STC ListEASA STC no.STC HolderOld STC ref.Rev. levelForeign/NAA STC ref.ModelsDescriptionCertification basisLimitationsConditionsDate of IssueStatus100316371263343 ALBERTA INC DBA ENERJETTCCA STC C-LSA10-077/D ISSUE 1B737-700Bucher LH Windscreen /Closet ModificationThe Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRI H-01 Issue 1: Special Condition - EWIS ICAThe requirements for environmental protection and the associatedcertificated noise and/ oru...Modification Data Summary R1004821 issue A dated April 2010Modification Review Continued Airworthiness & Safety Improvement R1006846 issue A dated June 2010or later revisions of the above listed documents approved by EASA inaccordance withEASA ED Decision 2004/02/CF (or subsequent revisions ofthis...Limited to B737-700 aircraft S/N 33920Maintenance of the Bucher Closet is to be performed by Boeing AircraftMaintenanceManual D633A101-CQT, and Bucher Component MaintenanceManual 25-30-6501/09/2010Active100316381263343 ALBERTA INC DBA ENERJETTCCA STC C-LSA08-311/D ISSUEB737-700131, 137 & 145 Passenger Seating ReconfigurationThe Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRI H-01 Issue 1: Special Condition - EWIS ICAThe requirements for environmental protection and the associatedcertificated noise and/ oru...Modification Data Summary R0810701 issue C dated April 2010Modification Review Continued Airworthiness & Safety Improvement R1006845 issue A dated June 2010or later revisions of the above listed documents approved by EASA inaccordance with EASA ED Decision 2004/02/CF (or subsequent revisions o...Limited to B737-700 aircraft S/N 33920Maintenance of the Recaro seats are to be performed per Recaro ComponentMaintenance Manual 25-22-11, 25-25-81 and 25-24-7901/09/2010Active100316391263343 ALBERTA INC DBA ENERJETTCCA STC C-LSA08-310/D ISSUEB737-700Artex C406-2 ELT InstallationThe Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRI H-01 Issue 1: Special Condition - EWIS ICAThe requirements for environmental protection and the associatedcertificated noise and/ oru...-Modification Data Summary R0810709 issue A dated November 2008.-Modification Review Continued Airworthiness & Safety ImprovementR1006844 issue A dated June 2010.-Aircraft Maintenance Manual Supplement R0809001 issue A.-ARTEX Maintenance Manual 570-5000 rev B and 870-4010 Rev A.or later revisions of...Limited to B737-700 aircraft S/N 33920 and 3448002/09/2010Active100316401263343 ALBERTA INC DBA ENERJETTCCA STC C-LSA10-078/D ISSUEB737-700TIA Model 1545 oven Installation in forward LH monument.The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRI H-01 Issue 1: Special Condition - EWIS ICAThe requirements for environmental protection and the associatedcertificated noise and/ oru...Modification Data Summary R1004825 issue A dated April 2010Modification Review Continued Airworthiness & Safety Improvement R1006847 issue A dated June 2010or later revisions of the above listed documents approved by EASA inaccordance with EASA ED Decision 2004/04/CF (or subsequent revisions o...Limited to B737-700 aircraft S/N 33920Maintenance of the TIA Model 1545 Oven is to be performed per TIAComponent Maintenance Manual 25-30-6101/09/2010Active1006166221JAERODESIGN LIMITEDREV. 1A321-111/-112/-211/-212/-213 A320-211/-212/-214/-215/-216 A319-111/-112/-113/-114/-115 A318-111/-112Nacelle - CFM56-5A/5B Engines - Thrust Reverser - Replacement of adapterring outer flange segments Amendment of modellistingThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS 25.601, CS 25.603, CS 25.609, CS 25.613, CS 25.1529 at Amdt 18The requirements for environmental protectionand the associatedcertified noise and/ or emissions levels o...Design Change Document DCD-0001M, Issue 4, dated 19/05/2017or later revisions of the above listed documents approved byEASA.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.14/08/2017Active1006258321JAERODESIGN LIMITEDA319-111Introduction of Zero-passenger Seating ConfigurationThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS 25 Amendment 18:CS 25.25, CS 25.27, CS 25.601, CS 25.601, CS 25.785, CS 25.803,CS 25.813, CS 25.815, CS 25.817, CS 25.853, CS 25.1529, CS 25.1541The requirementsc...21JAerodesign Design Change Document No. DCD-0007M Issue 01None.11/07/2017Active100152002 EXCEL DESIGN LIMITEDEASA.A.S.03592A320-232A320 In Flight Entertainment IFE Upgrade Compliance Plan and Checklist, ref. ADC14/JN116, Issue3, dated 24th October 2008 Master Data List, ref. ADC17/JN116, Issue 2, dated 23rd October 2008 CAANZ Approved Flight Manual Supplement Airbus A320-232 Panasonic EFX IFEUpgrade, ref. TMA6012503, dated 4th September 2008 Decla...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 ofthe product.29/10/2008Active100152462 EXCEL DESIGN LIMITEDEASA.A.S.03683DA 42 M (RESTRICTED)Banbury Modification 001 - FLIR Installation.JN147 ADC17 Issue 5 Master Data List.1. 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 installation of this modification by third pe...07/11/2008Active100346412 EXCEL DESIGN LIMITEDREV. 5PA-31Introduction of Chin Mount and re-located Pitot tubes.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.- Master Document List S21.MDL-0825 Issue 10- Flight ManualSupplement S21.FMS-0072 Issue 5- Compliance Record S21.COMP-0825 Issue 5- Instructions for Continuing Airworthiness S21.TEC-0305 Issue 3or later revisions of the above listed documents approved by EASAFlight Manual Supplement S21.FMS-0072 Issue 5The installation and subsequent operation of a sensor turret requires aseparate approval.