# STC SA01964WI - Type: Supplemental type certificate - Status: Current, Issued - Holder: Rockwell Collins Inc., United States - Description: Modification of Rockwell Collins Radio Interface Unit (RIU) SXM Receiver and Pro Line Fusion display system software - Applied: June 10, 2020 - Status date: December 7, 2021 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS 3A20](https://openairdocs.org/tcds/3A20) - Certificate PDF: https://openairdocs.org/files/sha256/50/dc/50dc04f81a6d594736da285ed073450aff8282fbb24a517d48c17dae13673b85 - Approved model list and other attachments: [SA01964WI_AML.pdf](https://openairdocs.org/files/sha256/7d/58/7d588038b87a6b32ba78a85dfea85f371e6a4c2b656b7bac61f572930c4e5ab7) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186909461720230223213909.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01964WI ## ADs that name it (0) None. ## Approved models (11) - Textron Aviation Inc. B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. C90GTi ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01964WI 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 Make: See attached FAA Approved Model List (AML) RCA-0671, Revision (-), dated December 07, 2021 Type Certificate Number: Model: See attached FAA Approved Model List (AML) RCA-0671, Revision (-), dated December 07, 2021 Description of Type Design Change: Modification of Rockwell Collins Radio Interface Unit (RIU), SXM Receiver and Pro Line Fusion Display System Software in accordance with: (1) FAA Approved Model List (AML) RCA-0671, Revision (-), dated December 07, 2021; (2) Instructions for Continued Airworthiness RCA-0673, Revision (-), dated August 13, 2021 or later FAA approved/accepted revision for items (1) and (2) See continuation sheet (page 3 of 4) for the applicable Airplane Flight Manual Supplements. Approval of this change in type design applies to the above model aircraft only; (2) A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft; (3) The installer must determine whether this design change is compatible with previously approved modifications; (4) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission; (5) Aircraft affected by Airworthiness Directive 2021-05-17 must be equipped with software specified in Rockwell Collins Service Information Letter FDSA-6500-19-1 prior to installation of this type design change. (6) For model specific limitations, see AML RCA-0671, Rev. (-), or later approved revisions. Note: This design change has been determined to be a no acoustic change in accordance with 14 CFR 21.93(b). Date of Application: June 10, 2020 Date Reissued: Date of Issuance: December 07, 2021 Date Amended: By Direction of the Administrator Thomas W, Shadle Title: STC ODA Assistant Administrator, ODA-500864-CE (Ref, 14 CFR 21.120). United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01964WI Signature of grantor. specifications, flight manual supplements, etc.) is the property of the STC hoider. 14 CFR 21 120). FAA For 8110-2 (03/21) Page 2 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01964WI December 07, 2021 Description of Type Design Change: Continued: (3) Airplane Flight Manual Supplement C90GTi RCA-0665, Revision (-), dated January 28, 2021 (4) Airplane Flight Manual Supplement C90GTi RCA-0679, Revision (-), dated January 28, 2021 (5) Airplane Flight Manual Supplement B200GT/B200CGT RCA-0680, Revision (-), dated January 28, 2021 (6) Airplane Flight Manual Supplement B200GT/B200CGT RCA-0667, Revision (-), dated January 28, 2021 Airplane Flight Manual Supplement B200GT/B200CGT RCA-0681, Revision (-), dated January 28, 2021 (8) Airplane Flight Manual Supplement B200GT/B200CGT RCA-0682, Revision (-), dated January 28, 2021 (9) Airplane Flight Manual Supplement B200/B200C RCA-0678, Revision (-), dated January 28, 2021 (10) Airplane Flight Manual Supplement B300/B300C RCA-0668, Revision (-), dated January 27, 2021 (11) Airplane Flight Manual Supplement B300/B300C RCA-0683, Revision (-), dated January 28, 2021 12) Airplane Flight Manual Supplement B300/B300C Heavy Weight RCA-0684, Revision (-), dated January 28, 2021 (13) Airplane Flight Manual Supplement B300/B300C or B300ER RCA-0685, Revision (-), dated April 9, 2021 (14) Airplane Flight Manual Supplement B300/B300C (B300ER) RCA-0686, Revision (-), dated January 25, 2021 (15) Airplane Flight Manual Supplement B300/B300C (B300ER) RCA-0669, Revision (-), dated January 28, 2021 (16) Airplane Flight Manual Supplement B300/B300C (B300ER) RCA-0670, Revision (-), dated January 28, 2021 (17) Airplane Flight Manual Supplement B300/B300C RCA-0692, Revision (-), dated January 28, 2021 or later FAA approved revision for items (3), (4), (5), (6), (7), (8), (9), (10), (11), (12), (13), (14), (15), (16), and (17). 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 FAA Approved Model List (AML) No. RCA-0671 is as follows: a. _The type certification basis for all Models included in AML No. RCA-0671 is included in the applicable TCDS as listed on the FAA approved AML for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by this change since the reference date of application, June 10, 2020 is based upon Part 23 as amended by Amendment 23-61. Data Pertinent to B300/B300С 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend. 23.301 (a) 42 23.1305 (c)(5) 52 23.1431 (aXb) 49 23.303 Orig 23.1306 (a)(b) • 61 23.1521 (a)(b)(])(c)(!) 50 23.305 (a)b) 45 23.1308 (a)b)(c) 57 23.1529 26 23.601 Ong 23.1309 [(a)(1)(4)(b)(1)(2)(3)(4)(c) (1)(2)(i)(3)(d)(e) 49 23.1549 (a)(b)(c) 45 23.603 (a)(b) 23 23.1322 (axb) (c)(d) 43 23.1555 (ayb) 50 23.605 (a) 23 23.1327 (a)I) (2)(b) 20 23.1581 (a)2)(b)(1)(3)(cXd)(D 50 23.867 (axb)(])(2)(c)(])(2) 49 23.1351 (a)(1)(2)(iї) 49 23.1583 (h)(m) 50 23.1301 (a)(b)(c)(d) 20 23.1353 (h) 49 23.1585 (a)Ui) 50 This (Ret. 14 CFR 21.55). FAA For 8110-2 (03/21) Page 3 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01964WI December 07, 2021 Data Pertinent to B200/B200C/B200CGT/B200CT 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend. 23.301 (a)(b) 48 23.1305 (e) 34 23.1431 (a)(b) 49 23.303 Orig 23.1306 (a)(b) 61 23.1521 (a)(b)(I)(c)(I) 50 23.305 (a)(b) 23.1308 (a)(b)(c) 57 23.1529 26 23.601 Orig 23.1309 (a)(1)(3)(b)(1)(2)(3)(4)(c) (1)(2) (i) (3)(d)(e) 23.1549 (a)(b)(c) 45 23.603 (a)(b) 23 23.1322 (a)(b)(c)(d) 23.1555 (a)(b) 50 23,605 (a) 23 23.1327 (a)(1)(2)(b) 20 23.1581 ((a)(2)(b)(1)(3)(c)(d)(f) 50 23.867 (a)(b)(])(2)(c)(])(2) 49 23.1351 (a)()(2)0) 49 23.1583 (h)(m) 50 23.1301 (a)b)(c)(d) 20 23.1353 (h) 49 23.1585 (a)(j) 50 Data Pertinent to C90GTi CAR Amend. CAR Amend. CAR Amend. **3.171 (CAR3) 3-0 3.173 (CAR3) 3-0 3.293 (CAR 3) 3-0** 3.172 (CAR3) 3-0 3.292 (CAR 3) 3-0 14 CFR Part Amend. 