STC SA01535WI-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01535WI-D This certificate issued to: Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 Part 23*_ of the Federal Aviation Requations Original Product Type Certificate Number: A24CE Description of Type Design Change:

Make: Textron Aviation Model: 200, 200C, A200, A200CT, B200, B200C, B200GT, B200CGT, 300, 3OOLW, B300, B300C 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 (except A200 Series):

(1) Garmin Master Drawing List (MDL) 005-00421-00, Revision 3, dated 3/14/2009

(2) For installations with system software version 0985.00 or later, Garmin Airplane Flight Manual Supplement (AFMS) 190-00915-02, Revision 1, dated 3/14/2009.

(3) For installations with system software version 2286.00 or later, Garmin Airplane Flight Manual Supplement (AFMS) 190-00915-N2, Revision 1, dated 9/16/2016.

Required Data for Model A200 Series:

(1) Garmin Master Drawing List (MDL) 005-00421-00, Revision 30, dated 11/30/2020.

(2) Garmin Airplane Flight Manual Supplement (AFMS) 190-00915-N6, Revision 1, dated 11/30/2020.

(continued on Page 3)

Date of Application: February 29, 2008 Date Reissued:

Date of Issuance: March 14, 2009 Date Amended: December 14, 2009; November 23, 2010; May 11, 2012;

May 14, 2013; February 28, 2014; September 16, 2016; February 17, 2017, July 16, 2018, April 30, 2019, November 18, 2020, November 30, 2020, July 26, 2021, September 6, 2023, August 22, 2025 By Direction of the Administrator Signature: _ Title: Paul Mast ODA STC Unit Administrator ODA-240087-CE Garmin International, Inc.

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 1 of 5

AVIATIO United States of America Department of Transportation AMAISTRAND Federal Aviation Administration Supplemental Type Certificate Number: _

TransferEndorsement Transfer the ownership of Supplemental Type Certificate Number:

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

The ST's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder.

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 2 of 5

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01535WI-D date 8/22/2025 Description of Type Design Change: (Cont.)

Required Data for Model 300 Series:

(1) Garmin Master Drawing List (MDL) 005-00629-00, Revision 1, dated 5/11/2012.

(2) For 300 and 300LW installations with system software version 0985.00 or later, Garmin Airplane Flight Manual Supplement (AFMS) 190-00716-02, Revision 1, dated 5/11/2012.

(3) For B300 and B300C installations with system software version 0985.00 or later, Garmin Airplane Flight Manual Supplement (AFMS) 190-00716-03, Revision 1, dated 5/11/2012.

(4) For 300 and 300LW installations with system software version 2286.01 or later, Garmin Airplane Flight Manual Supplement (AFMS) 190-00716-N2, Revision 1, dated 2/17/2017.

For B300 and B300C installations (standard weight) with system software version 2286.01 or later, Garmin Airplane Flight Manual Supplement (AFMS) 190-00716-N3, Revision 1, dated 2/17/2017.

(6) For B300 and B300C installations (heavy weight) with system software version 2286.10 or later, Garmin Airplane Flight Manual Supplement (AFMS) 190-00716-N8, Revision 1, dated 11/18/2020.

Later FAA-approved revisions to the data listed above are incorporated without further revision to this Supplemental Type Certificate .

(1) Compatibility of this design change with previously approved modifications must be determined by the installer.

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 operated in accordance with the Airplane Flight Manual Supplement (AFMS) identified above. In addition, aircraft with GPS3 interface must also be operated in accordance with the AFMS 190-02885-00, Revision 1, or later FAA-approved revision.

(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) If the 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 (RVSM).

(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 or AFMS 190-00915-N2 Rev 1 or later.

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 Raytheon Aircraft Company Airplane Flight Manual Supplement (AFMS) p/n 130-590031-75, must be attached to the POH/AFM for improved performance operation.

(9) This STC has not been shown to be compatible with the Rockwell Collins Pro Line Fusion installation effective at Serial Numbers (B200GT) BY-207, BY-239, BY-250 and after, (B200CGT) BZ-1 and after, (B300) FL-954, FL-1010, FL-1031 and after, (B300C) FM-66 and after; or those aircraft modified by installation of Pro Line Fusion.