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change...25/08/2017Active100347142 EXCEL DESIGN LIMITEDREV. 4PA-31Introduction of enlarged window and sensor turret provisionsThe 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.Master Document List S21.MDL-0914 Issue 7Flight Manual Supplement S21.FMS-0077 Issue 4Compliance Record S21.COMP-0914 Issue 3Instructions for Continuing Airworthiness S21.TEC-0374Issue 2or later revisions of the above listed documents approved by EASA.With a sensor turret with diameter greater than 15.5" installed, flightinto known or forecast icing conditions is prohibited.Limitations as defined in AFMS S21.FMS-0077 Issue 4.The installation and subsequent operation of a sensor turret requires aseparate approval.Prior to installation of this modi...25/08/2017Active100347342 EXCEL DESIGN LIMITEDREV. 2PA-31Introduction of a Belly PodThe 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.- Master Document List S21.MDL-0915 Issue 3 dated 13/11/2012- Flight Manual Supplement S21.FMS-0080 Issue 2 dated 31/10/2012- Compliance Record S21.COMP-0915 Issue 2 dated 13/11/2012- Instructions for Continuing Airworthiness S21.TEC-0311 Issue 1 dated20/04/2011or later revisions of the above listed...Not to be flown in icing conditions with the belly pod installedLimitations as defined in AFMS S21.FMS-0080 Issue 2 dated 31/10/2012.Prior to installation of this design change itmust be determined thatthe interrelationship between this design change and any otherpreviously installed design changea...25/08/2017Active100406912 EXCEL DESIGN LIMITEDREV. 3PA-31Provisions for the installation of a Sensor TurretThe 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.- Master Document List S21.MDL-1027 Issue 6- Flight Manual Supplement S21.FMS-0091 Issue 4- Compliance Record S21.COMP-1027 Issue 4- Instructions for Continuing Airworthiness S21.TEC-0374 Issue 2or later revisions of the above listed documents approved by EASA.With a sensor turret with diameter greater then 15.5'' installed,flight into known or forecast icing conditions is prohibited.Limitations as defined in AFMS S21.FMS-0091 Issue 4The installation and subsequent operation of a sensor turret requires aseparate approval.Prior to installation of this mod...25/08/2017Active100431362 EXCEL DESIGN LIMITEDEASA.A.S.036S7DC-9-32110Y LOPA (Removal of one row of seats to improve access totype IIIexits to meet localretroactive requirements).Master Data List MDL/JN139, issue 1, dated 14 August 2008.1. Prior to installation of this modification the installermustdetermine that theinterrelationship between this modification and any other previouslyinstalledmodification will introduce no adverse effect upon the airworthiness oftheproduct. The installation of this modification by third persons iss...20/08/2008Active100482322 EXCEL DESIGN LIMITEDREV. 1PA-31Introduction of modified winglets.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.- Installation in accordance with STC21 Modification S21.57-90-1001,S21.MDL-1010, issue 1, dated February 21, 2014.- Operation in accordance with Flight Manual Supplement S21.FMS-0107Issue 1, dated February 21, 2014.- Instructions for Continued Airworthiness as defined in S21.TEC-0360,Issue 1, dated...As per Aeroplane Flight Manual Supplement S21.FMS-0107Design change S21.57-90-1002 must be installed prior to incorporation ofthis design change.The operation of the wingtip strobe lights in aircraft fitted only withwingtip strobe light needs further approval.Installation of role equipment onto thea...25/08/2017Active100580442 EXCEL DESIGN LIMITEDREV. 1B727-2S2F(RE)Introduction of an Oil Dispersant Fluid Storage and Delivery System(TERSUS), project JN491-005REV. 1: Addition of Rhodamine B and Kilfrost DF Plus fluids to TERSUSsystem, project 2XL061The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- Special Condition(s): CRI F-01 Issue 2, HIRF Protection- the following paragraph(s) at a later amendment: Asper CRI A-01 Issue2The requirements for environmental protec...- Leading Edge Modification Sheet JN491-005, report ref JN491-005LEF79(1) iss 1.- Leading Edge Certification Record 2XL061, report ref 2XL061 LEF79(1)iss 1.- Leading Edge Master Data List for Modification JN491-005, report refJN491-005 LEF78(1) issue 1. This identifies all reports raised by theAppli...This modification is applicable to aircraft serial numbers 22938 and22929.The AFM Supplement introduces operational limitations, i.p. an airspeedlimitation of 250KIAS/0.75M, an altitude limitation of FL360 and a MTOWreduction from 203,100lbs to 195,300lbs whenever the external boom isinstalled (refe...18/06/2018Active100584482 EXCEL DESIGN LIMITED727-200FFQIS Wiring Changes on Boeing 727The 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.Leading Edge Master Data List No. 2XL011 LEF78 Issue 1 dated 13 June2016None15/06/2016Active100602392 EXCEL DESIGN LIMITEDB300, B300C B200CT, B200GT, B200T B200, B200C, B200CGT 200, 200C, 200CT, 200TApproval of the Introduction of Standalone GPS Antenna on BeechcraftKing Air 200 and B200 all variants, under Leading Edge Modification ref2XL030, Issue 1, dated, 21 October 2016.