna and Diplexer / Low Noise Amplifier (D/LNA).. Conditions: n/a
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FAA STC ST02316CH - ELEMENTARY AND ENHANCED MODE S. LIMITATIONS:...

FAA STC ST02316CH - Elementary and Enhanced Mode S. Limitations: Limited to configuration 3 of ECS MDL ECS- 203350 Rev. G dated July 7, 2006.This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraphs "Description" and “Associated Technical Documentation”.. Conditions: n/a
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INSTALLATION OF UNIVERSAL AVIONICS SYSTEMS CORPORATION TERRAIN AWARENESS AND WARNING...

Installation of Universal Avionics Systems Corporation Terrain Awareness and warning System (TAWS) Limitations: Aircraft Flight Manual Supplement ECS 202604, revision B, dated 11 October 2005 or later approved revisionInstruction for continued airworthiness ECS 202604, revision B, dated 5 December 2005If the holder agrees to permit another person to use this certifi. Conditions: n/a
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UPGRADE OF EXISTING MODE S TRANSPONDER INSTALLATION TO ADD ENHANCED...

Upgrade of existing Mode S transponder installation to add enhanced surveillance Mode S.
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INSTALLATION OF GPS ANTENNA PROVISIONS B747 SERIES IN ACCORDANCE WITH...

Installation of GPS Antenna Provisions B747 Series in accordance with ST01841CH Limitations: 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph 5Documentation. Compatibility with other aircraft/engine configurations shall be determined by the installer.2. The Boeing. Conditions: n/a
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INSTALLATION OF HONEYWELL ENHANCED GROUND PROXIMITY WARNING SYSTEM AND GPS...

Installation of Honeywell Enhanced Ground Proximity Warning System and GPS antenna structural provisions.
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INSTALLATION OF A HONEYWELL GROUND PROXIMITY WARNING SYSTEM IN ACCORDANCE...

Installation of a Honeywell Ground proximity Warning System in accordance with FAA STC ST01877CH Limitations: n/a. Conditions: n/a
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THE MODIFICATION WILL CONSIST OF A COMPOSITE STRUCTURE WITHA METAL...

The modification will consist of a composite structure witha metal faceplate wich will be fitted over the center of the existing Glareshield. An area of the existing glareshield will be removed to allow for wires to be routed to the annunciators and (...) Certification Basis Limitations Master Data List R25-0283 Rev. E, dated 17 January 2006AFM Supplement Doc. Nr. R25- 342, Rev. IR dated 24 November ...
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INSTALLATION OF A HONEYWELL ENHANCED GROUND PROXIMITY SYSTEM LIMITATIONS: NONE....

Installation of a Honeywell Enhanced Ground Proximity System Limitations: None. Conditions: n/a
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INSTALLATION OF GPS ANTENNA PROVISIONS IN ACCORDANCE WITH FAA STC...

Installation of GPS antenna provisions in accordance with FAA STC ST01887CH Limitations: The equipment for which these provisions are intended has not been certified. Additional EASA approval is required for the installation of this equipment. Conditions: n/a
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INSTALLATION OF HONEYWELL ENHANCED GROUND PROXIMITY WARNING SYSTEM AND HONEYWELL...

Installation of Honeywell Enhanced Ground Proximity Warning System and Honeywell Multi Function Radar Display.
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INSTALLATION OF UNIVERSAL AVIONICS SYSTEM CORPORATION MULTI-FUNCTION DISPLAY IN ACCORDANCE...

Installation of Universal Avionics system Corporation Multi-Function Display in accordance with Electronic Cable Specialists MasterData List ECS-2000416 rev. E dated 17.3.2003 Limitations: n/a. Conditions: n/a
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INSTALLATION OF ELEMENTARY & ENHANCED MODE S TRANSPONDERS LIMITATIONS: N/A....

Installation of elementary & enhanced Mode S Transponders Limitations: n/a. Conditions: n/a
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INSTALLATION OF A HONEYWELL KMH 880 MULTI-HAZARD AWARENESS SYSTEM OR...

Installation of a Honeywell KMH 880 Multi-Hazard Awareness System or a Honeywell KTA 870 Traffic Advisory System.
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SINGLE OR DUAL ARINC 743A GPS ANTENNA AND COAXIAL CABLE INSTALLATION

STC ST01060CH installs single or dual GPS antenna provisions, ARINC 743A GPS antennas and coaxial cables on 737-200/-300/-400/-500 series aircraft.   Please contact the factory for a complete list of available configurations and details of the kit content.
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INSTALLATION OF A SPECTRALUX DLINK AIRCRAFT COMMUNICATIONS ADDRESSING AND...