(10) 14 CFR 23.2005 certification level and performance level: for Model 200 series: Level 3, High Speed for Model 300 series, Level 4, High Speed (continued on Page 4) This

United States of America Department of Transportation TOMINI STRAND Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01535WI-D date 8/22/2025 Limitations and Conditions: (Continued)

(11) The optional Autothrottle and Emergency Autoland systems are approved for the Model 200 series (except A200 series) and require MDL 005-00421-00 Rev 39 or later and AFMS 190-00915-N2 Rev 8 or later.

(12) The optional Autothrottle system is approved for the Model 300 and 300LW and requires MDL 005-00629-00 Rev 34

(13) The optional Autothrottle and Emergency Autoland systems are approved for the Model B300 and B300C (except heavyweight configuration) and require MDL 005-00629-00 Rev 34 or later and AFMS 190-00716-N3 Rev 8 or later.

*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 Amat Section Amdt Section Amat

23.143 23-50 23.607 23-48 23.954 a,b,c 23-7

23.181 b 23-45 23.609 Original 23.1141 c, d, e 23-51

23.207 a, b 23-7 23.611 23-48 23.1301 23-20

23.251 23-45 23.613 a,b,c 23-45 23.1303 a,b,d,f 23-49

23.301 a 23-48 23.627 Original 23.1305 a(2)(3), c(1)(2)(5), e(1) 23-52

23.303 Original 23.671 Original 23.1307 23-49

23.305 23-45 23.677 a,d 23-49 23.1308 a,b,c 23-57

23.307 a Original 23.681 a Original 23.1309 a(1)(3),b,c,d,e,f 23-49

23.337 23-48 23.683 23-7 23.1311 a,b,c 23-49

23.365 d Original 23.685 a,b,c,d 23-17 23.1321 23-49

23.395 a(1) 23-7 23.689 a,b,c,d,e 23-7 23.1322 23-43

23.397 23-45 23.771 a 23-14 23.1323 a,b,c 23-49

23.561 e 23-34 23.713 a(2) 23-45 23.1325 a,b,e 23-50 *23.571 a, C 23-48 23.777 a, b 23-51 23.1327 23-20 *23.572 a(1)(3),b 23-48 23.779 a 23-51 23.1329 a,b,c,d,e,f,g,h 23-49 *except B300/B300C 23.781 (b) 23-33 23.1331 a, b(1) 23-43

23.573 b 23-48 23.853 a 23-49 23.1335 23-20

23.575 23-48 23.863 23-34 23.1351 a,g 23-49

23.601 Original 23.867 a,b,c 23-49 23.1353 h 23-49

23.603 23-23 23.901 a,e 23-53 23.1357 a,b,c,d 23-43

23.605 a 23-23 23.903 b(2), c 23-62 23.1359 23-49 (continued on Page 5) This

United States of America Department of Transportation VAAISTRAD Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01535WI-D date 8/22/2025 *Certification Basis (Cont.)

Section Amdt Section Amdt Section Amdt

23.1361 b 23-49 23.1529 23-26 23.2000 23-64

23.1365 a,b,d,e 23-49 23.1541 a,b 23-21 23.2005 23-64

23.1367 Original 23.1543 b,c 23-50 23.2010 23-64

23.1381 a,b Original 23.1545 a,b,d 23-50* 23.2500 23-64

23.1419 a,c 23-43 *A200/A200CT only, Amdt 23-7 23.2505 23-64

23.1431 a,b,e 23-49 23.1549 23-45 23.2510 23-64

23.1435 a(1) (3)(4), b 23-49 23.1555 a,b,e(2) 23-50 23.2515 23-64

23.1501 23-21 23.1581 a,b(1)(3), c,d,f 23-50 23.2520 23-64

23.1521 a, b(1) (3)(4)(5) 23-50 23.1583 e,h,m 23-50 23.2600 a,b 23-64 c(1) (3)(4) 23.1585 a(1),d(1), f(1),j 23-50 23.2605 23-64

23.1523 23-34

23.1525 23-45 Additional requirements for the Models 300 and 300LW:

Section Amat

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 Amat

23.149 a,b,c,d,e,f

23.574 23-48

23.672 b, c 23-45

23.1303 e,g 23-49

23.1309 a(4) 23-49

23.1323 e 23-49 -- END -- This