# STC SA01784WI - Type: Supplemental type certificate - Status: Current, Amended - Holder: Rockwell Collins Inc - Description: Installation of Rockwell Collins, Inc. Pro Line Fusion - Status date: September 28, 2017 - Data sheets: A24CE, A24CE - Certificate PDF: https://openairdocs.org/files/sha256/a1/62/a1621f946a6b9d92426bfe468fc8eef44a9fef1eb8787dc8ea7871aa21e7a600 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A91A499896B1272286258218004DE9AA.0001 - Page: https://openairdocs.org/stc/SA01784WI ## ADs that name it None. ## Approved models (2) - Beechcraft Corporation B300 (TCDS A24CE) - Beechcraft Corporation B300C (TCDS A24CE) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. Number: SA01784WI 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 Inc. Model: B300 B300C Description of Type Design Change: Installation of Rockwell Collins, Inc. Pro Line Fusion® in accordance with: (1) Master Drawing List RCA-0430, Revision (-), dated May 4, 2015; (2) Instructions for Continued Airworthiness RCA-0449, Revision (-), dated May 4, 2015; TABLE 1 - Pro Line Fusion ® without the Integrated Terrain Awareness and Warning System (ITAWS) (3) Airplane Flight Manual Supplement B300/B300C RCA-0434, Revision (-), dated May 4, 2015; (4) Airplane Flight Manual Supplement B300/B300C (B300ER) RCA-0522, Revision (-), dated May 4, 2015; (5) Airplane Flight Manual Supplement B300/B300C (B300ER) RCA-0550, Revision (-), dated January 11, 2016; TABLE 2 - Pro Line Fusion ® that includes the Integrated Terrain Awareness and Warning System (ITAWS) (6) Airplane Flight Manual Supplement B300/B300C RCA-0604, Revision (-), dated March 9, 2017; (7) Airplane Flight Manual Supplement B300/B300C (B300ER) RCA-0605, Revision (-), dated February 28, 2017; (8) Airplane Flight Manual Supplement B300/B300C (B300ER) RCA-0606, Revision (-), dated February 28, 2017; or later approved/accepted revision for items (1), (2), (3), (4), (5), (6), (7), and (8). (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) For aircraft model B300C, Beechcraft Corporation Kit – Cargo Wiring Modification document number 101-3299 must be installed prior to this modification; (Limitations and Conditions continued on Page 3) Date of Application: April 2, 2014 Date Reissued: Date of Issuance: May 4, 2015 Date Amended: June 7, 2016; September 28, 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 righ ts to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. FAA Form 8110-2 (5/14) Page 1 of 4 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 de sign data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. FAA Form 8110-2 (5/14) Page 2 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01784WI September 28, 2017 (6) For Master Drawing List RCA-0430 Table 1 installations, No. 1 and No. 2 VHF-4000 or VHF-4000E radio transceiver part number 822-1468-110 or 822-1872-110 must be installed prior to or in concurrence with this modification; (7) Equivalent Level of Safety Findings have been made for the following regulations: 14 CFR 23.1305(a)(2), (a)(3), (c)(2), and (c)(5) Amendment 23-52; 14 CFR 23.1311(a)(6), Amendment 23-49; 14 CFR 23.1549(a), (b), and (c), Amendment 23-45; Refer to ELOS Memo ACE-15-06. (8) Applicability:  Aircraft Serial Number FL-493, FL-500 and After; FM-14 and After.  Aircraft Serial Number FL-938 and After; FM-57 and After. (Heavy Weight Aircraft with or without Extended Fuel Capabilities)  Aircraft Serial Number FL-1 and After; FM-1 and After with FAA STC SA01177WI-D or SA01267WI-D installed. (9) The Pro Line Fusion installation is limited to Textron Aviation B300/B300C aircraft with:  Pratt & Whitney Canada Corp. PT6A-60A Engines with Hartzell Propeller, Inc. HUBS: HC-B4MP-3C / BLADES: M10476K or M10476NK.  Pratt & Whitney Canada Corp. PT6A-67A Engines with Hartzell Propeller, Inc. HUBS: HC-E4A-3M / BLADES: E10478SK FAA Form 8110-2 (5/14) Page 3 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01784WI September 28, 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 Inc. B300/B300C is as follows: (1) The type certification basis for the Textron Aviation Inc. B300/B300C 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, April 2, 2014 is based upon Part 23 as amended by Amendment 23-51. Textron Aviation Inc. B300/B300C 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend. 23.251 Orig. 23.901 (a)(e) 34 23.1351 (a)(2)(ii) 49 23.301 (a) 42 23.903 (b)(2) 29 23.1353 (h) 49 23.301 (b) 28 23.937 (a) 43 23.1357 (a)(b)(c)(d) 43 23.303 Orig. 23.1141 (g)(2) 18 23.1359 (c) 49 23.305 (a)(b) 45 23.1203 (a)(d) 18 23.1361 (a)(b)(c) 20 23.307 (a) Orig. 23.1301 (a)(b)(c)(d) 20 23.1365 (a)(b)(d)(e) 49 23.365 (a)(b)(c)(d) Orig. 23.1303 (a)(b)(c)(e)(f)(g) 49 23.1367 (a)(b)(c)(d) Orig. 23.561 (e) 34 23.1305 (a)(2)(3)(5) (c)(1)(2)(3)(4)(5)(6)(7)(e)(1)(2) 52 23.1419 (b) 14 23.571 (a)(b) 34 23.1431 (a)(b)(e) 49 23.601 Orig. 23.1306 (a)(b) 61 23.1501 (b) 21 23.603 (a)(b) 23 23.1308 (a)(b)(c) 57 23.1521 (a)(b)(1)(3)(4)(c)(1)(3) 50 23.605 (a) 23 23.1309 (a)(1)(3)(4)(b) (c)(1)(2)(i)(iii)(3)(d)(e) 49 23.1523 (a)(b)(c) 34 23.607 (a)(b)(c) 48 23.1525 45 23.609 (a)(b) Orig. 23.1311 (a)(b)(c) 49 23.1529 26 23.611 48 23.1321 (a)(b)(c)(d)(e) 49 23.1543 (b)(c) 50 23.613 (a)(b)(c)(d)(e) 45 23.1322 (a)(b)(c)(d)(e) 43 23.1545 (d) 50 23.625 (a)(b)(c) 7 23.1323 (a)(c)(e) 49 23.1547 (a)(b)(c)(d)(e) 20 23.627 Orig. 23.1325 (a)(b)(1)(2)(ii) 50 23.1549 (a)(b)(c)(d) 45 23.773 (a)(1)(2) 14 23.1327 (a)(1)(2)(b) 20 23.1555 (a) 50 23.777 (a)(b) 51 23.1329 (c)(h) 49 23.1581 (a)(2)(b)(1)(3)(c)(d)(f) 50 23.853 (a)(d)(3)(iv) 34 23.1331 (a)(b)(c) 43 23.1583 (h)(m) 50 23.867 (a)(b)(c) 49 23.1335 20 23.1585 (a)(j) 50 --------------------------------------------------------END-------------------------------------------------------- FAA Form 8110-2 (5/14) Page 4 of 4 ## Every issue (3) - September 28, 2017: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a1/62/a1621f946a6b9d92426bfe468fc8eef44a9fef1eb8787dc8ea7871aa21e7a600) - June 7, 2016: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/91/12/9112cd1e1117f311376fc49a71f180389e9d4a98c12dea935c99624416e8243d) - May 4, 2015: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/01/9d/019d54a5aa9cfe009675e59a1cc26ef197955575e2642e21874167ad286146ec) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.