14 CFR Part Amend 14 CFR Part Amend 23.601 Orig 23.1322 (a)(b)(c)(d) 43 23.1549 _(a)(b)(c) 45 23.867 (a)(b)(I) 49 23.1327 (a)(])(2)(b) 20 23.1555 _(a)(o) 50 23.1301 (a)(b)(c)(d) 20 23.1351 (a)(1)(2)(i) 49 23.1581 (a)(2)(b)(1)(3)(c)(d)() 50 23.1305 (c)(5) 52 23.1353 (h) 49 23.1583 (h)(m) 50 23.1306 (a)b) 61 23.1431 (a)(b) 49 23.1585 (a)U) 50 23.1308 (a)(b)(c) 57 23.1521 (a)(b)(I)(c)(1) 50 23.1300 (a)I)(3)(b)(|)(2)(3)(4) (c)(1)(2) (i)(3) (d)(e) 49 23.1529 26 --END This certicate may be bansferred or made available to third persons by licensing agreements in accordance with Title 14 of the Code of Federal Regulations, part 21, section 21.47 (14 CFR 21,47). A transfer must be endorsed as sovided on the reverse heredf. A Type Certicate holder who allows a person to use the Type Certificale lo manufacture a new aircran, accrat engine, or propeller must provide that person with a wntten licensing agreement acceptable to the FAA. (Raf. 14 CFR 21.55). FAA For 8110-2 (03/21) Page 4 of 4 ### SA01964WI_AML.pdf Some pages are OCR from the scanned FAA attachment. OCR can misread letters and numbers. Rock Collins **APPROVED MODEL LIST (AML)** **PRO LINE FUSION SOFTWARE/SXM WEATHER** UPDGRADE 14 CFR PART 23 AIRCRAFT STC SA01964WI RCA-0671 Revision: (-) December 07, 2021 FAA APPROVED BY: December 7, 2021 Thomas W. Shadle FAA Approved Date STC ODA Assistant Administrator ODA-500864-CE Date Amended: RCA-0671, Revision (-) 1 of 7 FAA Approved Model List NOTE(S): This document is maintained in the Aircraft Certification Center configuration management system. Revisions to this document are identified by change bars (I) outside the right margin of the page modified. CAGE Code: OEFDO SIGNATURES Name Signature Colin D. Reed Date: 2021, 12d by Col. D. Reed • Date: 2021.12.07 07:44:19 -06'00 Prepared by: Colin D. Reed Checked by: James B. Scroggs James B. Scroggs Scroggs Digitally signed by James B. Date: 2021.12.07 07:54:50 -06'00' Digitally signed by Gene L. Baker Gene L. Baker email-gene.baker@collins.com, c-us • DN: cn=Gene L. Baker, o, ou, Approved by: Gene L. Baker Date: 2021.12.07 08:18:35 - 06'00 RCA-0671, Revision (-) 2 0f7 FAA Approved Model List AML AMENDMENT / REVISION LOG Rev Page(s) Description Date (-→ All Original release 12/07/2021 RCA-0671, Revision (-) 3 of 7 FAA Approved Model List RCA-0671, Revision (-) 4 of 7 2. INTRODUCTION This document is the FAA Approved Model List for STC No. SA01964WI for the modification of Rockwell Collins, Inc. Pro Line Fusion System in 14 CFR Part 23 Aircraft. It is the responsibility of the installer to ensure the existing aircraft equipment configuration is compatible with this STC. Refer to Modification Instructions RCB-2001 for the approved equipment replacements. FAA Approved Model List APPROVED MODEL LIST FAA Approved Model List (AML) No. SA01964WI Modification of Rockwell Collins Radio Interface Unit (RIU), SXM Receiver and Pro Line Fusion Display System Software Item Make Model Certificate Type Supplemental Type Design Data1 Amdt AML Data Sheet and Limitations Date 1 Textron B300 A24CE Installation Instructions: Aviation Inc. B300C Revision 123 Drawing Index, RCA-0672, Rev. F 10/21/2019 Airplane Flight Manual Supplement 2: • RCA-0668 3, Rev - • RCA-0669 4, Rev - • RCA-0670 5, Rev - RCA-0685 6, Rev - RCA-0686 , Rev - RCA-0683 8, Rev - RCA-0684 , Rev - • RCA-0692 10, Rev - Instructions for Continued Airworthiness: RCA-0673, Rev. - Limitations: Type Design Change limited to Textron Aviation B300/B300C models that have installed Rockwell Collins STC SA01784WI Pro Line Fusion® and have IOC-3100 Part Number 822-1361-622 installed. • Type Design Change limited to Textron Aviation B300/B300C models that have factory installed Pro Line Fusion® (Serial Numbers FL-954, FL-1010, FL-1031 and after, FM-66 and after) and have IOC-3100 Part Number 822-1361- 622 or 822-1361-623 installed. 