# STC SA01268WI-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Rockwell Collins Inc, United States - Description: Installation of Collins Pro Line 21 Avionics System - Applied: August 26, 2004 - Status date: August 14, 2013 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/7f/65/7f657626177180947023d669d71128682eadf4984f0b9d73a9d61d15fae755c4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5727C501EF758F9186257CD8005E3CEC.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01268WI-D ## ADs that name it (0) None. ## Approved models (2) - Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/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 SA01268WI-D This certificate, issued to Part 23 of the Federal Aviation Regulations. Original Product--Type Certificate Number : A24CE Make : Hawker Beechcraft Corporation (formerly Raytheon) Model : B200 King Air, S/N BB-1769 B200C King Air, S/N BW-01 through BW-29 Description of Type Design Change: Installation of Rockwell Collins, Inc. Pro Line 21 Avionics System in accordance with: (1) Master Drawing List RCA-0129, Revision F, dated August 14, 2013; (2) Maintenance Manual Supplement RCA-0019-001 (B200), Revision -, dated October 15, 2004; (3) Airplane Flight Manual Supplement RCA-0028-001 (B200), Revision -, dated October 15, 2004; (4) Maintenance Manual Supplement (B200C) RCA-0109, Revision D, dated June 5, 2013; (5) Airplane Flight Manual Supplement (B200C) RCA-0110, Revision D, dated May 30, 2013; or later approved/accepted revisions for items (1), (2), (3), (4) or (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. Rockwell Collins, Inc. 400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Date of application : August 26, 2004 Date of issuance : October 15, 2004 Date reissued : Date amended : February 16, 2006; May 7, 2007, August 14, 2013 (Signature) Steven P. Brune STC ODA Administrator, ODA-500864-CE (Title) Number SA01268WI-D August 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 the Hawker Beechcraft (formerly Raytheon) B200 is as follows: (1) The type certification basis for the Hawker Beechcraft (formerly Raytheon) B200 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, August 26, 2004, is as follows: Hawker Beechcraft B200 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend. 23.29 (a)(b) Orig. 23.771 (a) Orig. 23.1331 (a)(b) Orig. 23.301 (a) Orig. 23.777 (a)(b) 7 23.1335 All 20 23.303 All Orig. 23.867 (a)(b) 7 23.1351 (a)(c) 7 23.305 (a)(b) Orig. 23.901 (a)(b) 7 23.1357 (a)(b)(c)(d) Orig. 23.307 (a) Orig. 23.1301 (a)(b)(c)(d) 20 23.1367 (a)(b)(c)(d) Orig. 23.365 (a)(b)(c)(d) Orig. 23.1303 (a)(b)(c) Orig. 23.1381 (a)(b)(c) Orig. 23.397 (a)(b) 7 23.1305 (a)(c) 7 23.1431 All Orig. 23.561 (a)(b) 7 23.1309 (a)(b)(c)(e) 41 23.1523 All Orig. 23.601 All Orig. 23.1311 (a)(b) 41 23.1525 All Orig. 23.603 (a)(b) Orig. 23.1321 (a)(b)(c)(d)(e) 41 23.1529 All 8 23.605 All Orig. 23.1322 (a)(b)(c)(d) 17 23.1545 (a) 23 23.607 All Orig. 23.1323 (a) 7 23.1545 (b)(c) 7 23.609 (a)(b) Orig. 23.1323 (b) 49 23.1547 (a)(b)(c)(d) Orig. 23.611 All 7 23.1325 (a)(b) 6 23.1549 (a)(b)(c)(d) Orig. 23.613 (a)(b)(c) Orig. 23.1327 (a)(b) Orig. 23.1583 (h) 10 23.677 (a)(b)(c) 7 23.1329 (a)(b)(d)(e)(f) Orig. 23.1585 (a) 7 Number SA01268WI-D August 