EASA STC no. STC holder

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10029091 (ATL) AVIATION TRADERS LIMITED P-EASA.A.S.03891 B747-400 Introduction of changes to the cabin layout in accordance with ATLModification Summary MOD-11427-00001Part A: introduces a seating configuration of 22 business class and 440economy classPart B: introduces all emergency equipment necessary to comply (...) The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalThe certificationbasis is CS25 at change 4 for changed parts except forthe following re (...) EASA AFM supplement 11427-AFM-0001 Issue 1, Installation ofPhoto-luminescent Aisle Path Marking System, shall be used with theaircraftInstructions for Continues Airworthiness included in ATL Mod SummaryMOD11427-00001 Issue 4 shall be incorporated in (...) None 03.03.2010 10029662 (ATL) AVIATION TRADERS LIMITED P-EASA.A.S.03876 B737-300 Business Interior - 48 PAX LOPA The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalCRI H-01/Special Condition H-01 "Enhanced Airworthiness Programme forAeroplane Systems (...) - Modification Summary Sheet: MOD-11348- 00001 Issue 2 dated30 March2010- Master Document List MDL-11348-00001 Issue 2 dated 29 March 2010- Airplane Flight Manual Supplement 11348-AFM-00001 issue 2;or later revisions of the above listed documents approved by EASA The STC holder shall provide by 7th June 2010 Instructions for ContinuedAirworthiness on Electrical Wiring Interconnection System - EWIS ICA -in accordance with Special Condition H-01 "Enhanced AirworthinessProgramme for Aeroplane Systems - ICA on E (...) 09.04.2010 10029965 (ATL) AVIATION TRADERS LIMITED B757-200 Boeing 757-200 229Y Passenger Configuration The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalCRI H-01/Special Condition H-01 "Enhanced Airworthiness Programme forAeroplane Systems - ICA on EWIS" -ATL Modification Summary Sheet, Doc. No. MOD-11682-00001, Issue 3 dated6th May 2010-ATL Master Document List, Doc. No.MDL-11682-00001, Issue 3 dated 5thMay 2010or later revisions of the above listed documents approved by EASA As per associated Technical documentation for weight and balance(maximum allowable limit in the forward and aft cargo area is to beamended as per indicated in doc. N° MOD- 11682-00001, Issue 3).Limited to: MSN 27973 07.05.2010 10031637 1263343 ALBERTA INC DBA ENERJET TCCA STC C-LSA10-077/D ISSUE 1 B737-700 Bucher LH Windscreen /Closet Modification 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 prote (...) 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 De (...) 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 25-30-65 01.09.2010 10031638 1263343 ALBERTA INC DBA ENERJET TCCA STC C-LSA08-311/D ISSUE B737-700 131, 137 <(>&<)> 145 Passenger Seating Reconfiguration 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 prote (...) 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 EAS (...) 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 25-24-79 01.09.2010 10031639 1263343 ALBERTA INC DBA ENERJET TCCA STC C-LSA08-310/D ISSUE B737-700 Artex C406-2 ELT Installation 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 prote (...) -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- (...) Limited to B737-700 aircraft S/N 33920 and 34480 02.09.2010 10031640 1263343 ALBERTA INC DBA ENERJET TCCA STC C-LSA10-078/D ISSUE B737-700 TIA 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 prote (...) 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 EAS (...) Limited to B737-700 aircraft S/N 33920Maintenance of the TIA Model 1545 Oven is to be performed per TIAComponent Maintenance Manual 25-30-61 01.09.2010 10014074 328 DESIGN GMBH EASA.A.S.01166 REV. 1 BAE JETSTREAM 31 BAE JETSTREAM 32 Installation 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 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. 11.03.2013 10014139 328 DESIGN GMBH EASA.A.S.01252 REV. 1 CESSNA 550 CESSNA 650 Installation 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. 11.03.2013 10014184 328 DESIGN GMBH EASA.IM.A.S.01322 REV. 1 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. 11.03.2013 10014198 328 DESIGN GMBH EASA.A.S.01341 REV. 1 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. 11.03.2013 10014215 328 DESIGN GMBH EASA.A.S.01376 REV. 1 CESSNA 550 SERIES CESSNA 560 SERIES Avionics 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 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. 11.03.2013 21/10/2013 Page 1/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10014303 328 DESIGN GMBH EASA.A.S.01547 REV. 1 PIPER PA-31T2 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 (...) 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. 11.03.2013 10014431 328 DESIGN GMBH EASA.A.S.02479 REV. 1 1124A WESTWIND II Installation 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. 11.03.2013 10014480 328 DESIGN GMBH EASA.A.S.02543 REV. 3 HS 125-700 SERIES Installation 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. 11.03.2013 10014481 328 DESIGN GMBH EASA.A.S.02544 REV. 1 HS 125-700 SERIES Installation 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 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. 11.03.2013 10015249 328 DESIGN GMBH EASA.A.S.03688 REV. 1 BAE JETSTREAM 41 Mode-S Enhanced Surveillance (EHS) Upgrade Certification Program AM1577003A- 01Instructions for Continued Airworthiness AM1557007A-01Flight Manual Supplement AM1557008A-01 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 (...) 15.04.2013 10015654 328 DESIGN GMBH EASA.IM.A.S.0163 REV. 2 HS 125-700 SERIES Installation 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 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. 11.03.2013 10015663 328 DESIGN GMBH EASA.IM.A.S.0164 REV. 2 HS 125-700 SERIES Installation 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 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. 11.03.2013 10031570 328 DESIGN GMBH P-EASA.A.S.03968 REV. 1 DORNIER 328-100, 328-300 Installation of Emergency Lighting Power Supply System The 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 (...) 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 EASA None 15.04.2013 10036511 328 DESIGN GMBH REV. 1 HAWKER 800XP Installation of a Flight Data Recorder (FDR) System. 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. Installation in accordance with Avionics Mobile Design ServicesEngineering Order ref AM1581009A-01 Issue A dated 05 August 2011.Operation in accordance with Avionics Mobile DesignServices AircraftFlight Manual Supplement ref AM1581008A-01, dated, Ju (...) None. 15.04.2013 10043118 328 DESIGN GMBH EASA.A.S.01322 REV. 1 CN-235M-100 SERIES Installation 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. 11.03.2013 10043137 328 DESIGN GMBH 2003-2150 REV. 1 BAE JETSTREAM 31 Installation 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. 11.03.2013 10043139 328 DESIGN GMBH 2004-2293 REV. 1 BAE 125-800B Installation of a Honeywell Airborne Collision Avoidance System (ACASII).This STC follows EASA approval letter 2004-2293 due to a transfer ofownership. 11.03.2013 10043140 328 DESIGN GMBH 2004-5548 REV. 1 DORNIER 328-100 Installation 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. 11.03.2013 21/10/2013 Page 2/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10044141 328 DESIGN GMBH CL-600-2B19 Cabin 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 environme (...) 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 (...) 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. 20.03.2013 10044717 328 DESIGN GMBH REV.1. GIV Cabin 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.Ma (...) Aircraft Serial 1027. 30.04.2013 10046552 328 DESIGN GMBH CL 604 VARIANT Cabin refurbishment Incl LOPA change 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. 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. 30.09.2013 10014424 A&M AVIONICS, SL EASA.A.S.02469 PIPER PA-31-350 Verification of the B-RNAV Capability.Installation of GPS Modes Panel Annunciator.Installation of new XPDR Mode S Garmin GTX-330 and Encoder AK-350. A&M Avionics PC No. 02/2006 Rev. 0, dated 30/11/2005. In accordance with Supplement No. SMV 02/06 R0, to the original Flight Manual approved by FAA.SN 31-7952088 21.12.2007 10014434 A&M AVIONICS, SL EASA.A.S.02483 CESSNA 404 Remove Weather Radar Bendix King RDS81. Install Weather Radar Bendix King DRD 2000 with MFD Avidyne EX 500. Reinvestigation of DualGNS530 Installation according to A&M Avionics BINº 017/2006 for B-RNAV Approval, Model: Cessna 404, S/N 404 0614 ¿ Design Definition A&M Doc. DDI Nº 03/06 Rev.1¿ New Supplements to Aircraft Fligth Manual A&M Avionics Doc. SMV Nº 03/06 Rev.1 and A&M Avionics Doc. SMV Nº 04/06 Rev.1¿ Operating & Service Instructions: A&M Avionics Doc. BI Nº 24/05 Rev.0 1. The design changes to be approved are only applicableto Cessna 404 airplanes with Dual GNS530 Installation according to A&M Avionics BI Nº 017/2006, and EHSI SANDEL SN 3500previously installed and approved as Primary Navigation Display.2. P (...) 