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.Installation in accordance with Leading Edge Master DrawingList ref,2XL030 LEF78(1), Issue 1, dated, 21 October 2016 and InstallationInstructions ref, 2XL030 LEF49A(1), Issue 1.There is no AFMS associated to this Change.Instructions for Continued Airworthiness in accordance with documentref, 2XL03...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.28/11/2016Active100605052 EXCEL DESIGN LIMITED737-200Introduction of Honeywell TCAS 7.1 to Boeing 737This designchange entails the upgrade of the existing TCAS II processorVersion 7.0 to 7.1The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:Regulations at the amendment level: 14 CFR 25.1529Amdt 25-54.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of t...Leading Edge Aircraft Flight Manual Supplement, 2XL027 LEF71B (1) Issue3or later revisions of the above listed documents approved by EASA.Leading Edge Master Data List, 2XL027 LEF78(1) Issue 3.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.16/12/2016Active100618122 EXCEL DESIGN LIMITEDB200CT, B200T 200, 200C, 200CT, 200TIntroduction of antennas and pressure hull feed through provisions andinstallationsThe 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.To be installed according to documents in Master data list in 2XL019LEF78(1) Issue 1 dated 26th April 2017;To be maintained according to Instructions for Continued Airworthiness2XL019 LEF73(1) Issue 1 ICA dated 14th December 2016.No AFM Supplement is issued with this STC.or later revisions of the ab...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.09/05/2017Active100620952 EXCEL DESIGN LIMITEDREV. 1PA-31Transfer of EASA STC No. 10062095 for Activation of Wi-Fi for SATCOMSystem including Swift Broadband from STC Twenty One Ltd to 2ExcelDesign Ltd.The Certification Basis (CB) for the original product remains applicableto this certificate/ approval. The requirementsfor environmentalprotection and the associated certified noise and/ or emissions levelsof the original product are unchanged and remain applicable to thiscertificate/ approval.STC Twenty One Ltd Flight Manual Supplement S21.FMS-0130 Issue 2 dated 8December 2016or later revisions of the above listed documents approved by EASA.STC Twenty One Ltd Master Document List S21.MDL-1294 Issue 3Applicable to aircraft serial number 31-7400984 only.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and anyotherpreviously installed design change and/ or repair willintroduce noadverse effect upon the airworthiness of the pro...27/04/2018Active100621932 EXCEL DESIGN LIMITEDB200CT, B200T 200, 200C, 200CT, 200TIntroduction of Leading Edge Applications Pod (LEAP) provisions andinstallation.The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.This certificate/approval involves a change to the requirements forenvironmental protection or a change to the certified noise or emissionslevels.To be installed according to documents in Master data list in 2XL020LEF78(1) Issue 2 dated 13th June 2017;To be maintained according to Instructions for Continued Airworthiness2XL020 LEF73(1) Issue 1 ICA dated 13th June 2017;To be operatedaccording to AFM supplement 2XL020 LEF71B(1) issue dated13th...- The following EASA STC shall be installed: 10030124, 10016599;- Propeller Hartzell HC-D4N-3A/D9383K (as per EASA STC 10031275) shallbe installed;- Engine PT6A-41 (Pratt & Whitney Canada) shall be installed;- The LEAP installation is designed to withstand (within the designenvelope of this STC) a m...14/06/2017Active10014074328 DESIGN GmbHEASA.A.S.01166REV. 1JETSTREAM 3200 SERIES JETSTREAM 3100 SERIESInstallation of Airborne Collision Avoidance System (ACASII).This certificate follows EASA.A.S.01166 due to a transfer of ownership.-Avionics Mobile Services Definition Document Part 21-002/1485-01 Issue 1 or later approved revision-Avionics Mobile Services AFM Supplement Part 21-008/011 Issue 1 or later approved revisionThis STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10014139328 DESIGN GmbHEASA.A.S.01252REV. 1550 AND 650Installation of an Airborne Collision Avoidance System (ACAS II).This certificate follows EASA.A.S.01252 due to a transfer of ownership.Avionics Mobile Services Project Certification Plan AM/1493. Avionics Mobile Services AFM Supplement Number Part21-008/008.This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10014184328 DESIGN GmbHEASA.IM.A.S.01322REV. 1HAWKER 800XP (BAE 125-800)Installation of an Airborne Collision Avoidance System (ACAS II).This certificate follows EASA.IM.A.S.01322 due to a transfer ofownership.Avionics Mobile Services Project Certification Plan AM/1498 ReferencePART21-003/1498-01 or later approved revision.Avionics Mobile Services AFM Supplement reference AFM PART21-008 Issue 2or later approved revision.This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10014198328 DESIGN GmbHEASA.A.S.01341REV. 1HAWKER 800XP (BAE 125-800)Installation of an Airborne Collision Avoidance System (ACAS II).This certificate follows EASA.A.S.01341 due to a transfer of ownership.Avionics Mobile Services Project Certification Plan AM/1498Reference PART21-003/1498-01 or later approved revision.Avionics Mobile Services ARM Supplement reference ARM PART21-008 Issue 2 or later approved revision.This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10014215328 DESIGN GmbHEASA.A.S.01376REV. 1550 AND 560Avionics Mobile Services Modification AM/1478. Installationof anAirborne Collision Avoidance System (ACAS II).This certificate follows EASA.A.S.01376 due to a transfer of ownership.