Garmin SA01535Wi_D FAA Supplemental Type Certificate
Contents
1. Signature of grantor D47 Any alteration of this certificate is punishable by a fine of not exceeding 1 000 or imprisonment not exceeding 3 years or both FAA Form 8110 2 1 10 69 PAGE 2 of 4 PAGES This certificate may be transferred in accordance with FAR 21 47 Hnit States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Continuation Sheet Narr E SA01S35WI D Yate of issuance March 14 2009 Qute Amended December 14 2009 November 23 2010 May 11 2012 May 14 2013 Linilalions and Condilions 1 Compatibility of this design change with previously approved modifications must be determined by the installer 2 Additional airframe engine and propeller configuration requirements are defined in the data shown on the Garmin Master Drawing List MDL identified above 3 Aircraft modified by this STC must be operated in accordance with the Airplane Flight Manual Supplement AFMS identified above 4 Aircraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness ICA listed in the Master Drawing List MDL identified above 5 Ifthe holder agrees to permit another person to use this certificate to alter the product the holder must give the other person written evidence of that permission 6 This STC provides Group Airworthiness Approval for Reduced Vertical Separation Minimum R2. United States of America Department of Transportation Federal Aviation Administration Supplemental Cype Certificate WN rnb 2 SA01535WI D Ihes cerlifecate issued lo Garmin International Inc 1200 East 151 Street Olathe KS 66062 cordifies lhl lhe change tn the byjee Leste for lhe fobielt ng s prodik uti the briitalicrs and coridilions thuvrefere as wrecifoed hereon meeli the wsvucrbliness reguibrepovttils of Lat 23 o h Federal Aviation Soepuledlions OQuptnal Poduct Type bertifucale Sinb A24CE Mbake Hawker Beechcraft Mbcdel 200 200C B200 B200C 300 300LW B300 B300C Lesocplion fe Vigne Design Bhange Installation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection ESP Required Data for Model 200 series 1 Garmin Master Drawing List MDL 005 00421 00 Revision 3 dated 3 14 2009 2 Garmin Airplane Flight Manual Supplement AFMS 190 00915 02 Revision 1 dated 3 14 2009 Required Data for Model 300 series 1 Garmin Master Drawing List MDL 005 00629 00 Revision 1 dated 5 11 2012 _ 2 300 300LW Garmin Airplane Flight Manual Supplement AFMS 190 00716 02 Revision 1 dated 5 11 2012 3 B300 B300C Garmin Airplane Flight Manual Supplement AFMS 190 00716 03 Revision 1 dated 5 11 2012 Later FAA approved revisions to the data listed above are incorporated without further revision to this Supplemental Type C
3. 3 1329 a b c d e hg h 23 49 23 181 b 23 45 23 681 a _ Original 23 1331 a b 1 23 43 23 207 a b 23 7 23 683 23 7 23 1335 23 20 23 251 23 45 23 685 a c d 23 17 23 1351 ag 23 49 23 301 a 23 48 23 689 a b c d e 23 7 23 1353 h 23 49 23 303 Original 23 771 a 23 14 23 1357 a b c d 23 43 23 305 23 45 23 773 a 2 23 45 23 1359 23 49 23 307 a Original 23 777 a b 23 51 23 1365 a b d e 23 49 23 337 23 48 23 779 a 23 51 23 1367 Original 23 365 d Original 23 853 a 23 49 23 1381 a b Original 23 395a 1 23 7 23 863 23 34 23 1419 ac 23 43 23 397 23 45 23 867 a b c 23 49 23 1431 a b e 23 49 23 561 e 23 34 23 901 e 23 53 23 1501 23 21 23 571 c 23 48 23 1301 23 20 23 1521 a b c 23 50 23 573 b 23 48 23 1303 a b d f 23 49 23 1523 23 34 23 601 Original 23 1305 a 2 3 c 1 2 5 e 1 23 52 23 1525 23 45 23 603 23 23 23 1307 23 49 23 1529 23 26 23 605 a 23 23 23 1308 a b c 23 57 23 1541 ab 23 21 23 607 23 48 23 1309 a 1 3 b c d e f 23 49 23 1543 b c 23 50 23 609 Original 23 1311 a b c 23 49 23 1545 a b d 23 50 23 611 23 48 23 1321 23 49 23 1549 23 45 23 613 a b c 23 45 23 1322 23 43 23 1555 a b e 2 23 50 23 627 Original 23 1323 a b c 23 49 23 1581 a b 1 3 d f 23 50 23 671 Original 23 1325 a b e 23 50 23 1583 e h m 23 50 23 1327 23 20 23 1585 a 1 j 23 50 Additional requirements for the Models 300 and 300LW Section Amdt 23 149 a b c d e 23 50 23 672 b c 23 45 23 1303 e 23 49 Additional requirements for the Models B300 and B300C Section i Amdt S