30.01.2009 10014788 A&M AVIONICS, SL EASA.A.S.02988 FAIRCHILD SWEARINGEN SA 226- TC Installation of New Avionics Equipment.Transponders Mode S Filser Electronics TRT800H. New Supplement to Aircraft Flight ManualA&M Avionics Document SMV 01/07 R0.Operating & Service InstructionsA&M AvionicsEngineering Bulletin BI 02/07 R0. 08.10.2007 10014877 A&M AVIONICS, SL EASA.A.S.03104 CESSNA 500 Installation of New Avionics Equipement.Transponder Mode S GARMIN GTX-330D. New Supplement to Aircraft Flight Manual A&M Avionics Doucment SMV N° 08/07 RO.Operating & Service Instructions A&M Avionics Engineering Bulletin BI N° 08/07 RO. 05.02.2008 10043289 A&M AVIONICS, SL EASA.A.S.03339 REV. 1 PA-34-200 Installation of Dual COM/NAV/GPS GARMIN GNS 430 & GNS 530 The Certification Basis for the original product remains applicable tothis certificate/ approval. Technical Documents to be Approved by EASA:- SERVICE BULLETIN BI Nº: 19/07 R1- SMV Nº 19/07 R1, Airplane Flight Manual Supplement for IFR operationswith Dual Garmin GNS 530 & Garmin GNS 430. or later revisions of the above listed documentsapproved by EASA Approval limited to Airplane Model PA-34- 200, S/N 34-7250309 19.02.2013 10046100 A&M AVIONICS, SL T310R Installation of Dual System Garmin GNS530W in accordance withInstallation Bulletin BI 05/13 Other: 14 CFR Part 23 according to Certification Programme PC & MCU05/13The requirements for environmental protection and the associatedcertified noise and/ or emissions levels ofthe original product areunchanged and remain applicable to this certificate/ approval. Installation Bulletin A<(>&<)>M Avionics IB 05/13Supplementto AFM A<(>&<)>M Avionics SMV 05/13or later revisions of the above listed documents approved by EASA Approval limited to Airplane CESSNA T310R, S/N 310R-1408Prior 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 introd (...) 14.08.2013 10032066 A.I.M.S. INTERNATIONAL Corp. FAA ST02675AT BD-700-1A10 Sound Reduction Kit EASA IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approvalThe requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areuncha (...) FAA SoC dated 30 September 2010.FAA STC No. ST02675AT dated22 April 2004.AIMS International Corp engineering top- leveldrawing 53G2521522 Rev I/Rdated 15 March 2003 and installation instruction document No.AIMS-INST-1 Rev I/R dated 16 April 2003 or l (...) None 06.10.2010 10045364 A.S. AVIONICS SERVICES LTDA. EMB-135BJ Installation of IWG-A4 Potable Water Treatment Unit on EMB-135BJEASA validation of ANAC STC 2012S09-08 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 Drawing List ref. EMB135BJ-38- 0001MD, Rev. D, dated 11/09/2012.Certification Plan ref. EMB135BJ- 38- 0001CP, Rev.B, dated 07/03/2012;supplemented by EASA Declaration of Compliance ref.EMB135BJ-38- 0001EASA-DC, Rev. Original, dated 20/02/2013.In (...) Applicable to EMB-135BJ S/N 14500997, 14501029 and onPrior 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 n (...) 19.06.2013 10044063 A/C SYSTEMS L.L.C. FAA STC SA03065CH-D G58, 58, 58A, D055, E55, E55A Installation of an A/C Systems Air- conditioning 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 Standard Aero Master Drawing List1021376 Rev (I), dated 20 April 2012.Operation in accordance with FAA Approved Airplane Flight ManualSupplement number FTA-010-6 Rev (IR) dated 23 April 2012.Maintain in accordance wit (...) The installer must determine whether this design change is compatiblewith previously approved modifications.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviousl (...) 14.03.2013 21/10/2013 Page 3/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10044069 A/C SYSTEMS L.L.C. FAA STC SA00257BO 1- G36 2- F33A, A36 Installation of an A/C Systems Air- conditioning 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 A/C Systems Master Drawing ListFTA-000-1 Rev C, dated 07 June 2012;Operation in accordance with FAA Approved Airplane Flight ManualSupplement number FTA-010-2 Rev (I) dated 25 April 2012;Maintain in accordance with A/ (...) Model F33A Applicability Serials CE-748, CE- 772 and after.Model A36 Applicability Serials E1111, E-1241 through E-3635,excludingE- 3630.Model G36 All Serials.The installer must determine whether this design change is compatiblewith previously approve (...) 15.03.2013 10015780 AAE LTD EASA.IM.A.S.01826 REV. 1 FAA STC ST01114WI BOEING 737 CLASSIC SERIES Installation of Smoke Detection and Fire Suppression System AAE Ltd. Master Drawing List TFA10-0061, Revision H, dated 01 December 2005 or later approved revision.AFM Supplement ref. TFA09-0063, TFA09-0064, TFA09-0065, TFA09-0066 dated 20 November 2002, TFA09-0085, TFA09-0086 dated 29 June 2005, TFA09-0088, (...) 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. 26.11.2002 10015840 AAE LTD EASA.IM.A.S.01934 FAA STC ST03001AT FOKKER F.28 MARK 0100 Smoke detection and Fire Suppression System for lower Deck Class C Cargo Compartments of Fokker F100 Series Aircraft 1. TFA 18-0179 Instructions for Continued Airworthiness2. TFA 10-0062 Master Drawing List3. TFA 18-0178 Structural Substantiation Report4. TFA 18-0134 Alteration Cettification Plan5. TFA 18-0180 Weight Information Report6. TFA 18-0183 Alteration Com (...) 1. AAE, Ltd. Document TFA09-0087, Revision IR, dated January 14, 2005 "FAA approved Airplane Flight Manual Supplement for the Class"C" Cargo Compartment Smoke Detection and Fire Suppression System on the Fokker F.28 Mark 0100 Series Aircraft" 25.09.2006 10043324 AAE LTD EASA.IM.A.S.03172 REV. 1 FAA STC ST01077WI A320 Installation of AAE's smoke detection and fire suppression System in thelower Class C Cargo compartments. - FAA STC STOlO77WI- Master Drawing List, ref. doc. TFAlO-0057, Revision U, dated 11thMarch 2009 *- Airplane Flight manual Supplement ref. doc. TFA09-0062/ doc.TFA09-0088/ doc. TFA09-0089, Revision IR, dated 4th November 2008*- Instructionfor Contin (...) 1. Prior to installation of this modification the installermustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.2. The (...) 23.06.2009 10040411 AAR AIRCRAFT SERVICES FAA STC ST03119CH B717-200 Interior Reconfiguration EASA.IM.A.211The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) FAA STC No. ST03119CH dated 25 June 2012.AAR Engineering Services Master Data List ERP 11-062 Revision C dated 23June 2012.Instructions for Continued Airworthiness (ICA), AAR Aircraft ServicesReport No. ERP 11-068 Revision IR, dated 28 March 2012.or (...) None 02.07.2012 10015931 AAR AIRCRAFT SERVICES INC.- INDIANAP EASA.IM.A.S.02068 SA7467SW FOKKER F.27 Installation of dual freon air conditioning systems in accordance with AAR Oklahoma, Inc., Drawing List 19L002, Revision F, dated July 19, 1988, or later FAA approved revision. AAR Oklahoma, Inc., Drawing List 19L002, Revision F, dated July 19, 1988, or later FAA approved revision. 1. FAA approved flight manual supplement dated August 10, 1988, is required.2. Compatibility of this modification with previously installed equipment must be determined by installer. 13.10.2006 10015627 AAR CARGO SYSTEMS EASA.IM.A.S.01579 REV. 1 FAA STC ST02021CH MD-11 Installation of a Main Deck Cargo Handling System (FAA STC ST02021CH) The Certification Basis for the original product remains applicable tothis certificate/ approval AAR Report 1826 Instruction for Continued Airworthiness None 10.12.2010 10028433 AAR CARGO SYSTEMS P- EASA.IM.A.S.03180 FAA STC ST02767CH B767-300 Install Main Deck Cargo Loading System The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificateCertification basis is as defined in EASA STC 10028430The certificated noise and/ or emissions le (...) Drawing List Report Number 3255, Revision C, 30/09/2009Applicable revisionsor later revisions of the above listed documents approved by EASA inaccordance with EASA ED Decision 2004/04/CF (or subsequent revisions ofthis decision) To be installed on a/c converted by IAI Freighter Conversion (EASA STC10028430) 08.01.2010 10040510 AAR CARGO SYSTEMS REV. 1 FAA STC ST02665CH A300B4-601, A300B4-603 A300B4-605 R, A300B4-620 A300B4-622, A300B4-622 R Validation of FAA Supplemental Type Certificate (STC) ST02665CHInstall a Main Deck Cargo Loading System (AAR Part Number 58535-101) onAirbus A300-600 series aeroplanes in accordance with AAR Master DrawingList Report Number 2149 Revision B, dated 15 December 2008. 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. AAR Weight & Balance Report A300-600 FSI Main Deck Cargo Loading System(MDCLS) P/N 58535-101 No.2147 Rev.A, dated 25 Aug. 2008.AAR Instructions For Continued Airworthiness A300-600 FSI MDCLS P/N58535-101 No.2148 original issue, dated 16 July 2007.or (...) none 13.07.2012 10016873 AAR COMPOSITES, INC. EASA.IM.R.S.01249 FAA STC SR01934LA SIKORSKY S-92A Installation of Partial Search and Rescue Interior Configuration. Install in accordance with AAR Composites Master Data List SAR-620-010, Revision M dated 1/31/2007, or later approved revisions.Maintenance in accordance with AAR Composites Document Number AAR- ER-1169, Sikorsky S-92A SAR Search and Rescue (SAR) In (...) No passengers permitted in the main cabin until the complete interior arrangement has been EASA or cognizant National AirworthinessAuthority approved. 