-Avionics Mobile Services Ltd Project Certification Plan AM/1478 reference PART21-003/1478-01-Avionics Mobile Services Ltd AFM Supplement PART21-008/008 dated April 08 2005 or later approved revisionThis STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10014303328 DESIGN GmbHEASA.A.S.01547REV. 1PA-31T2 (CHEYENNE IIXL)Certification of FAA Approved field modifications for the issue of anEASA C of A.Avionics Mobile Services AFM supplement Part 21-008 014 GNS-530.Avionics Mobile Services AFM supplement Part 21-008 015 KMH-880.Avionics Mobile Services AFM supplement Part 21-, 008 016 SN3308.This certificate follows...This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10014431328 DESIGN GmbHEASA.A.S.02479REV. 11124AInstallation of Airborne Collision Avoidance System (ACAS II).This certificate follows EASA.A.S.02479 due to a transferof ownership.Avionics Mobile Services Modification AM/1486.Avionics Mobile Services AFM Supplement No. PART21-008/017 Revision - dated April 08 2005 or later approved revision.This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10014480328 DESIGN GmbHEASA.A.S.02543REV. 3HS 125-700 SERIESInstallation of an Airborne Collision Avoidance System (ACASII).This certificate follows EASA.A.S.02543 due to a transfer of ownership.Avionics Mobile Services Limited Modification AM/1517Avionics Mobile Services Limited AFM Supplements ref. PART21-008/018Issue 1 or later approved revision & PART21-008/001 Issue 1 or laterapproved revision.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 be determined by the installer.11/03/2013Active10014481328 DESIGN GmbHEASA.A.S.02544REV. 1HS 125-700 SERIESInstallation of a Digital Air Data Display System.This certificate follows EASA.A.S.02544 due to a transfer of ownership.Avionics Mobile Services Modification AM/1518Avionics Mobile Services AFM Supplement PART21-008/019 Issue 1 or later approved revisionThis STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.11/03/2013Active10015249328 DESIGN GmbHEASA.A.S.03688REV. 1JETSTREAM 4100 SERIESMode-S Enhanced Surveillance (EHS) UpgradeCertification Program AM1577003A-01Instructions for Continued Airworthiness AM1557007A-01Flight Manual Supplement AM1557008A-01Prior 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 installation of this modification by third persons...15/04/2013Active10015654328 DESIGN GmbHEASA.IM.A.S.0163REV. 2HS.125 SERIES 700A/BInstallation of a Rockwell Collins TCAS-4000 Traffic Alert and CollisionAvoidance System (TCAS-II)This certificate follows EASA.IM.A.S.0163 due to a transfer ofownership.Avionics Mobile Services Limited modification AM/1469Avionics Mobile Services Limited AFM Supplement, reference:PART21-008/001 or later approved revisionThis 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 be determined by the installer.11/03/2013Active10015663328 DESIGN GmbHEASA.IM.A.S.0164REV. 2HS 125-700 SERIESInstallation of a Ground Proximity Warning System (GPWS) and TerrainAwareness Warning System (TAWS).This certificate follows EASA.IM.A.S.0164 due to a transfer ofownership.Avionics Mobile Services Limited modification AM/1470Avionics Mobile Services Limited AFM Supplement, reference: PART21-008/006 or later approved revisionThis 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 be determined by the installer.11/03/2013Active10031570328 DESIGN GmbHEASA.A.S.03968REV. 1DORNIER 328-100, 328-300Installation of Emergency Lighting Power Supply SystemThe Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRI H-01/SpecialCondition H-01 "Enhanced Airworthiness Programme forAeroplane Systems - ICA on EWIS"The requirements for environmental p...Master Document List - AM1561010A-01 Issue 2 dated 16 AUG 2010AFM Supplement - AM1561008A-01 Issue 1Instructions for Continued Airworthiness - AM1561007A Issue Aor later revisionsof the above listed documents approved by EASANone15/04/2013Active10036511328 DESIGN GmbHREV. 2800XP, 850XPInstallation of a Flight Data Recorder (FDR) System.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.Installation in accordance with 328 Design GmbH EngineeringOrder refAM1581009A-01 Issue B, dated 16.12.2014Operation in accordance with 328 Design GmbH Aircraft Flight ManualSupplement ref AM1581008A-01, dated Dec 16, 2014Instructions forContinued airworthiness in accordance with 328 DesignGmbH IC...None.17/12/2014Active10043118328 DESIGN GmbHEASA.A.S.01322REV. 1CN-235-100Installation of a Ground Proximity Warning System (GPWS) & TerrainAwareness Warning System (TAWS).This certificate follows EASA.A.S.01322 due to a transfer of ownership.Avionics Mobile Services Definition Document PART21-002/1504-01, Issue1, dated September 9, 2005 or later approved revision.Avionics Mobile Services AFM Supplement PART21-008-012,Revision 1 orlater approved revision.1. Aircraft Registrations A40-CU and A40-CV.2. This STC is approved only for the product configuration as defined intheapproved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurationsshall bedetermined by the installer.11/03/2013Active10043137328 DESIGN GmbH2003-2150REV. 1JETSTREAM 4100 SERIESInstallation of Honeywell MK VI Enhanced Ground Proximity WarningSystem. STC CAA.21NE2.00044.This STC follows the EASA approval letter 2150 of December 2003 due to atransfer of ownership.11/03/2013Active10043139328 DESIGN GmbH2004-2293REV. 