Garmin G1000 EASA Supplemental Type Certificate
Contents
1. the Instructions for Continued Airworthiness ICA listed in the Master Drawing List MDL identified above This STC provides Group Airworthiness Approval for Reduced Vertical separation Minimum RVSM for Models 200 and B200 Optional Electronic Stability and Protection requires MDL 005 00421 00 Rev 9 or later and AFMS 190 00915 02 Rev 4 or later Prior to installation of this modification it must be determined that the interrelationship between this modification and any other previously installed modification and or repair will introduce no adverse effect upon the airworthiness of the product end Note The following numbers are listed on the certificate EASA current Project Number 0060006239 001 EASA old Project Number P EASA IM A S 03191 REV 2 SUPPLEMENTAL TYPE CERTIFICATE 10033158 REV 2 GARMIN INTERNATIONAL Inc EASA Form 91 Issue 4 24 09 2010 2 22. European Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10033158 REV 2 This Supplemental Type Certificate is issued by EASA acting in accordance with Regulation EC No 216 2008 on behalf of the European Community its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation and in accordance with Commission Regulation EC No 1702 2003 to GARMIN INTERNATIONAL Inc 1200 EAST 151ST STREET OLATHE KS 66062 USA and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and environmental protection requirements when operated within the conditions and limitations specified below Original Product TC Number EASA IM A 277 TC Holder HAWKER BEECHCRAFT CORPORATION Model BEECH 200 200C B200 B200C Original STC Number FAA STC SA01535WI D Description of Design Change Installation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection system ESP EASA Certification Basis The Certification Basis for the original product and the following additional or alternative airworthiness requirements are applicable to this certificate approval CS 23 Amdt for areas of change The requirements for environmental protection and the associated certificated noise and o
3. r emissions levels of the original product are unchanged and remain applicable to this certificate approval See Continuation Sheet s For the European Aviation Safety Agency European Aviation Safety Agency Date of issue 05 10 2011 ae GA Permit to Fiy Scordinaior amp Project Certification Manager Tel 49 221 89990 4117 Michael duesing easa europa eu Note The following numbers are listed on the certificate EASA current Project Number 0060006239 001 EASA old Project Number P EASA IM A S 03191 REV 2 SUPPLEMENTAL TYPE CERTIFICATE 10033158 REV 2 GARMIN INTERNATIONAL lac EASA Form 91 Issue 4 24 09 2010 1 2 European Aviation Safety Agency Associated Technical Documentation Installation in accordance with Garmin Master Drawing List MDL 005 00421 00 Revision 3 dated 3 14 2009 Operation in accordance with Garmin Airplane Flight Manual Supplement AFMS 190 00915 02 Revision 1 dated 3 14 2009 and EASA approved Flight Manual Supplement ref 190 00915 04 Rev 1 or later approved revisions or later revisions of the above listed documents approved by EASA in accordance with EASA ED Decision 2004 04 CF or subsequent revisions of this decision Limitations None Conditions Additional airframe engine and propeller configuration requirements are defined in the data shown on the Garmin Master Drawing List MDL identified above Aircraft modified by this STC must be maintained in accordance with
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