07.05.2007 10016932 AAR COMPOSITES, INC. EASA.IM.R.S.01318 FAA STC SR03370AT SIKORSKY S-92A Structural provisions for a composite ramp floor panel. Install in accordance with AAR Composites Master Data List SRP-620-010, Revision B dated 18 December 2006, or later approved revisions.Maintenance in accordance with AAR Composites Document Number AAR- ER-1180, Revision A, dated December 7,2006 or later approved revision. MDL items under this STC meet Part 29.853. The installer isresponsible for panel sealant and all fasteners as well as for structural provisions to the aircraft ramp door. User must not exceed the maximum load per surface area of the ramp panel as specified by the TC holder. 07.05.2007 10017082 AAR COMPOSITES, INC. EASA.IM.R.S.01540 FAA STC NO. SR03077 AT SIKORSKY S-92A S-92A Structural Provisions for a Composite Passenger CabinVIP Interior. # S92-620-011 revision L dated 22 February 2008 or laterapproved revision # Master Document List# AAR-ER-1116 revision E dated 25 January 2008 or later approved revision # Instructions for Continued Airworthiness# AAR-ER-1264 revision IR da (...) 1. The installer is responsible for the addition of decorative finish to continue to comply with JAR 29.853.AAR bulkheads are for interior partitions only and are not intended means of compliance for cargo or smoke retention that the installer mu (...) 23.04.2009 21/10/2013 Page 4/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10015303 AB LUFTFAHRTTECHNIK BERLIN GMBH EASA.A.S.03868 AIRBUS A319-112 Change of the Cabin Configuration (150 Pax)/The cabin configuration will be changed to increase the certified 145pax configuration to a 150 pax configuration with minimum CabinCrew of 3 Flight Attendants # Certification Report, ref. doc. A319-CR25- 03-2009, Issue 1, dated 17th March 2009# Design Modification Document, ref. doc. A319-DMD25-03-2009, Issue 1, dated 17th March 2009# Compliance Record Document, Issue 2, dated 5th May 2009 1. Prior to installation of this modification the installermust determine that the interrelationship between this modificationand any other previously installed modification will introduce no adverse effect upon the airworthiness of the (...) 05.05.2009 10013958 ACC COLUMBIA JET SERVICE GMBH EASA.A.S.00516 REV. 1 BOMBARDIER CL-600-2B16 (604) Installation of an Artex ELT C406-1 Master Document List CL604-40163-000-S- LP 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. 19.01.2005 10014138 ACC COLUMBIA JET SERVICE GMBH EASA.A.S.01249 LEARJET 35 LEARJET 35A Installation of Honeywell MST-67A dual Mode S XPDR/CAS-67A TCAS II System. - ACC Master Document List ACC-LR35- 50096, revision 0, or later EASA-approved revisions.- ACC AFMS LR35-50096-820-S- MF,Revision 0, or later EASA-approved revisions.- ACC AFMS LR35-50096-830-S- MF, Revision 0, or later EASA-approved revisions. 28.04.2005 10014160 ACC COLUMBIA JET SERVICE GMBH EASA.A.S.01292 FOKKER F.27 MARK 500 Installation of an ARTEX ELT C406-1/-2 26.07.2005 10014764 ACC COLUMBIA JET SERVICE GMBH EASA.A.S.02954 LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A Installation of Honeywell EGPWS Mk. VIII(in combination with an existing Weather Redar display) Master Document List LR35-60514-000-LP, rev. 1AFM Supplement LR35-60514-800-MF, rev. 1 None 02.03.2007 10017178 ACC COLUMBIA JET SERVICE GMBH EASA.R.S.01296 EUROCOPTER DEUTSCHLAND EC-135- Installation of a HeliMap.MIDI.P0252 Moving Map System - Rotorcraft Flight Manual Supplement P1, P2, T1, (CDS, CPDS), EC 135-69008-800-S- MF Rev. 0 - Instructions for Continued Airworthiness EC 135-69008-810-S-MM Rev. 0 19.09.2006 10017179 ACC COLUMBIA JET SERVICE GMBH EASA.R.S.01297 EUROCOPTER DEUTSCHLAND MBB-BK Installation of a HeliMap MIDI.P0252 Moving Map System - Rotorcraft Flight Manual Supplement BK117 B-2, BK 117-69007-800-S-MF - Instructions for Continued Airworthiness BK117-69007-810-S-MM 19.09.2006 10017213 ACC COLUMBIA JET SERVICE GMBH EASA.R.S.01369 EUROCOPTER DEUTSCHLAND MBB-BK Installation of an EAE Heli.Map.MDI.P0252 system with extension box (for advisory only).Installation of a moving map system into BK117B-2 and BK117C-1 models. Rotorcraft Flight Manual Supplement Eurocopter BK117B-2/C-1ACC-BK117-79003- 800-S-MF Rev. 1, dated 31.05.2007.Instructions for Continued Airworthiness ACC-BK117-79003-810-S-MM Rev.0, dated 03.04.2007. 14.06.2007 10034112 ACC COLUMBIA JET SERVICE GMBH CL-600-2B16, CL-600-2B19 Installation of a combined IRIDIUM-GPS Antenna as provisionof anoptional Sky Tracking System. EASA IM-A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) ACC Master Document List ACC-CRJ200- 09016 Revision 0 dated 24 February2011.ACC ICA CRJ200-09016-810- MM Revision 0 dated29 November 2010.or later revisions of the above listed documents approved by EASA. None 08.03.2011 10014653 ACI SYSTEMES EASA.A.S.02810 BEECH 200 ATC replacement and Mode S installation. ACI S007/2006AFMS No ACI 05 AFM S007 Revision 0 or later approved revision AFMS must be on board when modified 07.05.2007 10014737 ACI SYSTEMES EASA.A.S.02920 CESSNA 550 Single pilot operation and associated modifications AFM Supplement ACI-00-AFM-M-021-Rev. 1Compliance Checklist ACI-00-CCL-M-021- Rev. 3, dated 05/06/2007 06.06.2007 10014902 ACI SYSTEMES EASA.A.S.03137 REIMS AVIATION CESSNA F 406 ACI-024 - Universal UNS-1L Installation - B- RNAV and P-RNAVCapability. Flight Manual Supplement ACI-10-AFM-M- 024-Rev3, Dated 14 September 2007. F406 equipped with KCP220 Allied Signal AutoPilot. 10.10.2007 10014905 ACI SYSTEMES EASA.A.S.03140 REIMS AVIATION CESSNA F 406 ACI-030 - Installation of an NAT NTX138 - FM Communication device. - 08.10.2007 10014996 ACI SYSTEMES EASA.A.S.03293 BEECH 90 GNS 430 and B-RNAV capability on Beech 90 AFM Supplement ACI-09-AFM-M-047-Rev0 N/A 18.02.2008 10015003 ACI SYSTEMES EASA.A.S.03303 FALCON 50 FALCON 900 Falcon 50 and F900 EHS Mode S Capability AFM Supplement ACI-05-AFM-M-033- Rev0ACI-05-TD-M-033-Rev0 Applicability for Falcon 50 and F900 which are already ModeA, C and ELS Mode S certified, ACAS certified and equipped with a dual transponder system. 29.10.2007 10015016 ACI SYSTEMES EASA.A.S.03320 CESSNA 550 ACI-045 - DFDR Upgrade. AFM Supplement ACI-12-AFM-M-045-Rev. 1Maintenance Manual Supplement ACI-12- MPS-M-045-Rev.0. This STC is only applicable to aircraft equipped with Fairchild F800 FDR. 16.05.2008 10015075 ACI SYSTEMES EASA.A.S.03406 BEECH 200 BEECH 300 Installation of a Garmin 400 Series with B- RNAV capability on Beech 200. 05.02.2008 10015099 ACI SYSTEMES EASA.A.S.03441 BEECH 90 Installation of Garmin 500 Series GPS with B- RNAV capability on Beech 90. ACI-09-AFM-M-070, Revision 0, dated 15 January 2008Modification file ACI-09-TD-M- 070, Revision 0, dated 15 January 2008. The supplemental Airplane Flight Manual ACI- 09-AFM-M-070, revision 0, dated 15 January 2008 must be on board when the modification is installed. 04.04.2008 10016968 ACROHELIPRO GLOBAL SERVICES, INC EASA.IM.R.S.01369 FAA STC SR02292AK BELL 206 BELL 206A BELL 206B BELL 206L BELL 206L-1 BELL 206L-3 BELL 206L-4 Sagem ICDS and Crossbow AHRS Installation. Consists of two 8 inch integrated cockpit display units (one PFD and one MFD) including engine instruments and an attitude and heading reference system. This STC is classified as "BASIC" by the FAA and is a (...) HP 206-34-33-102 # Certification Data List # revision A dated 3 July 2007 or later approved revision;HP 206-34-33-251 -Instructions for Continued Airworthiness - revision N/C dated 3 February 2007 or later approved revision;Addendum to ICA HP 206-34 (...) Maximum ambient operating temperature of 40 degrees Celsius(103 degrees Fahrenheit) 31.10.2007 21/10/2013 Page 5/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10016665 ACS-NAI Ltd. EASA.IM.A.S.03135 REV. 1 TCCA LSTC C-LSA09-031/D ISS. 2 BOMBARDIER CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. TCCA LSTC No. C-LSA09-031/D Issue 2 dated 17 June 2013.AeroConsulting Services Ltd. Modification Data Summary G120000 RevisionH.Midcoast Aviation Inc. Airplane Flight Manual Supplement for theComplete Custom Aircraft Interior Installation, 33- 299M00 (...) Restricted to ASN 8088.Prior to installation of this modification the installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. 16.08.2013 10016669 ACS-NAI Ltd. EASA.IM.A.S.03151 REV. 1 LSTC C-LSA09-009/D ISSUE 2 CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. Transport Canada LSTC C-LSA09-009/D Issue 2 dated 28 September 2012.Aero Consulting Services Ltd. Modification Data Summary G099000 Rev E.Midcoast Aviation Inc. Flight Manual Supplement 33-299M006 Rev NC.or later revisions of the above listed docume (...) Restricted to ASN 8081.Prior to installation of this designchange 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. 24.05.2013 10026769 ACS-NAI Ltd. P- EASA.IM.A.S.03137 REV. 1 TCCA LSTC C-LSA09-026, ISS. 1 CL-600-2B19 Installation, Complete Custom Aircraft Interior 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 TCCA LSTC No. C-LSA09-026 Issue 1 dated 04 August 2009.AeroConsulting Services Ltd. Modification Data Summary G103000 RevisionG.Midcoast Aviation Inc./ Aero Consulting Services Ltd Airplane FlightManual Supplement for the Complete Custom Aircraft In (...) Restricted to ASN 8079. 