1BAE.125 SERIES 800BInstallation of a Honeywell Airborne Collision Avoidance System (ACASII).This STC follows EASA approval letter 2004-2293 due to a transfer ofownership.11/03/2013Active10043140328 DESIGN GmbH2004-5548REV. 1DORNIER 328-100Installation of a Honeywell MK VI Enhanced Ground ProximityWarningSystem (EGPWS).This STC follows EASA approval letter2004-5548 due to a transfer ofownership.STC Definition Document PART21-003/1459-01.11/03/2013Active10044141328 DESIGN GmbHCL-600-2B19Cabin Modification to VIP.The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- the following paragraph(s) at a later amendment:CS 25.1701 to CS 25.1729 at Amendment 11.The requirements for environmental protection and the associatedcertified noiseu...Declaration of Compliance, Doc. No. DC-10D003Z0001, Issue Bdated20.03.2013;Master Document List, Doc. No. MDL003Z0001,Issue A dated 19.03.2013;Instructions for Continued Airworthiness, Doc. No. ICA010D259Z0001,Issue A dated 19.03.2013;AFM Supplement, Doc. No. AFMS010D043Z0001, Initial Release date...Aircraft Serial Number 7617 only.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverseeffect upon the airworthiness of the product.20/03/2013Active10044717328 DESIGN GmbHREV.1.GIVCabin Refurbishment with LOPA Change, Cabin Lighting, CabinPower SupplySystem, and new In-Flight Entertainment.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.Installation in accordance with 328DO Engineering Order EO-16H259Z0001and Master Data List ref MDL002Z001 Issue A dated29 April 2013.Operate in accordance with 328DO Flight Manual Supplement refAFM016H043Z0001 Initial Release, dated 29 April 2013.Maintain in accordance with 328DO ICA ref ICA016H259...Aircraft Serial 1027.30/04/2013Active10046552328 DESIGN GmbHCL 604 VARIANTCabin refurbishment Incl LOPA changeThe 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.328 Design Master Document List No. MDL006Z001 Issue A dated 25September 2013.or later revisions of the above listed documents approved by EASA.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.30/09/2013Active10048621328 DESIGN GmbHF900EXSeat Change on Dassault Falcon 900EX SN096The 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.Master Document List ref. MDL016Z001 issue B, dated 26/03/2014.or later revisions of the above listed documents approved by EASA.Applicability limited to Falcon 900EX SN096.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness of the product.26/03/2014Active10048622328 DESIGN GmbHF900EXCabin Refurbishment with replacement of CMS / IFE and CabinLighting onDassault Falcon 900EX SN096.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.Master Document List ref. MDL017Z001 issue A, dated 21/03/2014.or later revisions of the above listed documents approved by EASA.Applicability limited to Falcon 900EX SN096Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introducenoadverse effect upon the airworthiness of the product.26/03/2014Active10050209328 DESIGN GmbHBD-700-1A10Cabin refurbishment including LED Cabin lighting installation.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.328 Design Master Document List No. MDL021Z001 Issue A dated 08 August2014.Restricted to ASN 9083.13/08/2014Active10051291328 DESIGN GmbHREV. 1A318-111/-112Installation of Chelton Swift Broad Band (SBB) Satcom system, includingcabin WiFi router for passenger's high speed internet connection usageonly.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.- Master Document List, 328 Design GmbH document No. MDL027Z001,Revision B, dated 19 November 2014- Airplane Flight Manual Supplement, 328 Design GmbH document No.AFM018H043Z0001,Revision A, dated 19 November 2014- Instructions For Continued Airworthiness, 328 Design GmbH document No.ICA018H231Z000...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.28/11/2014Active10052358328 DESIGN GmbHMF 50EXInterior Modification and In-Flight Entertainment System upgradeThe 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.-Master Document List, 328 Design GmbH document No. MDL043Z001, RevisionA, dated 19 February 2015.-Airplane Flight Manual Supplement, 328 Design GmbH document No.AFMS020C043Z001, Revision A, dated 2 February 2015.or later revisions of the above listed documents approved by EASA.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.19/02/2015Active10054441328 DESIGN GmbHCL-600-2E25 (RJ SERIES 1000) CL-600-2D24 (RJ SERIES 900) CL-600-2D15 (RJ SERIES 705) CL-600-2C10 (RJ 700/701/702) CL-600-2B19 (RJ SERIES 100) CL-600-2B16 (604 VARIANT) CL-600-2B16 (601-3R VARIANT) CL-600-2B16 (601-3A VARIANT) CL-600-2A12 (601 VARIANT) CL-600-1A11 (600)TCAS Change 7.1 UpgradeThe 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.328 Design GmbH Aircraft Flight manual Supplement No.HBKAFMS010C344Z0001 Issue Aor later revisions of the above listed documents approved by EASA328 Design GmbH Master Document List No. MDL076Z0001 Issue A.None17/08/2015Active10055322328 DESIGN GmbHHAWKER 1000BACSS TCAS Change 7.1 UpgradeTCAS II Change 7.1 Upgrade withP/N 4066010-914TCAS 2000 RT-951 Change 7.1 Upgrade with P/N7517900-55020The Certification Basis (CB) for the original product remains applicableto this certificate/ approval. The requirementsfor environmentalprotection and the associated certified noise and/ or emissions levelsof the original product are unchanged and remain applicable to thiscertificate/ approval328 Design GmbHAFM supplement AFMS022B344Z0002 Issue A released 29 Oct. 2015 for TCASIIAFM supplement AFMS022B344Z0001 Issue A released 18 Sept. 2015 for TCAS2000 Change 7.1or later revisions of the above listed documents approved by EASA.Master Data List MDL079Z001 Issue C from 30 Oct. 2015Declarat...The approval is limited to TCAS II Change 7.1 Upgrade with computer P/N4066010-914 and TCAS 2000 RT-951 Change 7.1 Upgrade with computer P/N7517900-55020Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously inst...30/10/2015Active10055745328 DESIGN GmbHDORNIER 228-212 DORNIER 228-202 DORNIER 228-201 DORNIER 228-200 DORNIER 228-101 DORNIER 228-100Approval of TCAS Change 7.1 software upgrade.