STC SA01769WI

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraf t, aircraft engine, or propeller.

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SA01769WI

This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A24CE Make: Textron Aviation Model: B200GT/B200CGT B200/B200C

Description of Type Design Change: Installation of Rockwell Collins, Inc. Pro Line Fusion® in accordance with:

(1) Master Drawing List RCA-0420, Revision (-), dated December 15, 2014;

(2) Airplane Flight Manual Supplement B200GT/B200CGT, RCA-0422, Revision (-), dated December 15, 2014;

(3) Airplane Flight Manual Supplement B200GT/B200CGT, RCA-0603, Revision (-), dated August 7, 2017;

(4) Airplane Flight Manual Supplement B200/B200C, RCA-0609, Revision (-), dated August 7, 2017;

(5) Instructions for Continued Airworthiness RCA-0441, Revision (-), dated December 15, 2014;

or later approved/accepted revision for items (1), (2), (3), (4), and (5).

(1) Approval of this change in type design applies to the above model aircraft only;

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

(3) A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft;

(4) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission;

(5) This design change is not approved for commuter and restricted category airplanes;

(6) Equivalent Level of Safety Findings have been made for the following regulations:

14 CFR 23.1305(b)(c)(e)(k) Amdt 34, 23.1311(a)(6), (a)(7) Amdt 49 and 23.1549 Amdt 45. Refer to ELOS Memo ACE-15-02 dated June 30, 2017;

(7) For model specific limitations, see MDL RCA-0420, Revision (-), or later approved revision.

This certificate and the supporting data whi ch is the basis for approval shall remain in effect until surrendered, suspended, and revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of Application: May 18, 2012 Date Reissued: May 19, 2016

Date of Issuance: December 15, 2014 Date Amended: April 10, 2015 ; September 1, 2016; November 30, 2017

Signature __Original signed by Steve Brune

Title STC ODA Administrator, ODA-500864-CE

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraf t, aircraft engine, or propeller.

FAA Form 8110-2 (5/14) Page 2 of 3

To (Name and address of transferee)

From (Name and address of grantor)

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraf t, aircraft engine, or propeller.

FAA Form 8110-2 (5/14) Page 3 of 3

(Continuation Sheet) Number: SA01769WI November 30, 2017

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are not significant in FAA Order 8110.48, the certification basis for the Textron Aviation B200GT/B200CGT/B200/B200C is as follows:

(1) The type certification basis for the Textron Aviation B200GT/B200CGT/B200/B200C is shown on TCDS A24CE for parts not changed or not affected by the change.

(2) The certification basis for parts changed or affected by this change since the reference date of application, May 18, 2012 is based upon Part 23 as amended by Amendment 23-62.

Textron Aviation B200GT/B200CGT/B200/B200C 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend.

23.251 Orig. 23.901 (a)(e)(1) 53 23.1335 20

23.301 (a)(b) 48 23.903 (b)(2) 62 23.1351 (a)(2)(i) 49

23.303 Orig. 23.937 7 23.1353 (h) 49

23.305 (a)(b) 45 23.1141 (g)(2) 51 23.1357 (a)(b)(c)(d) 43

23.307 (a) Orig. 23.1165 (d) 62 23.1359 (c) 49

23.365 (a)(b)(c)(d) Orig. 23.1203 (a)(d) 51 23.1361 (a)(b) Orig.

23.561 (e) 7 23.1301 (a)(b)(c)(d) 20 23.1365 (a)(b)(d)(e) 49

23.571 (a)(b) 48 23.1303 (a)(b)(c)(e)(f) 49 23.1367 Orig.

23.601 Orig.

23.1305 (b)(c)(e)(j)(k)(m)(n)(q)(s)(t)(w) 34 23.1431 (a)(b)(e) 49 23.603 (a)(b) 23 23.1501 (b) 21

23.605 (a) 23 23.1306 (a)(b) 61 23.1521 (a)(b)(c)(d)(e) 50

23.607 (a)(b)(c) 48 23.1308 (a)(b)(c)(d) 57 23.1525 45

23.609 (a)(b) Orig. 23.1309 (a)(1)(3)(b)(c)(d)(e) 49 23.1529 26

23.611 48 23.1311 (a)(b)(c) 49 23.1543 (b)(c) 50

23.613 45 23.1321 (a)(b)(c)(d)(e) 49 23.1545 (d) 50

23.625 (a)(b)(c) 7 23.1322 43 23.1547 (a)(b)(c)(d)(e) 20

23.627 Orig. 23.1323 (a)(c)(e) 49 23.1549 (a)(b)(c)(d) 45

23.773 (a)(1)(2) 45 23.1325 (a)(b)(1)(2)(ii) 6 23.1555 (a) 50

23.777 (a)(b) 51 23.1327 (a)(1)(2)(b) 20 23.1581 (a)(b)(1)(3)(c)(d)(f) 50

23.853 (a) 34 23.1329 (h) 49 23.1583 (h)(m) 50

23.867 (a)(b)(1)(2)(c)(1)(2) 49 23.1331 (a)(b)(c) 43 23.1585 (a)(j) 50

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