16.08.2013 10026840 ACS-NAI Ltd. REV. 1 TCCA LSTC C-LSA09-028/D, ISS.1 BOMBARDIER CL-600-2B19 Installation, Complete Custom Aircraft Interior. 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. TCCA LSTC No. C-LSA09-028/D Issue 1 dated 04 August 2009.Aero Consulting Services Ltd. Modification Data Summary G100000 RevisionE.Midcoast Aviation Inc/Aero Consulting Services Ltd Airplane FlightManual Supplement for the Complete Custom Aircraft I (...) Restricted to ASN 8070.Prior to installation of this designchange 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. 16.08.2013 10026904 ACS-NAI Ltd. P- EASA.IM.A.S.03136 REV. 1 TCCA LSTC C-LSA09-032/D BOMBARDIER CL-600-2B19 Installation, Complete Custom Aircraft Interior. 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. TCCA LSTC No. C-LSA09-032/D Issue 1 dated 12 August 2009.Aero Consulting Services Ltd. Modification Data Summary G121000 RevisionD.Midcoast Aviation Inc Airplane Flight Manual Supplement for the CompleteCustom Aircraft Interior Installation, 33-299M (...) Restricted to ASN 8089.Prior to installation of this designchange 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. 16.08.2013 10027086 ACS-NAI Ltd. P- EASA.IM.A.S.03165 REV. 2 TCCA LSTC NO. C-LSA09-033/D CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. TCCA LSTC No. C-LSA09-033/D Issue 2 dated 24 September 2010.Aero Consulting Services Ltd. Modification Data Summary G122000 RevisionF.Midcoast Aviation Inc Airplane Flight Manual Supplement for the CompleteCustom Aircraft Interior Installation, 33-2 (...) Restricted to ASN 8085.Prior to installation of this designchange 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. 16.08.2013 10028761 ACS-NAI Ltd. P- EASA.IM.A.S.03154 REV. 1 TCCA LSTC C-LSA09-004D, ISS. 2 BOMBARDIER CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. TCCA LSTC No. C-LSA09-004D Issue 2 dated 22 July 2009.Aero Consulting Services Ltd. Modification Data Summary G115000 RevisionB.Savannah Air Center Inc. Airplane Flight Manual Supplement for theComplete Custom Aircraft Interior, G115090 Revision A, (...) Restricted to ASN 8083. 16.08.2013 10028762 ACS-NAI Ltd. P- EASA.IM.A.S.03131 REV. 1 TCCA LSTC NO. C-LSA09-023/D BOMBARDIER CL-600-2B19 Installation, Complete Custom Aircraft Interior. 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. TCCA LSTC No. C-LSA09-023/D Issue 1 dated 02 July 2009.AeroConsulting Services Ltd. Modification Data Summary G098000 RevisionD.Midcoast Aviation inc. Airplane Flight Manual Supplement for theComplete Custom Aircraft Interior Installation, 33- 299M00 (...) Restricted to ASN 8065.Prior to installation of this designchange 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. 16.08.2013 10028763 ACS-NAI Ltd. P- EASA.IM.A.S.03134 REV. 1 TCCA LSTC NO. C-LSA09-030/D BOMBARDIER CL-600-2B19 Installation, Complete Custom Aircraft Interior. 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. TCCA LSTC No. C-LSA09-030/D Issue 2 dated 21 July 2009.AeroConsulting Services Ltd. Modification Data Summary G119000 RevisionC.Midcoast Aviation Inc. Airplane Flight Manual Supplement for theComplete Custom Aircraft Interior Installation, 33- 299M01 (...) Restricted to ASN 8078.Prior to installation of this designchange 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. 16.08.2013 10031149 ACS-NAI Ltd. TCCA STC SA10-26 CL-600-2B19 Installation, CMC Electronics Pilot view Class II Electronics Flight Bag EASA.IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The certificated noise and/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval. TCCA SoC ref. C-10-0364 dated 20 July 2010.TCCA STC ref. SA10-26 Issue 1 dated 19 March 2010.ACS-NAI Ltd Modification Data Summary Number G370000 Revision A.Savannah Air Center Airplane Flight Manual Supplement for Class 2Electronic FlightBag (EFB), (...) None 29.07.2010 21/10/2013 Page 6/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10031944 ACS-NAI Ltd. TCCA STC #C-LSA10-034/D ISS 1 BD-700-1A10 Installation of Two 16G Side Facing Divans EASA TCDS No EASA.IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approvalThe requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original pro (...) Transport Canada SoC ref. C-10-0708 dated 22 September 2010.Transport Canada STC No. C-LSA10-034/D Issue 1 dated 16 August 2010.ACS-NAI Ltd. Modification Data Summary Number G471000 Revision NC orlater approved revision. Refer to drawings listed in (...) Restricted to ASN 9347 23.09.2010 10032295 ACS-NAI Ltd. EASA.IM.A.S.03152 REV. 2 TCCA STC C-LSA09-021/D ISS.3 CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. TCCA STC No. C-LSA09-021/D Issue 3 dated 17 June 2013.ACS-NAI Ltd. Modification Data Summary G116000 Revision F.Aero Consulting Services Ltd. Mandatory Maintenance Manual SupplementG116070 Revision NC.Savannah Air Center Inc. Airplane Flight Manual (...) Restricted to ASN 8080 16.08.2013 10032519 ACS-NAI Ltd. TCCA STC NO. SA10-25 DHC-8-401, DHC-8-402 Installation of LED Lavatory Light System JAR/CS-25 as per EASA.IM.A.191The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.plus:Special Condition H-01 "Enhanced Airworthiness Prog (...) Installation must be in accordance with ACS- NAI Ltd. TCCA approvedModification Data Summary Number E 998000, Rev. N/CMaintenance must be in accordance with Instructions for ContinuedAirworthiness E 998071, Rev. A, E 998073 Rev. A andE 998074, (...) none 12.11.2010 10032736 ACS-NAI Ltd. EASA.IM.A.S.03130 REV. 2 TCCA LSTC C-LSA09-024/D, ISS.3 BOMBARDIER CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. TCCA LSTC No. C-LSA09-024/D Issue 3 dated 20 October 2010.Aero Consulting Services Ltd. Modification Data Summary G102000 RevisionG.Midcoast Aviation Inc. Airplane Flight Manual Supplement for theComplete Custom Aircraft Interior Installation, 33-29 (...) Restricted to ASN 8077.Prior to installation of this designchange 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. 16.08.2013 10033800 ACS-NAI Ltd. TCCA STC NO.C-LSA11-040/D BD700-1A11 Cabin Modifications for Wheelchair Access EASA.IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) TCCA SoC ref. C-10-1061 dated 08 February 2011TCCA STC No.C-LSA11-040/D Issue 1 dated 02 February 2011ACS-NAI Ltd. Modification Data Summary G950000 Revision NC or laterapprovedrevisionor later revisions of the above listed documents approved by E (...) Restricted to ASN 9373.Previous embodiment of EASA STC No. 10031088 (TCCA STC SA05-60). 09.02.2011 10034703 ACS-NAI Ltd. REV. 1 TCCA STC SA07-40 PC-12/45, PC-12/47, PC-12/47E Installation Utility DoorExisting Cargo door modified to incorporate a utility door (990 mm highby 635 mm wide) FAR 23The Certification Basis for the original product remains applicable tothis certificate/ approval. Flight manual supplement Doc. No. F195090;Modification datasummary Doc. No. F195000;Maintenance manual supplement Doc.No.E550070-MMS;or later revisions of the above listed documents approved by EASA inaccordance with EASA ED Decision 2004/02/CF (or subsequent revisions ofthis decision). none 28.11.2012 10034865 ACS-NAI Ltd. TCCA STC SA98-60 ISSUE 2 DHC-8-102,-103,-106 DHC-8-201,-202 DHC-8-301,-311,-314,-315 DHC-8-401,-402 Flight Deck Manual Stowage BoxTCCA STC SA98-60, Issue 2, dated 12.02.2001. FAR 25 as per EASA.IM.A.191, Iss. 4 for DHC-8-100/200/300 SeriesJAR-CS-25 as per EASA.IM.A.191, ISS, 4 for DHC-8-400 SeriesThe Certification Basis for the original product remainsapplicable tothis certificate/ approval.The requirements for environme (...) Installation must be in accordance with ACS- NAI Ltd. TCCA approvedModification Data Summary B 78600, Rev. H<(>,<)>Maintenance must be in accordance with Instructions for ContinuedAirworthiness MMS B 78671<(>,<)>or later revisions of the above listed (...) None. 06.05.2011 10035310 ACS-NAI Ltd. REV. 1 TCCA STC C-LSA11-075/D ISS1 BD-700-1A10 Installation, Complete Custom Aircraft Interior. 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. TCCA STC No. C-LSA11-075/D Issue 1 dated 13 May 2011.ACS-NAI Ltd. Modification Data Summary G789000 Revision NC or laterapproved revision.ACS- NAI Ltd. Airplane Flight Manual Supplement for the Complete CustomAircraft Interior, G789091 Revision B or (...) Restricted to ASN 9403.This system is intended to provide internet connectivity and emailservices to the airplane's cabin using portable electronic devices(PEDs). Any other intended function of this equipment will require are-examination of the cert (...) 15.06.2011 10036101 ACS-NAI Ltd. TCCA STC C-LSA11-134/D BD-700-1A10 Installation, Complete Custom Aircraft Interior - ASN 9412 EASA.IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) TCCA STC No. C-LSA11-134/D Issue 1 dated 03 August 2011.ACS-NAI Ltd. Modification Data Summary H039000 Revision NC or laterapproved revision.ACS- NAI Ltd. Airplane Flight Manual Supplement for the Complete CustomAircraft Interior, G789091 Revision B (...) Restricted to ASN 9412.The Wireless Local Area Network (WLAN) system is intended to provideinternet connectivity and email services to the airplane's cabin usingportable electronic devices (PEDs). Any other intended function of thisequipment will re (...) 