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.Installation in accordance with 328 Design modification DC-12A032Z0001Issue A, dated 25.11.2015 and MDL ref MDL083Z001 Issue A, dated25.11.2015.Operate in accordance with 328 Design Flight Manual Supplement refAFMS012A344Z0001 Rev A, dated21.11.2015.or later revisions of the above listed documents...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.01/12/2015Active10055850328 DESIGN GmbHJETSTREAM SERIES 3200 JETSTREAM SERIES 3100TCAS II Change 7.1 SW Upgrade for British Aerospace (BAe) Jetstream 3100/ 3200 SeriesThe 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.AFMS026B34Z0001CP-26B084Z0001_ADC-26B084Z0001GTR026B344Z0001_SN857MDL084Z001None08/12/2015Active10058644328 DESIGN GmbHEMB-135LR EMB-135BJ/ EMB-135ERReplacement of cockpit displays DU-870 with DU-875 on EMBRAER 135 SeriesAircraft.The Certification Basis (CB) for the original product remains applicableto this certificate/ approval. The requirementsfor environmentalprotection and the associated certified noise and/ or emissions levelsof the original product are unchanged and remain applicable to thiscertificate/ approval.Master Document List, document N MDL095Z001 Issue A dated 24.06.2016or later revisions of the above listed documents approved by EASA.None.07/07/2016Active10060149328 DESIGN GmbHDORNIER 328-100Empty Cabin Layout, Project No. 099The 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.Master Document List MDL099Z001 Iss. B dated 18.11.2016Declaration of Compliance DC-12B099Z0001 Iss. B dated 18.11.2016Compliance Statements CS-12B099Z0001 Iss. A dated 25.10.2016A/C Flight Manual Supplement AFMS012B099Z0001 Iss. B dated 15.11.2016,,or later revisions of the above listed documents a...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.22/11/2016Active10062897328 DESIGN GmbHGULFSTREAM 200/GALAXYADS-B OUT on RC Pro Line 4 (G-200).The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:Deviation(s):CRI F-01, Continuity Requirements for ADS-B function.The following paragraph(s) at a later amendment:CS-ACNS, Initial Issue:CS ACNS.D.ADSB.001, C...Master Document List (MDL), Document No. MDL113Z001, Rev. A.AFM Supplement, Document No. AFMS016C345Z001, Rev. B.MMEL Supplement, Document No. MMELS016C345Z000, Rev. Aor later revisions of the above listed documents approved by EASA.Limited to S/N 062 and up.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effectupon the airworthiness of the product.16/08/2017Active10064470328 SUPPORT SERVICES GmbHREV. 1FALCON 900EX (F900EX)CMS/IFE, SatCom & LED Cabin Lighting.This STC installs the following cabin system: Rockwell Collins VenueCMS/IFE System, True North Optelity Pro Iridium Phone System,Mid-Continent universal AC Cabin Outlets with dual USB Charger, B/EAerospace cabin Up-wash and Downwash LED Lighting and B/E Aeros...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.- Master Document List No.MDL118Z001, Revision B, dated 24th January2018;- Airplane Flight Manual Supplement Document No AFMS020E043Z0001,Revision A, dated 15th January 2018;- Instructions for Continued Airworthiness Document No.:AMMS020E043Z0001 Revision: A, dated 18th January 2018;or later revisio...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.24/01/2018Active10064604328 SUPPORT SERVICES GmbHGULFSTREAM G150ADS-B OUT - Rockwell Collins Pro Line 21 Avionics on GULFSTREAM 150.The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- Deviation(s): CRI F-01, Continuity Requirements for ADS-B function.- The following paragraph(s) at a later amendment: CS-ACNS, InitialIssue:CS ACNS.D.ADSB.001, CS ACNS.D...Master Document List (MDL), Document No. MDL128Z001, Rev. B;AFM Supplement, Document No. AFMS016B345Z0001, Rev. B;MMEL Supplement, Document No. MMELS016B345Z0001, Rev. B;or later revisions of the above listed documents approved by EASA.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.08/02/2018Active10065118328 SUPPORT SERVICES GmbHREV. 1750Installation of modifications for introduce ADS-B Out capability onCessna Citation X aircraft equipped with Primus II Radio Suites.The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:the following paragraph(s) at a later amendment: CS-ACNS, Initial Issue,dated 19.12.2013.The requirements for environmental protection and the associatedcertified noise an...Installation in accordance with 328 Design Master Document List ref MDL139Z001 Rev B dated 03 May 2018.Operate in accordance with 328 Design Airplane Flight Manual Supplementref AFMS024K345Z001 Rev B dated 03 May 2018.There is no ICA associated with this STC, refer to Cessna ICA and AMMor later revi...Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product.04/05/2018Active10065308328 SUPPORT SERVICES GmbHHAWKER 900XP HAWKER 800XP, HAWKER 850XP,Swift Broadband SBB Satcom with WiFi.The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:the following paragraph(s) at a later amendment: 14CFR Part 25,Amendment 25-1 through 25-97The requirements for environmental protection and the associatedcertified noiseu...Installation according to Master Document List MDL138Z001 Issue B, dated19/04/2018Operation according to Aircraft Flight Manual SupplementAFMS022A231Z0001 Issue A, dated 04/04/2018Maintenance according to Aircraft Maintenance Manual SupplementAMMS022A231Z0001 Issue A, dated 04/04/2018or later revisi...Limited to aircraft with Rockwell Collins Proline 21 avionics suiteinstalled.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffect upon the airwort...23/04/2018Active10065511328 SUPPORT SERVICES GmbHBD-700-1A10, BD-700-1A11Replacement of Honeywell DU-870 display units with DU-875 Elite withbasic functions.This supplemental type certificate (STC) installation consists ofreplacement of the existing Honeywell cockpit display units DU-870 (CRTmodel) with DU-875 (Part Number K9321060A13-03 and Software variantV01.10.01) on...The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:the following paragraph(s) at a later amendment: CS 25.1316 and 25.1317at amendment level 21.The requirements for environmental protection and the associatedcertified nois...328 Support Services GmbHs Master Document List MDL 109Z001 Issue A,dated 07th May 2018or later revisions of the abovelisted document(s) approved under theEASA system.This supplemental type certificate (STC) installation consists ofreplacement of the existing Honeywell cockpit display units DU-870 (CRTmodel) with DU-875 (Part Number K9321060A13-03 and Software variantV01.10.01) on Bombardier BD-700 series aircrafts equipped with HoneywellPrimus 2000XP avionics su...14/05/2018Active10014371365 AEROSPACE LTDEASA.A.S.01645REV. 2737-600/-700/-800/-900/-900ERInstallation of an Enhanced Surveillance Mode S SystemThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS 25 Amendment 1225.869, 25.1301, 25.1307, 25.1309, 25.1321, 25.1333, 25.1351, 25.1353,25.1355, 25.1357, 25.1431, 25.1529, 25.1581, 25.1701, 25.1703, 25.1705,25.1707, 25....Aerospace Design & Engineering ConsultantsAFM Supplement 1 FMA-0014-001 Issue AAerospace Design & Engineering ConsultantsFlight Manual Supplement FMA- 1370-083 Revision 1or later revisions of the above listed documents approvedby EASA.Aerospace Design & Engineering Consultants Mod...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.07/07/2016Active10014405365 AEROSPACE LTDEASA.A.S.01700REV. 1737-200/-300/-400/-500/-600Installation of Dual High Frequency (HF) Communications SystemThe 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.Aerospace Design & Engineering Consultants Modification SummaryMOD-0001 Revision B dated 16th May 2007Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.07/07/2016Active10014460365 AEROSPACE LTDEASA.A.S.02518REV. 3737-300, 737-400, 737-500Installation of an Enhanced Surveillance Mode S System / Installation ofnew Mode S Transponders, components and data link wiring whichwill provide the ATC System with additional parameters necessary tocomply with TGL N 18 Revision 1, dated August 3, 2003.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.Aerospace Design & Engineering Consultants Flight ManualSupplement FMA-0031 Issue 1or later revisions of the above listed documents approved by EASA.Aerospace Design &Engineering Consultants Modification SummaryMOD- 0031 IssueA dated 21st February 2006Aerospace Design & Engineeri...This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph Description.Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this design change it must be determined thatt...14/07/2016Active10015297365 AEROSPACE LTDEASA.A.S.03847REV. 4A321-212/-213/-231/-232 A321-111/-112/-131/-211 A320-215/-216/-231/-232/-233 A320-111/-211/-212/-214 A319-115/-131/-132/-133 A319/-111/-112/-113/-114 A318-111/-112/-121/-122Installation of an Enhanced Surveillance Mode S SystemThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS 25 Amendment 1225.869, 25.1301, 25.1307, 25.1309, 25.1321, 25.1333, 25.1351, 25.1353,25.1355, 25.1357, 25.1431, 25.1529, 25.1581, 25.1701, 25.1703, 25.1705,25.1707, 25....Aerospace Design & Engineering Consultants Flight ManualSupplement FMA- 0544-062 Revision 1 dated 13th March 2009Aerospace Design & Engineering Consultants Flight ManualSupplement FMA- 1374-085 Revision 1Aerospace Design & Engineering Consultants Flight ManualSupplement FMA- 1374-0...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.14/07/2016Active10029548365 AEROSPACE LTDREV. 2737-600/-700/-800/-900Introduction of a Dual Battery SystemThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:Special Conditions:CRI H-01 Issue 2 / Special Condition H-01 Enhanced AirworthinessProgramme for Aeroplane Systems ICA on EWISThe requirements for environmental protec...Aerospace Design & Engineering Consultants Modification SummaryMOD- 0702 Revision C dated 22nd March 2010Aerospace Design & Engineering Consultants EZA-0702 Revision Adated 10th November 2011The STC holder shall monitor all documentary changes of thebasic AFMand related operational documentation issued by the TC-holder to assurethat those documents remain suitable tobe used operationally for theinstallation of dual batteriesunder this STC.Prior to installation of this design change i...07/07/2016Active10032318365 AEROSPACE LTDREV. 