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 the Hawker Beechcraft (formerly Raytheon) B200C is as follows: (1) The type certification basis for the Hawker Beechcraft (formerly Raytheon) 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 amended, May 7, 2007, is as follows: Hawker Beechcraft B200C 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend. 23.29 (a)(b) 21 23.672 (a)(b)(c) Orig. 23.1329 (e)(f) Orig. 23.301 (a) 48 23.771 (a) 14 23.1331 (a)(b) Orig. 23.303 All Orig. 23.777 (a)(b) 14 23.1335 All 20 23.305 (a)(b) 45 23.867 (a)(b) 49 23.1351 (a)(c) 49 23.307 (a) Orig. 23.901 (a)(b) 53 23.1357 (a)(b)(c)(d) 51 23.365 (a)(b)(c)(d) Orig. 23.1301 (a)(b)(c)(d) 20 23.1367 (a)(b)(c)(d) Orig. 23.397 (a)(b) 7 23.1303 (a)(b)(c) 49 23.1381 (a)(b)(c) Orig. 23.561 (a)(b) 48 23.1305 (a)(c) 52 23.1431 (a)(b)(c)(e) 49 23.601 All Orig. 23.1309 (a)(b)(c)(e) 49 23.1501 (a)(b) 23 23.603 (a)(b) 23 23.1311 (a)(b) 49 23.1523 All 34 23.605 All Orig. 23.1321 (a)(b)(c)(d)(e) 49 23.1525 All 45 23.607 All 48 23.1322 (a)(b)(c)(d)(e) 43 23.1529 All 26 23.609 (a)(b) Orig. 23.1323 (b) 49 23.1549 (a)(b)(c)(d) Orig. 23.611 All 48 23.1325 (a)(b) 50 23.1581 (a)(b)(c) 50 23.613 (a)(b)(c) 45 23.1327 (a)(b) 20 23.1583 (h) 10 23.671 (a)(b) Orig. 23.1329 (a)(b)(d) 49 23.1585 (a) 7 Number SA01268WI-D August 14, 2013 (3) After the initial certification basis of the Hawker Beechcraft B200C for parts changed or affected by this change since the reference date amended, August 14, 2013, the differences are as follows: Hawker Beechcraft B200C 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend. 23.251 All Orig. 23.615 (a) 7 23.1331 (a)(b)(c) 62 23.301 (a)(b) Orig. 23.619 All 7 23.1335 All 20 23.303 All Orig. 23.625 (a)(b)(c) 7 23.1351 (a)(1)(2)(i)(b)(1) 49 23.305 (a)(b) Orig. 23.627 All Orig. 23.1353 (h) 49 23.307 (a) Orig. 23.867 (a)(b) 49 23.1357 (a)(b)(c) 43 23.321 (a) Orig. 23.1301 (a)(b)(c) 62 23.1359 (c) 49 23.341 All 7 23.1303 (a)(b)(c)(e) 62 23.1365 (a)(b)(d)(e) 49 23.365 (a)(b)(c)(d) Orig. 23.1305 (a)(c)(e) 52 23.1367 (a)(b)(c)(d) Orig. 23.561 (a)(b) 7 23.1306 (a)(b) 61 23.1431 (a)(b)(e) 62 23.571 (a) Orig. 23.1308 (a)(b)(c) 57 23.1501 (a)(b) 21 23.601 All Orig. 23.1309 (a)(1)(2)(b)(c)(d) 62 23.1545 (d) 62 23.603 (a)(b) Orig. 23.1311 (a)(b)(c) 62 23.1547 (a)(b)(c)(d)(e) 20 23.605 All Orig. 23.1321 (a)(b)(c)(d)(e) 49 23.1549 (a)(b)(c)(d) 45 23.607 All Orig. 23.1322 (a)(b)(c)(d)(e) 43 23.1581 (a)(b)(1)(3)(c)(d)(f) 50 23.609 (a) Orig. 23.1323 (a) 62 23.1583 (h)(m) 62 23.611 All 7 23.1327 (a)(1)(2)(b) 20 23.1585 (a)(j) 62 23.613 (a)(b)(c) Orig. 23.1329 (h) 49 ----------------------------------------End---------------------------------------- ## Every issue (4) - August 14, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/7f/65/7f657626177180947023d669d71128682eadf4984f0b9d73a9d61d15fae755c4) - May 7, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3a/a2/3aa2b3c4ca213f2ccd0fed20b33836237107e14c66f27abfffe14304dfcf92b9) - February 16, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/5f/88/5f8873b8a21656d8b1d11ba079b380a5c85ce24c24dd84fd8467a3ccb89fa1dd) - October 15, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/95/e2/95e2b8a23bfc1bab26ba20ce13096f8abec16eeaca9aa529e0a959162094283b) --- 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.