11.08.2011 10036345 ACS-NAI Ltd. TCCA STC C-LSA11-058/D BD-700-1A10 Installation of Tailwind 500 System EASA.IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/or emissions levels of the original product areuncha (...) -Transport Canada STC No. C-LSA11-058/ D Issue 1 dated 21 April 2011-ACS-NAI Ltd. Modification Data Summary H058000 RevN/C or laterapproved revision.-ACS-NAI Ltd Instructions forContinued Airworthiness H058071 Rev N/C orlater approved revision.- Tran (...) None 02.09.2011 21/10/2013 Page 7/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10037710 ACS-NAI Ltd. TCCA STC C-LSA10-169/D CL-600-2B19 Installation, Complete Custom Aircraft Interior. 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. TCCA STC No. C-LSA10-169/D Issue 1 dated 03 December 2010.ACS-NAI Ltd. Modification Data Summary G773000 Revision NC orlaterapproved revision.Aero Consulting Services Ltd. Mandatory Maintenance Manual SupplementG192070 Revision NC or later approved (...) Restricted to ASN 8101. 16.12.2011 10037711 ACS-NAI Ltd. TCCA STC C-LSA11-165/D CL-600-2B19 Installation, Complete Custom Aircraft Interior. 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. TCCA STC No. C-LSA11-165/D Issue 1 dated 11 October 2011.ACS-NAI Ltd. Modification Data Summary H133000 Revision NC or laterapproved revision.Aero Consulting Services Ltd. Mandatory Maintenance Manual SupplementG192070 Revision NC or laterapproved r (...) Restricted to ASN 8107. 16.12.2011 10038022 ACS-NAI Ltd. TCCA STC NO. C-LSA11-009/D CL-600-2B19 Installation, Complete Custom Aircraft Interior. EASA.IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) TCCA STC No. C-LSA11-009/D Issue 2 dated 22 July 2011.ACS-NAI Ltd. Modification Data Summary G583000 Revision A or laterapproved revision.ACS-NAI Ltd. Mandatory Maintenance ManualSupplement, G583070 RevisionNC or later approved revision.ACS-NAI Ltd. (...) Restricted to ASN 81051.The Wireless Local Area Network (WLAN) system installed as part of theinterior completion is intended to provide cached internet content andemail services to Portable Electronic Devices. Any other use of thisequipment will re (...) 12.01.2012 10038149 ACS-NAI Ltd. TCCA STC NO. C-LSA11-179/D BD-700-1A10 Modifications to Existing Interior Completions - ASN 9393. 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. TCCA STC No. C-LSA11-179/D Issue 3, dated 12 January 2012;Aero Consulting Services Modification Data Summary H267000, Revision B,dated 22 December 2011 or later approved revision;Aero Consulting Services Mandatory Maintenance Manual Supplement forAn (...) Restricted to ASN 9393 andThe Installation of EASA STC No. 10036060 is a prerequisite for theapproval of this STC. 24.01.2012 10039631 ACS-NAI Ltd. TCCA STC C-LSA05-318/D CL-600-2B16 Aircraft Completion ASN 5618, 12 Passenger Interior Configuration. EASA.IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) TCCA STC No. C-LSA05-318/D Issue 2, dated 21 July 2006.AeroConsulting Services Ltd Modification Data Summary 610000 RevisionA, dated 18 July 2006.Midcoast Aviation Airplane Flight Manual Supplement 34-424M005 RevisionA.Midcoast Aviation Airplane Fli (...) Restricted to ASN 5618 15.05.2012 10039703 ACS-NAI Ltd. TCCA STC NO. C- LSA12-038/D BD-700-1A10 Installation of Complete Custom Aircraft Interior - ASN 9434 EASA.IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) TCCA STC No. C-LSA12-038/D Issue 1, dated 30 April 2012.Aero Consulting Services Ltd Configuration Definition List H282000Revision NC.Aeroplane Flight Manual Supplement H282090, Revision N/C.Instructions for Continued Airworthiness for theinstallati (...) Restricted to ASN 9434.The Wireless Local Area Network (WLAN) system is intended to provideinternet connectivity and email services to the airplane's cabin usingportable devices (PEDs). Any other intended function of this equipmentwill require a re-examination of the certification basis. 18.05.2012 10040686 ACS-NAI Ltd. JAA STC ACG.21NE2.084 TCCA SA01-77/JAA ACG.21NE2.084 DHC-8-102,-103,-106 DHC-8-201,-202, DHC-8-301,-311,-314,-315 Installation of an improved Aft Jet Pipe SupportTCCA STC N° SA01-77, Issue 3 FAR 25 as per EASA.IM.A.191, Issue 5 (incl. EWIS)The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions le (...) InstallationMust be in accordance with Aero Consulting Service Ltd. ModificationData Summary N° C 54600, Revision B.Maintenance:Must be in accordance with Aero Consulting Service Ltd. MaintenanceManual Supplement N° C 54672, N/C.or later revisions o (...) None. 19.07.2012 10041474 ACS-NAI Ltd. REV. 1 TCCA STC SA12-17 PC-6/B2-H2 PC-6/B2-H4 Installation of Vapour Cycle Air Conditioner System. US CAR 3 dated May 15, 1956 Arndt: 3-1 to 3-5and Special Conditions notified by the FAA to the Swiss FOCAThe Certification Basis for the original product remains applicable tothiscertificate/ approval.Derogation to latest amendment (Part 21 A.101):T (...) Airplane Flight Manual Supplement H404091 Revision N/C;Maintenance Manual Supplement H404071 Revision N/C and H404072 RevisionN/C;Wiring Diagram Manual Supplement H404073 RevisionN/C;or later revisions of the above listed documents approved by EASA (...) Refer to the Airworthiness Limitations contained in Airplane FlightManual Supplement H404091 Revision N/C. 04.10.2012 10042346 ACS-NAI Ltd. ACG.21NE2.108 TCCA SA02-127 / ACG.21NE2.108 DHC-8-102,-103,-106 DHC-8-201,-202 DHC-8-301,-311,-314,-315 Installation of an Improved Gound Power Current Limiter(ACS-NAI Ltd. Modification Data Summary D 11900)TCCA STC SA02- 127, Issue 1 FAR 25 as per EASA.IM.A.191, Issue 6 (incl. EWIS)The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions le (...) Installation:Must be in accordance with-,,ACS- NAI Ltd. Modification Data Summary D 11900, Revision C, dated22.03.2012 and- ,,ACS-NAI Ltd. Installation Instructions D 11981, Rev. E,dated23.03.2012.Maintenance:Must be in accordance with-,,ACS Ltd. Main (...) None. 26.11.2012 10043074 ACS-NAI Ltd. EASA.IM.A.S.03133 REV. 1 TCCA STC C-LSA09-029/D, ISS.2 CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. TCCA LSTC No. C-LSA09-029/D Issue 2 dated 17 June 2013.AeroConsulting Services Ltd. Modification Data Summary G118000 RevisionD.Midcoast Aviation Inc. Airplane Flight Manual Supplement for theComplete Custom Aircraft Interior Installation, 33- 299M00 (...) Restricted to ASN 8087. 16.08.2013 10043075 ACS-NAI Ltd. EASA.IM.A.S.03132 REV. 1 TCCA STC C-LSA09-027/D, ISS. 2 CL-600-2B19 Installation, Complete Custom Aircraft Interior 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. TCCA LSTC No. C-LSA09-027/D Issue 2 dated 17 June 2013.AeroConsulting Services Ltd. Modification Data Summary G117000 RevisionH.Midcoast Aviation Inc. Airplane Flight Manual Supplement for theComplete Custom Aircraft Interior Installation, 33- 299M00 (...) Restricted to ASN 8084. 16.08.2013 21/10/2013 Page 8/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10043177 ACS-NAI Ltd. CL-600-2B16 (604 VARIANT) Installation, Aircell Communication System EASA.IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) -Transport Canada STC No. C-LSA12-046/D, Issue 1 dated 12 July 2012.-ACS-NAI Ltd Modification Data Summary H048000 Revision NC.-ACS-NAI Ltd Mandatory Maintenance Manual Supplementfor theinstallation, Iridium Antenna FS 580, H048075 Revision N/C.-ACS (...) Restricted to ASN 5541 09.01.2013 10044051 ACS-NAI Ltd. TCCA STC SA12-40 BD-700-1A10, BD-700-1A11 Installation, Complete Custom Aircraft Interior The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS-25 Amendment 1Special Condition(s): CRI D-02 Issue 2, Side Facing DivansEquivalent Safety Finding(s): CRI D-04 Issue 2 (...) Transport Canada STC No. SA12-40 Issue 1, dated 08 June 2012ACS-NAI Configuration Definition Record H525001 Revision NC, dated 07June 2012ACS-NAI Airplane Flight Manual SupplementH525090 Revision NCInstructions for Continued Airworthinessdocument IC (...) EASA approved configurations are identified in Configuration DefinitionRecord H525001.The Wireless Local Area Network (WLAN) is intended to provide internetconnectivity and email services to the airplanes cabin using portableelectronic devices (PEDs (...) 14.03.2013 10046554 ACS-NAI Ltd. TCCA C-LSA13-057/D CL-600-2B19 Cabin Interior Re-configuration 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. Transport Canada STC No. C-LSA13-057/D Issue 1 dated 6th September2013.ACS-NAI Ltd. Modification Data Summary H989000 Revision N/C or laterapproved revision.ACS- NAI Ltd. AirplaneFlight Manual Supplement H989091 Revision N/C orlater approved revisio (...) Restricted to ASN 7248 30.09.2013 10015375 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01045 FAA STC ST01583LA BOEING 737-300 BOEING 737-400 Installation of ACSS T2CAS System according to FAA STC ST01583LA dated 20th January 2004.