1 Or later FAA approved/accepted revisions 2 Airplanes with IOC-3100 Part Number 822-1361-623 do not require an AFMS. 3 Pro Line Fusion® installed by STC SA01784WI, B300/B300C equipped with federated TAWS 4 Pro Line Fusion® installed by STC SA01784WI, B300/B300C with Extended Range equipped with federated TAWS 5 Pro Line Fusion® installed by STC SA01784WI, B300/B300C (B300ER) with Extended Range with PT6A-67A Engines equipped with federated TAWS 6 Pro Line Fusion® installed by STC SA01784WI, B300/B300C and B300/B300C (B300ER) with Extended Range with PT6A- 67A Engines equipped with iTAWS 7 Pro Line Fusion® installed by STC SA01784WI, B300/B300C with Extended Range equipped with TAWS 8 Pro Line Fusion® installed at Factory, B300/B300C equipped with federated TAWS 9 Pro Line Fusion® installed at Factory, B300/B300C Heavy Weight equipped with federated TAWS 10 Pro Line Fusion® installed at Factory, B300/B300C and equipped with TAWS RCA-0671, Revision (-) 5 of 7 FAA Approved Model List Item Make Model Certificate Data Sheet Type and Limitations Supplemental Type Design Data11 AML Amdt Date 2 Textron B200 A24CE Installation Instructions: Aviation Inc. B200C Revision 123 Drawing Index, RCA-0672, Rev. F B200GT 10/21/2019 Airplane Flight Manual Supplement 12; B200CGT RCA-0667 13, Rev. - RCA-0678 14 , Rev - Instructions for Continued Airworthiness: RCA-0673. Rev. - Limitations: Type Design Change limited to Textron Aviation B200/B200C or B200GT/B200CGT models that have installed Rockwell Collins STC SA01769WI Pro Line Fusion® and have IOC-3100 Part Number 822- 1361-622 installed. • Type Design Change limited to Textron Aviation B200GT/B200CGT models that have factory installed Pro Line Fusion® (Serial Numbers BY-207, BY-239, BY-250 and after, BZ-1 and after) and have IOC-3100 Part Number 822-1361-622 or 822-1361-623 installed. 11 Or later FAA approved/accepted revisions 12 Airplanes with IOC-3100 Part Number 822-1361-623 do not require an AFMS. 13 Pro Line Fusion® installed under STC SA01769WI, B200GT/B200CGT equipped with iTAWS 14 Pro Line Fusion® installed under STC SA01769WI, B200/B200C equipped with ITAWS 15 Pro Line Fusion® installed under STC SA01769WI, B200GT/B200CGT equipped with federated TAWS 16 Pro Line Fusion® installed at Factory, B200GT/B200CGT equipped with iTAWS 17 Pro Line Fusion® installed at Factory, B200GT/B200CGT equipped with federated TAWS RCA-0671, Revision (-) 6 0f7 FAA Approved Model List Item Make Model Certificate Type Supplemental Type Design Data 18 AML Amdt Data Sheet and Limitations Date Textron C9OGTi 3A20 Installation Instructions: Aviation Revision 82 Drawing Index, RCA-0672, Rev. F 09/05/2019 Airplane Flight Manual Supplement: RCA-0665 19 RCA-0679 20' Rev. - , Rev. - Instructions for Continued Airworthiness: RCA-0673, Rev. - Limitations: • Type Design Change limited to Textron Aviation C90GTi models that have installed Rockwell Collins STC SA01792WI Pro Line Fusion® and have IOC-3100 Part Number 822-1361-622 installed. Type Design Change limited to Textron Aviation C90GTi models that have factory installed Pro Line Fusion® (Serial Number LJ-2129 and after) and have IOC- 3100 Part Number 822-1361-622 installed under Rockwell Collins STC SA01857WI. 18 Or later FAA approved/accepted revisions 19 Pro Line Fusion® installed under STC SA01792WI 20 Pro Line Fusion® installed at Factory RCA-0671, Revision (-) 7 of7 ## Every issue (1) - December 7, 2021: Issued, Current. [certificate](https://openairdocs.org/files/sha256/50/dc/50dc04f81a6d594736da285ed073450aff8282fbb24a517d48c17dae13673b85), [SA01964WI_AML.pdf](https://openairdocs.org/files/sha256/7d/58/7d588038b87a6b32ba78a85dfea85f371e6a4c2b656b7bac61f572930c4e5ab7) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.