Installation of a Spectra Lux Dlink Aircraft Communications Addressing and Reporting System (ACARS).
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HONEYWELL MK V ENHANCED GROUND PROXIMITY WARNING SYSTEM (FAA STC...

Honeywell MK V Enhanced Ground Proximity Warning System (FAA STC ST01839CH) as per Master Data List ECS-201736 revision H dated 25 May 2004 or later FAA-approved revision. Limitations: 1. Subject to compliance with the provisions of Part 21 Subpart E, this STC and associated data shall remain valid until surrendered, withdrawn or otherwise terminated.2. If transfer of this Certificate is requested under Part 21A.116, the STC ...
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DUAL GPS ANTENNA AND COAX CABLE (FAA STC ST01449CH) AS...

Dual GPS Antenna and Coax Cable (FAA STC ST01449CH) as per Master Data List ECS- 200555 revision B dated June 11, 2003 or later FAA-approved revision. Limitations: 1. Subject to compliance with the provisions of Part 21 Subpart E, this STC and associated data shall remain valid until surrendered, withdrawn or otherwise terminated.2. If transfer of this Certificate is requested under Part 21A.116, the STC will ...
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INSTALLATION OF A UNIVERSAL AVIONICS SYSTEMS CORPORATION TERRAIN AWARENESS AND...

Installation of a Universal Avionics Systems Corporation Terrain Awareness and Warning System (TAWS).
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INSTALLATION OF A SPECTRA LUX AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING...

Installation of a Spectra Lux Aircraft Communications Addressing and Reporting System (ACARS).
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INSTALLATION OF A CONNEXION BY BOEING SATELLITE TV AND DATA...

Installation of a Connexion by Boeing Satellite TV and Data System per Star Aviation, Inc. Master Data List R-23-E04-0098, Rev F, dtd 2/3/03 or later FAA approved revision.
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INSTALLATION OF UNIVERSAL AVIONICS SYSTEM CORPORATION MULTI-FUNCTION DISPLAY.

Installation of Universal Avionics System Corporation Multi-Function Display.
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INSTALLATION OF DUAL HONEYWELL HT-9100 GPS FLIGHT MANAGEMENT SYSTEMS.

Installation of dual Honeywell HT-9100 GPS Flight Management Systems. The HT9100 Global Navigation Flight Management System is a lightweight state of the art navigation system designed for application on almost any analog or digital aircraft. This system brings internal GPS precision together with the function of current air transport flight management operations to provide direct operational benefit. With the standard configuration module, the same part number ...
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INSTALLATION OF IFE SMOKE DETECTION PROVISIONS AND VENTING SYSTEM.

Installation of IFE Smoke Detection Provisions and Venting System.
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INSTALLATION OF A HONEYWELL COMMUNICATIONS MANAGEMENT UNIT AND A VHF...

Installation of a Honeywell Communications Management Unit and a VHF communication system.
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INSTALLATION OF DUAL UNIVERSAL AVIONICS UNS-1K GPS FLIGHT MANAGEMENT SYSTEMS.

Installation of Dual Universal Avionics System Corporation UNS-1K GPS flight Management Systems.
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INSTALLATION OF AN ALLIEDSIGNAL CAS-81 TCAS II SYSTEM WITH DUAL...

Installation of an AlliedSignal CAS-81 TCAS II System with AlliedSignal Mode S Transponders.
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INSTALLATION OF AUTOMATIC DEPENDENT SURVEILLANCE-BROADCAST (ADS-B) PROVISIONS AND A SINGLE...

Installation of Automatic Dependent Surveillance-Broadcast (ADS-B) Provisions and a single Honeywell Mode-S transponder.
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INSTALLATION OF A DIGITAL FLIGHT DATA RECORDER (DFDR) SYSTEM UPGRADE.

Installation of a Digital Flight Data Recorder (DFDR) System Upgrade.
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INSTALLATION OF AUTOMATIC DEPENDENT SURVEILLANCE-BROADCAST (ADS-B) PROVISIONS AND DUAL HONEYWELL...

Installation of Automatic Dependent Surveillance-Broadcast (ADS-B) Provisions and Dual Honeywell or Collins Mode-S Transponders.
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INSTALLATION OF AUTOMATIC DEPENDENT SURVEILLANCE-BROADCAST (ADS-B) PROVISIONS AND DUAL HONEYWELL...

Installation of Automatic Dependent Surveillance-Broadcast (ADS-B) Provisions and Dual Honeywell or Collins Mode-S Transponders.
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INSTALLATION OF SINGLE AND DUAL HONEYWELL HT-9100 GNSS GPS NAVIGATION...

Installation of Single and Dual Honeywell HT-9100 GNSS GPS Navigation Systems with provisions for Single or Dual DME.
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