- ACSS Index of Master Data Lists, Document No. 8900034, Revision "A" dated 3rd September 2004, or later FAA approved revision- ACSS Airplane Flight Manual Supp (...) - ACSS Index of Master Data Lists, Document No. 8900034, Revision "A" dated 3rd September 2004, or later FAA approved revision- ACSS Airplane Flight Manual Supplement, Document No. 8002391-001, Revision "A" dated 21st October 2004, or later FAA approved revision 1. According to limitations section in FAA STC ST01583LA dated 20th January 2004.2. 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 a (...) 17.08.2005 10015406 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01117 FAA STC ST01702LA BOEING 747-200 BOEING 747-300 Installation of ACSS T2CAS -in accordance with Approval Report DL/LVT/05.532542-FAA approved ACSS Index of Master Data lists, Document No 8900035 revision A, dated 27 October 2004 or later approved revision-FAA approved ACSS Airplane Flight Manual Supplement Document No 8003638- 1. in accordance with Approval Report DL/LVT/05.5325422. T2CAS Airplane Flight Manual Supplement (AFMS), ACSS document number 8003638-001 revision A, approved by the FAA on May 25, 20053. This STC is approved only for the product configuration as de (...) 01.08.2005 10015573 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01480 FAA STC SA4839NM BOEING 757-200 Installation and activation of TCAS and the XS-950 Mode S Transponder (including ELS/EHS). Honeywell Master Data List ML4070373 Revision F dated July 24 1990 or later approved revision.Honeywell AFM Supplement 5140-0885 approved July 14 1990 or later approved revision. 07.11.2005 10015650 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01625 FAA STC SA5061NM DC-9-81 (MD-81) DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87) MD-88 Installation of Honeywell Traffic Alert & Collision Avoidance System (TCAS II) -Honeywell Master Data List No ML40741700 Revision A dated March 21 1991 or later approved revision-Honeywell AFM supplement TCAS-APPS-02494 Revision A dated October 18, 2000 or later approved revision 30.01.2006 10015651 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01626 FAA STC SA5541NM BOEING 767-200 BOEING 767-300 Installation of Honeywell Traffic Alert & Collision Avoidance System (TCAS) Honeywell Master Data List No ML4076520 Revision N/C dated July 24 1992 or later approved revision 1. TCAS Airplane Flight Manual Supplement (Change 7) TCAS-APPS-0294, Rev A.2. This STC is approved only for the productconfiguration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft (...) 12.12.2005 10015731 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01753 - AIRBUS A320-200 Installation of Honeywell TCAS II system Master Data List ref. ML-4075160, revision A, dated September 25, 1992 or later approved revisionAFM supplement ref. TCAS-APPS- 0294 revision A or later approved 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. 25.11.2005 10015838 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01932 FAA STC SA4882NM BOEING 747-100 BOEING 747-100B SUD BOEING 747-200B BOEING 747-200C BOEING 747-200F BOEING 747-300 BOEING 747-400 BOEING 747-SP BOEING 747-SR Installation of a Honeywell Traffic Alert and Collision Avoidance System (TCAS II) in accordance with FAA approved Honywell Master Data List number ML4071598 Data package containing the following documents, and additional supporting data:1. FAA Letter to Honeywell of approval pertaining to Honeywell previously approved STCs TCAS II installations to be upgraded to TCAS (10004) and to Mode S (10004) as (...) FAA approved Flight Manual Supplement required for this configuration is listed on the appropriate approved Honeywell and ACSS Master Index List. 31.07.2006 10031364 ACSS, AVIATION COMMUNICATION AND FAA STC ST01911LA B747-400 Installation of ACSS Mode S Transponder with ELS/EHS capability toreplace Mode S Transponder in existing ACSS Traffic Alert and CollisionAvoidance system TCAS II in accordance with FAA approval ACSS MasterData List Document No. 8900019-001, Revision (...) The Certification Basis for the original product remains applicable tothis certificate/ approval. None See Limitation Section of FAA approved ACSS Master Data List No. 8900019 11.08.2010 21/10/2013 Page 9/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10032094 ACSS, AVIATION COMMUNICATION AND FAA STC NO. ST00411LA B747-400 Installation of Honeywell Traffic Alert and Collision Avoidance System(TCASII) The Certification Basis for the original product remains applicable tothis certificate/ approval. FAA approved Air New Zealand Master Drawing List TX30031 Revision A,dated June 26, 1996 or later approved revision.For appropriate FAA approved Airplane Flight Manual Supplement refer toassociated section of the Air New Zealand Master Drawing List Document. none 07.10.2010 10042297 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01059 REV. 1 FAA ST01646LA ATR 42-200, ATR 42-300 ATR 42-320, ATR 42-500 ATR 72-101, ATR 72-102 ATR 72-202, ATR 72-211 ATR 72-212, ATR 72-212A Installation of ACSS Terrain and Traffic Collision Avoidance System(T2CAS).The revision 1 has introduced an AFM Supplement update. 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. ACSS Master Data List document, ref: 8900038 Rev. BEASA Aircraft Flight Manual Supplement, ref: 8004809-001 Rev. Aor 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 produc (...) 23.01.2013 10042553 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01044 REV. 1 FAA STC SA5530NM B737-100/200/300/400/500 FAA STC SA5530NM validation - Installation of the ACSS TCASII Systemwith Change 7.1 software The Certification Basis for the original product remains applicable tothis certificate/ approval.The certificated noiseand/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval. - ACSS Index of Master Data Lists (IMDL), Reference 8900010, Revision J,FAA approved the 06 July 2010;- Airplane FlightManual Supplement (AFMS) according to Honeywell MasterData List (MDL), Reference ML4075161, Revision AH, dated 14 May 2002;- ACSS, (...) None. 14.12.2012 10042711 ACSS, AVIATION COMMUNICATION AND REV. 3 FAA STC ST02406LA SEE EASA APPROVED MODEL LIST Installation of Traffic Alert and Collision Avoidance Systems (TCAS II)version 7.1Revision to incorporate additional aircraft models to the Approved ModelList:1. Hawker BeechcraftCorporation: BAe 125 Series 1000A, BAe 125 Series800B, and Hawker 800X (...) 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. -FAA STC ST02406LA, issued 6th February 2012-FAA Approved Model List AML No. ST02406LA, dated 3rd June 2013-Master DataList ref. doc. 8900067-002, Rev. D, dated 16th May 2013-Aircraft Flight Manual Supplement ref. doc. 8008565-001, Rev. IR, dated9t (...) 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 produc (...) 15.10.2013 10042940 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01064 FAA STC ST02788AT B767-200/-300/-300F Installation of Provisions for Terrain and Traffic Collision AvoidanceSystem (TTCAS)This STC is a validation of FAA STCST02788AT. -EMTEQ Engineering Master Drawing List EMTEQ-025-MDL Revision datedJanuary 27, 2004 or later Faa approved revision-AFM supplement Doc No 8002964-001 1. 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. 09.03.2005 10042943 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01065 REV. 1 FAA STC ST001627LA B767-200/-300 Installation of T2CAS -FAA STC ST001627LA-Doc. No. 8900037, Rev A dated 11 May 2004 or later FAA revision.-AFM Doc. No. 8002964-001, Rev "-" dated 27 April 2004, or later FAArevision 1. 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. 21.09.2005 10042944 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01067 REV. 1 FAA STC ST001628LA B757-200 Installation of T2CAS -FAA STC ST001628LA-ACSS Index of Master Data Lists Document Number 8900036 Revision Bdated May 10 2004 or later FAA approved revision-ACSS Flight Manual Supplement number 8002942-001 revision "-" dated May5 2004 or later FAA approved revision 1. 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. 21.09.2005 10044749 ACSS, AVIATION COMMUNICATION AND FAA STC SA4839NM 757-200, 757-200PF Installation of the ACSS TCAS system[description: Installation and activation of ACSS TCAS Change 7.1software and deactivation of the ACSS TCAS Change 7.0 software] 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 - Master Data List, Honeywell document No. ML4070373, Revision F, dated24 July 1990 ;- Aircraft Flight Manual Supplement, Honeywell document No. 5140-0885,approved on 14 July 1990;or later revisions of the above listed documents approved by EASA ina (...) None 03.05.2013 10033485 ADAC LUFTFAHRT TECHNIK GmbH EC135P2 (CPDS), EC135 P2+, EC135T2 (CPDS), EC135 T2+ Installation of Dual Garmin GNS 430W into EC 135 with MEGHAS cockpitInstallation of two GNS430W linked with indication on the FCDSas definedin the Master Drawing List EC135-01 066-005-LIN and based on ALT MajorChange EC135-01066. The Certification Basis for the original product remains applicable tothis certificate/ approvalThe requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval Flight Manual Supplement:-,,EC135-01066- 025-MFS-00 Rev. 0orlater revisions of the above listed documents approved by EASA·,,EC135-01066-023-MMS Rev. 0 Instructions for Continued Airworthiness·,,EC135-01066-004-DIN Rev. 0 Installation Instructionsor later revisions of the above listed documents. None 25.01.2011 10035671 ADAC LUFTFAHRT TECHNIK GmbH EC135 T1(CDS) EC135 T1(CPDS) EC135 T2(CPDS) EC135 T2+ EC135 P1(CDS) EC135 P1(CPDS) EC135 P2(CPDS) EC135 P2+ Installation of fixed Landing Lights on the forward crosstube.Installation of a second fixed landing light on the forward cross tubeas defined in the MDL EC135-01072-001-LMD and based on ALT changeproject EC135- 01072. 