4. VSM 7 The Model 200 series optional Electronic Stability and Protection requires MDL 005 00421 00 Rev 9 or later and AFMS 190 00915 02 Rev 4 or later 8 Aircraft s n FL 1 to FL 110 FM 1 to FM 8 and FN 1 are approved for improved field performance when modified by Beech Kit 130 3004 prior to or concurrent with this STC installation The Hawker Beechcraft Airplane Flight Manual Supplement AFMS p n 130 590031 75 must be attached to the POH AFM for improved performance operation Any alteration of this certificate is punishable by a fine of not exceeding 1 000 or imprisonment not exceeding 3 years or both FAA ForM 8110 2 1 10 69 PAGE 3 of 4 PAGES This certificate may be transferred in accordance with FAR 21 47 Hnit States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Continuation Sheet N urnl er SA01535WLD Dato of cssuance March 14 2009 izte Aemended December 14 2009 November 23 2010 May 11 2012 May 14 2013 Certification Basis Based on 14 CFR 21 115 and 21 101 and the FAA policy for significant changes in FAA Order 8110 48 the certification basis for this change is as follows a The certification basis for parts not changed or not affected by this change is shown on TCDS A24CE b The certification basis for parts changed or affected by this change is Section Amdt Section Amdt Section Amdt 23 143 23 50 23 677 a d 23 49 2
5. ection Amdt 23 149 a b c d e f 23 50 23 1309 a 4 23 49 23 672 b c 23 45 23 1323 e 23 49 23 1303 e g 23 49 meme cere nn ee mena nana na en nnnn nnn nennnnnmnn manne EN Dqnnnn2nnnnenencnnnnnn ne en enna nn ennnennennnnnnane Any alteration of this certificate is punishable by a fine of not exceeding 1 000 or imprisonment not exceeding 3 years or both FAA ForM 8110 2 1 10 69 PAGE 4 of 4 PAGES This certificate may be transferred in accordance with FAR 21 47
6. ertificate Kees certifecale and the SY UIT daia uhai ts the Cases fer gywovdl shall remain an ffet untel surrendered suspended reveked or a lerpunutior dale ts clherutse established by lhe Sodorintstraler ts the Jederal Aviation Adinrinisteabicr Yule of onplication February 29 2008 Date of issuance March 14 2009 Date reissued QYote anentled December 14 2009 November 23 2010 May 11 2012 May 14 2013 By davedien tf lhe SAedaunistraber a a Pa LEP hwo Signature Robert Murray ODA STC Unit Administrator ODA 240087 CE Garmin International Inc Title Any alteration of this certificate is punishable by a fine of not exceeding 1 000 or imprisonment not exceeding 3 years or both FAA Form 8110 2 10 68 PAGE 1 of 4 PAGES This certificate may be transferred in accordance with FAR 21 47 INSTRUCTIONS The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate The FAA will reissue the certificate in the name of the transferee and forward it to him Transfer the ownership of Supplement Type Certificate Number To Narre afd Cuaresperee Print or Wye vA Aides of grante Neurber and streed From Varne ok grantes Pant or Y et fe Address of grater Neurber and streed Sil Shale and Bija cede Extent of Authority if licensing agreement Date of Transfer
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