1DHC-8-401, DHC-8-402Installation of Ground Recognition LightsThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS-25 Amendment 8 for changed areasThe requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunch...Aerospace Design & Engineering Consultants Ltd Aircraft ManualSupplement No. AMS-DHC-8-Q 400-FLYBE, dated 01 August 2010or later revisions of the above listed documents approved by EASA.Aerospace Design & Engineering Consultants Ltd ModificationSummary, MOD-0753, Revisi...Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.07/07/2016Active10044229365 AEROSPACE LTDREV. 1767-200/-300/-300F/-400ERIntroduction of Controller-Pilot Data-Link CommunicationsThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:Special Conditions:CRI F-01 Data Link Services forthe Single European SkyCS-25 Amendment 1225.601, 25.611, 25.899, 25.1301, 25.1302, 25.1307, 25.1309, 25.1321,25.1322, 25...Aerospace Design & Engineering Consultants Ltd Flight Manual SupplementFMA-1282-084 Revision 1or later revisions of theabove listed documents approved by EASA.Aerospace Design & Engineering Consultants Ltd Modification SummaryMOD-1282 Revision APrior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.07/07/2016Active10046805365 AEROSPACE LTDREV. 1767-300767-300 Condor Cabin LED Lighting UpgradeThe 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.AERODEC Modification Summary No. MOD-1338 Revision A,dated 24thOctober 2013Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.03/06/2015Active10048649365 AEROSPACE LTDREV. 1737-600/-700/-800/-900/-900ERIntroduction of Controller-Pilot Data-Link CommunicationsThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CRI F-01 Data Link Services for the Single European Sky.CRI F-02 Flight Recorders including Data Link RecordingThe requirements for environmental protection and the associ...AERODEC Flight Manual Amendment FMA-1446-106 Revision 1or later revisions of the above listed documents approved by EASA.AERODEC Modification Summary No. MOD-1446 Revision A, dated 26thMarch 2014ACARS OPC Software must be installed on the Digital Electronic Unit(DEU) for correct annunciation.Prior to installationof this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadv...02/06/2015Active10053928365 AEROSPACE LTDCL-600-2B16 CL-600-2A12 CL-600-1A11SATCOM Antenna InstallationThe 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.365 Aerospace Ltd MDL-0024 Revision A dated 02 July 2015None03/07/2015Active10054305365 AEROSPACE LTDREV. 1757-200Installation of a Controller Pilot Data Link Communications(CPDLC)SystemRev. 1: corrects Limitations on this certificateThe Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS 25 Amendment 1525.301, 25.303, 25.305, 25.307, 25.365,25.561, 25.571, 25.581, 25.601, 25.603,25.605, 2...-365 Aerospace Ltd Flight Manual Supplement No. 1, FMS-0006-001Issue 3 to B757 Flight Manual Reference No. D631N005-365 Aerospace Ltd Instructions for Continued Airworthiness,paragraph 4.2 Airworthiness Limitations, ICA-0006-001 Revision Bdated 27 July 2017or later revisions of the...1. Boeing 757-200 aircraft must have skin configuration 143N3121-4 atthe GPS antenna location as defined by Boeing drawing 143N3121.2. Each Boeing 757-200 aircraft, by serial number, must have a specificDeclaration of Design and Performance document calling up the necessaryEmteq documents.Prior to i...14/08/2017Active10059766365 AEROSPACE LTDCL-600-1A11/ -2A12/ -2B16Change for the introduction of Satellite Communications System (SATCOM)and Cabin Local Area Network (WI-FI).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.365 Aerospace Ltd Flight Manual Supplement No.1 FMS-0074-001 REVISION A.365 Aerospace Ltd Instructions for Continued Airworthiness ICA-0074-001Issue 3or later revisions of the above listed documents approved by EASA.365 Aerospace Ltd MDL-0074 Revision A dated 12 October 2016.None.13/10/2016Active10061156365 AEROSPACE LTDS-76CInstallation of Nginuity DAQ9000 as an alternate Flight Data AcquisitionUnit (FDAU)The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS-29 Amdt. 3:29.251, 29.1301, 29.1309, 29.1351, 29.1353, 29.1357, 29.1459, 29.1529,29.1541, A29.1, A29.2, A29.3, A29.4The requirements for environmental protection and th...Airworthiness Limitations as per Section 4.2. of the Instructions forContinued Airworthiness ICA-0182-001, Rev Aor later revisions of the above listed documents approved by EASA.-Engineering Order EO-0182-001, Rev A- Certification Plan CCP-0182, Rev C- Instructions for Continued Airworthiness ICA-0...This STC requires as a pre-requisite the installation of Major ChangeEASA.IM.R.C.01404, dated 13 September 2006.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will i...02/03/2017Active10061170365 AEROSPACE LTD737-800 737-700Change to introduce a 189Y LOPA and recline installation onto Weber C100seatsThe 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.365 Aerospace Ltd Master Data List No. MDL-0237 Revision A dated 20February 2017None03/03/2017Active10061389365 AEROSPACE LTDATR42-500Change to introduce a Zero Pax Configuration.The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:The following paragraph(s) at a later amendment: CS25 Amendment 18:25.29, 25.301, 25.303, 25.305, 25.307,25.601, 25.785, 25.789