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. Flight Manual Supplement:-,,EC135-01072- 025-MFS-00 Rev. 0orlater revisions of the above listed documents approved by EASA.- EC135-01072-023-MMS Rev. 0 Instructions for Continued Airworthiness<(>,<)>- EC135- 01072-004-DIN Rev. 0 Installation Instructi (...) None 08.07.2011 10036349 ADAC LUFTFAHRT TECHNIK GmbH REV. 1 EC135 P2+ / EC135 P2(CPDS) EC135 T2+ / EC135 T2(CPDS) Installation of an NVIS lighting system in a Eurocopter EC 135 (MEGHAS)- Major Change to EASA STC 10036349 - in accordance with Master DocumentList EC 135-02956-001-LMD-00 Rev 0.Note: This revision of the EASA STC 10036349 change introduces a filte (...) 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. STC 10036349: (Applicable to EC 135 T2+/EC 135 P2+/EC135 T2(CPDS)/EC135P2(CPDS)- Flight Manual Supplement EC 135-01065-025-MFS, Revision 0STC 10036349 Revision 1: (Applicable to EC 135 T2+)- Flight Manual Supplement EC 135-02956-025-MFS, Revision 0o (...) - The first installation of this kit must be supervised by the STCholder.- This rotorcraft employs Night Vision ImagingSystem lightning,commonly named NVIS lightning, that has been certified to ensure theaircraft is compatible with night vision gogg (...) 07.10.2013 21/10/2013 Page 10/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10039230 ADAC LUFTFAHRT TECHNIK GmbH BK117 C-2 NVIS Certification of mission equipment on an Eurocopter BK117 C2 The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CS29 Amdt 2 incl. App. BThe requirements for environmental protection and the associat (...) Flight Manual Supplement:-EC145-01932- 025-MFS-00 Rev. 0or later revisions of the above listed documents approved by EASA- EC145-01932-023-MMS-01 rev 1 MAINTENANCE MANUAL SUPPLEMENT- EC145-01932-004-DIN-00 Rev. 0 Installation Instructionsor later revisions of the above listed documents. Required pre-modification EASA approval 10038241 (ECD majorchange 2237) 19.04.2012 10044319 ADAC LUFTFAHRT TECHNIK GmbH MBB-BK117 B-2, MBB-BK117 C-1 Installation of an external mirror with electrical remote control asdefined in BK117-02441- 001-LMD-00. 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. Flight Manual Supplement BK117-02441-025- MFS Rev. 0;or later revisions of the above listed documents approved by EASA.-Master Document List BK117-02441-001-LMD Rev. 0,- Certification Programme BK117-02441- 003-RCP Rev. 1,- Installation Instructions B (...) None. 10.04.2013 10044463 ADAC LUFTFAHRT TECHNIK GmbH EC 135 P1 (CDS), EC 135 P1 (CPDS), EC 135 P2 (CPDS), EC 135 P2+, EC 135 T1 (CDS), EC 135 T1 (CPDS), EC 135 T2 (CPDS), EC 135 T2+. Installation of a FLARM - CS 27 Amdt 2- Original Type Certification Basis Special Condition "Protection ofElectrical and Electronic Systems from High Intensity Radiated Fields"(CRI F-7, Issue 5)The requirements for environmental protection and the associatedcertified noise (...) - Flight Manual Supplement EC 135-02376- 025-MFS-00, Rev 0orlater revisions of the above listed documents approved by EASA.- Master Document List EC 135-02376-001- LMD-00, Rev 0- Maintenance Manual Supplement/ICA EC 135-02376-023-MMS, Rev 0 None 15.04.2013 10028594 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03223 REV. 1 FAA STC ST09365SC DHC-8-201, DHC-8-202 Installation of dual Collins Mode S TranspondersFAA STC ST09365SC, IR, August 14, 1997 FAR 25 as per EASA.IM.A.191, Issue 4 (incl. SC H-01 ICA on EWIS)The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/o (...) -Installation of dual Collins Mode S Transponders iaw. AAT MasterDrawing List 1101-000, Rev. B, dated September 18, 2000- Airplane Flight Manual Supplement Doc. No. 1101-916, Rev. IR, August14, 1997Maintenance iaw Bombardier Maintenance Manual PSM 1- (...) None 19.07.2011 10028595 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03220 REV. 2 FAA STC ST09326SC DHC-8-201, DHC-8-202 Installation of Dual Universal Navigation UNS- 1C Flight ManagementSystemFAA STC ST09326SC, Rev. 1, dated 14 November 2000 FAR 25 as per EASA.IM.A.191, Issue 4 (incl. SC H-01 ICA on EWIS)The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/o (...) -Installation of Dual Universal Navigation UNS- 1C Flight ManagementSystem iaw AAT Master Drawing List 1061-000, Rev. G- Airplane Flight Manual Supplement Doc. No. 1061-916, Rev. B-Maintenance iaw Bombardier Airplane Maintenance Manual PSM 1-82-2.or l (...) None 20.07.2011 10028911 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03222 REV. 2 FAA STC ST09347SC DHC-8-201, DHC-8-202 DHC-8-401, DHC-8-402 Installation of Coltech ATSCALL SystemFAA STC ST09347SC, Rev. 1, dated May 08, 2001. FAR Part 25 as per TCDS EASA.IM.A.191, Issue 4 (including SpecialConditions H-01 "Enhanced Airworthiness Programme for Aeroplane Systems- ICA on EWIS") for DHC- 8-100/200/300 SeriesCS 25/JAR 25 as per TCDS EASA.IM.A.191 Issue 4 (including SpecialCond (...) -Installation of Coltech ATSCALL iaw. AAT Master Drawing List 1078-000,Rev. B, dated February 01, 2001.-Airplane FlightManual Supplement Doc. No. 1078-916, Rev. A, dated May06, 2001.- Maintenance iaw Bombardier Airplane Maintenance ManualPSM 1-82-2, (...) None 20.07.2011 10029263 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03221 REV. 2 FAA STC ST09346SC DHC-8-201, DHC-8-202 Installation of Honeywell Traffic Alert and Collision Avoidance System,TCAS IIFAA STC ST09326SC, Rev.1, dated 14 November 2000. FAR-25 as per EASA.IM.A.191, Issue 4 (incl. SC H-01 ICA on EWIS).The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ (...) Installation of Honeywell Traffic Alert and Collision Avoidance System,TCAS II iaw. AAT Master Drawing List 1065-000, Rev. B, dated March 17,1997.Airplane Flight Manual SupplementDoc. No. 1065-916, Rev. IR.- Maintenance iaw Bombardier Airplane Maint (...) none 20.07.2011 10017156 AERAZUR - ZODIAC AEROSPACE GROUP EASA.R.S.01263 REV. 6 S-92A Installation of AERAZUR Internal Auxiliary Fuel System (IAFS) completionkit p/n 508617 or 508617-1 or 508617-2 or 508617-3.STC revision 1 introduces kit p/n 508617-1 and revised documentation.STC revision 2 introduces edition 15 of RFM supplement.ST (...) The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:Special Condition(s): IADS CRI C-1 Issue 3 - Crashconditions - Fittingfactor and IAFS CRI E-1 Issue 3 - Fuel system crash (...) S-92A Flight Manual Supplement n° 060S437, edition 16 dated06 December2010 or later revisions of the above listed documents approved by EASA.AERAZUR document CBIA n°060S149, revision 11 dated 27 September 2013.AERAZUR document CBIA n°060S147, revisi (...) The IAFS Completion Kit can be installed only on S-92A helicoptersequipped with:- S-92A Avionics Management System (AMS) version n° 091-2527-007 orlater approved version, and- AERAZUR IAFS Provision Kit p/n 509429-02 or 509429-03 approved underEASA (...) 04.10.2013 10017259 AERAZUR - ZODIAC AEROSPACE GROUP EASA.R.S.01466 REV. 7 S-92A Installation of Provision Kit p/n 509429-02 or p/n 509429-03 of InternalAuxiliary Fuel System (IAFS).STC revisions 1 and 2 introduce minor design modifications for kit p/n509429-02 and revised documentation.STC revision 3 introduces kit p/n 509429-0 (...) 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. Aerazur Organigramme Technique ref. 509429-03 issue 13 dated 05 July2013;Aerazur Organigramme Technique ref. 509429-02 issue 12 dated 26 May2010.IAFS - High Profile (HP) version - Maintenance Manual Supplement forprovision kit - chapter 11and 28, iss (...) Refer to applicable installation instructions for compatibility of theIAFS provision kit with S- 92A cabin interior panels as stated in STC10017259 revisions 1 to 6.Prior to installation of this design change it must be determined thatthe interrelati (...) 26.08.2013 10014306 AERLYPER S.A. EASA.A.S.01550 BEECH 200 Installation of MST67A Transponder Mode S Equipment. Master Data List AERLYPER DOC N° 100469 Ed. 04Instruction for continuous Airworthiness AERLYPER DOC: N° 100482 Ed. 01 06.12.2007 10014317 AERLYPER S.A. EASA.A.S.01567 BEECH 200, SUPER KING AIR Tactical console installation on B-200 aircraft with ARGOS system, tactical communications system and fixed provisions for ASTRA system. Documentation referred to in Doc. No. 100513 "Documents andDrawings List" Issue 04, 27 November 2006. Doc. No. 100528 "Aircraft Flight Manual Supplement", Issue 1, 27 November 2006 included. In accordance with Doc. No. 100528 "Aircraft Flight Manual Supplement", Issue 01, 27 November 2006. 31.05.2007 10014318 AERLYPER S.A. EASA.A.S.01568 BEECH 200 Inmarsat SATCOM installation on board B200.The modificationis optional and fixed. It consists of an Inmarsat SATCOM terminal to be installed in the passenger cabin. A SATCOMantenna is installed on the upper part of the fuselage. Documentation referred in: Doc 100423 Ed.04: Documents andDrawings List. In accordance with Doc. No. 100429 AFM Supplement ED.03. 31.05.2007 21/10/2013 Page 11/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10014319 AERLYPER S.A. EASA.A.S.01569 BEECH 200 Installation of New Avionics Equipment to comply with COM/NAV regulations for IFR and B-RNAV Operation. Master Data List AERLYPER DOC N° 100542 Ed. 4New Supplementto Aircraft Flight Manual AERLYPER DOC N° 100553 Ed. 00Instructions for Continuous Airworthiness AERLYPER DOC N° 100554Ed. 02 06.12.2007 10014420 AERLYPER S.A. EASA.A.S.01741 FAIRCHILD SWEARINGEN SA 227- BC Garmin GPS 155XL with antenna GA-56, Mid- Continent MD41-448Annunciation control Unit and copilot CDI Mid-Continent MD 40-09L installation for B-RNAV operation Doc No AI03-081-01 "Plan de Certification" Edition 04Installation Instructions in accordance withDoc No AI03-081-00, "Lista de Documentos y Planos" Edition 05Doc No AI03-081-14, "Decripcion de la Instalacion" Edition 01Doc No AI03-081-15, "Boletin d (...) The aircraft is approved for dual pilot B-RNAV operation, subject to the conditions, limitations and procedures contained in Doc NoAI03-081-03 "Flight Manual Supplement", Rev 03 17.01.2006 10017103 AERLYPER S.A. EASA.R.S.01073 EC 135 P2 Microwave Transmission System on EC-135 Helicopters Documentation referred in: Doc No. 100189: Documents and Drawings List In accordance with Doc No 100198: RFM Supplemt Ed. 3 14.02.2006 10017104 AERLYPER S.A. EASA.R.S.01075 BO105 C, BO105 S ASTRA System installation on BO-105 C/S Helicopters -Documentation referred in Doc No 100130: Documents and Drawings List In accordance with Doc No 100137: RFM Supplement Ed.4 30.01.2006 10017105 AERLYPER S.A. EASA.R.S.01076 EC 135 P2 Installation of Image Recorder System UM III and Options System Documentation referred in Doc: No 100052: Documents and Drawings List Doc No 100059: RFM Supplement Ed. 3 08.02.2006 10017137 AERLYPER S.A. EASA.R.S.01231 BO 105 C, BO 105 S Digital microwave transmission system installation on boardBO-105 C/S. Doc. No. 100388 "Master Data List", issue 3, June 2008.Doc. No. 100589 "Aircraft Flight Manual Supplement", issue 1, April 2008.Doc. No. 100590 "Continuing Airworthiness Instructions", issue 00, February 2008. In accordance with Doc. No. 100589 "Aircraft Flight Manual Supplement", issue 1, April 2008.Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously instal (...) 01.07.2008 10017197 AERLYPER S.A. EASA.R.S.01338 REV. 1 EC-135-P2 (CPDS) EC-135-P2+ UM-III HD Camera System & Microwave Transmission System Installation Onboard EC135. ¿ Master Data List Aerlyper DOC No. 100961 Ed. 03;¿ Supplement to Rotorcraft Flight Manual (RFM) Aerlyper Doc No.100973 Ed. 01;¿ Instructions for Continuous Airworthiness Aerlyper Doc No. 100974 Ed. 01. 1. Master Data List and RFM Supplement mentioned above. 13.05.2008 10033659 AERLYPER S.A. P-EASA.R.S.01507 REV. 1 EC135 P2 & EC135 P2+ Installation of STAR SAFIRE HD Camera System & Digital TransmissionSystem The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalJAR 27 Amendment 3, dated 01/04/2002, for paragraphs 27.561 & 27.602JAR 27 Amendment 2, (...) - Document: «Lista de Documentos y Planos», n°: 101499, Edition: 03,Date: 28-01- 2011- Document: «Suplemento al Manual de Vuelo», n°: 101511, Edition: 00,Date: 28-01- 2011- Document: «Instrucciones de Aeronavegabilidad Continuada», n°: 101512,Edition: (...) None 02.03.2011 10015399 AERO ASSOCIATES INC EASA.IM.A.S.01109 FAA STC SA00548AT CESSNA 172 SERIES Camera Hole Installation Aero Associates Inc Drawing ED94003 no revision dated march25, 1994 or later FAA approved revison as defined in FAA STC SA00548AT 1. Continued Airworthiness-All new and modified structure that forms part of this STC must be inspected at least annually for damage. Any defects found must be repaired by approved repair scheme.2. This STC is approved only for the productconfigurat (...) 30.05.2005 10015649 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01624 REV 1 TCCA STC C-LSA05-303/D ISSUE 2 BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior Configuration - Aero Consulting Services Modification Data Summary E596000 Revision B or later approved revision.- Midcoast Aviation AFM Supplement 34-424M005 Revision N/C or later approved revision.- Midcoast Aviation AFM Supplement 34-261M017Revision N/C or later approved revision. Restricted to Aircraft Serial Number 5610 25.07.2006 10015653 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01628 REV 1 TRANSPORT CANADA STC C-LSA05- 2 BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior Configuration - Aero Consulting Services Modification Data Summary E281000 Revision B or later approved revision.- Midcoast Aviation AFM Supplement 34-424M005 Revision N/C and 34-261M017 Revision N/C or later approved revision. 1. This STC is approved only for the product configuration as defined in the approved design data referred to in theparagraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.2. Restricted to Aircraft Serial Number 5609. 25.07.2006 10015670 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01647 REV 1 TCCA STC C-LSA05-317/D ISSUE BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior Configuration -Transport Canada STC C-LSA05-317/D Issue 2-Aero ConsultingServices Modification Data Summary E611000 Revision A or later approved revision-Midcoast Aviation AFM Supplement 34-261M017 Revision N/C & 34- 42M005 Revision N/C or later approved revision 1. Restricted to ASN 5620 only.2. This STC is approved onlyfor the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10.08.2006 10015671 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01649 REV 1 TCCA C-LSA05-315/D ISSUE 2 BOMBARDIER CL-600-2B16 (CL- 604 Aircraft Completion 12 Passenger Interior Configuration -Transport Canada STC C-LSA05-315/D Issue 2-Aeroconsulting Services Modification Data Summary E613000 Revision A or later approved revision-Midcoast Aviation AFM Supplemetn 34-261M017 Revision N/C & 34- 42M005 Revision N/C or later approvedrevision 1. Restricted to ASN 5612 only2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 11.08.2006 10015678 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01659 REV 1 TCCA STC C-LSA05-328/D BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior Configuration Transport Canada Limited STC C-LSA05- 328/D Issue 2 dated October 02 2006.Aero Consulting Servies Modification Data Summary E640000 Revision A or later approved revisionMidcoast Aviation Airplane Flight Supplement 34-424M005 Revision N/C and 34-261M017 Revision N/C or later approved revision 1. Limited to S/N 56172. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 27.10.2006 21/10/2013 Page 12/494 EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Certification Basis Limitations Conditions Date of issue 10015859 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01967 TCCA STC SA03-43 BOMBARDIER CL-600-2B19 Installation of Safe Flight Autopower (Autothrottle) System Transport Canada STC SA03-43 Issue 1 dated May 09, 2003AeroConsulting Services Modification Data Summary D45150Safe Flight AFM Supplemetn R-2827 Revision N/C dated May 09 2003 orlater approved revision -- 14.09.2006 10016132 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02326 TCCA STC SA95-67 BOMBARDIER DHC-8-100 SERIES BOMBARDIER DHC-8-200 SERIES BOMBARDIER DHC-8-300 SERIES Installation of Aero Consulting Services Ltd. "Improved Exhaust Outlet Shroud Assembly" according to Transport Canada STC SA 95- 67 The manufacture and installation of the Improved Exhaust Outlet Shroud Assembly is to be completed in accordance with Aero Consulting Services Ltd. Modification Data Summary Number A23820, Revision D, dated March 27, 2001 or later DOT approved revis (...) 01.03.2007 10016192 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02429 TCCA SA01-65, ISSUE 4 BOMBARDIER DHC-8-100 SERIES BOMBARDIER DHC-8-200 SERIES BOMBARDIER DHC-8-300 SERIES Addition of filtration to Cabin Recirculation Air.Addition of recirculation air filter reduces potential blockage of the condenser mixer and promotes peak performance of the ECS system. TCCA STC SA01-65, Issue 4, dated 24 June 2005. Aero Consulting Services Modification Data Summary No. C46000 Revision D or later approved revisions for DHC-8-100 and DHC- 8-200 series or S46030 Revision C or later TCCA approved revisions for DHC-8-300 series.Maintenance Manual Supplement (MMS) C (...) 1. Applicable to DHC-8-100 series with 1990 (Post-Mod 8/1127*) cabin interior, all DHC-8-200 series and DHC-8-300 series with 1990 (Post-Mod 8/1128*) cabin interior.*Including Hunting and CD interior.2. Prior to installation of this modificati (...) 06.07.2007 10016270 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02554 TCCA STC C-LSA07-190/D ISSUE 2 Upgrade to Honeywell Mark V EGPWS. Aero Consulting Services Modification Data Summary F379000,rev B.Flight Manual Supplement, F379091, rev N/C.Instructions for Continued Airworthiness, F379071, rev N/C. 02.11.2007 10016376 AERO