# STC SA015444WI-D - Type: Supplemental type certificate - Status: Current, Issued - Holder: Rockwell Collins Inc, United States - Description: Modification of a Rockwell Collins, Inc. AFD-3010 and AFD-3010E Adaptive Flight Display Installation in Part 23 Aircraft. - Applied: March 9, 2009 - Status date: February 11, 2010 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A1WI](https://openairdocs.org/tcds/A1WI), [TCDS A27CE](https://openairdocs.org/tcds/A27CE), [TCDS A59EU](https://openairdocs.org/tcds/A59EU), [TCDS A18SW](https://openairdocs.org/tcds/A18SW), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A00010WI](https://openairdocs.org/tcds/A00010WI), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A26CE](https://openairdocs.org/tcds/A26CE) - Certificate PDF: https://openairdocs.org/files/sha256/70/9a/709a50be449b1b86ad9855d3a538b0040d6c870b9d9b3f88ad050c0d8480bc5a - Approved model list and other attachments: [Sa01544WI-D_AML.pdf](https://openairdocs.org/files/sha256/a2/75/a275b1bd0341841bb3b8cf127a7e633c6786ab0aa9b074188d146d5676c8dde1) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AD91673C5800EF98862576FE00646EBD.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA015444WI-D ## ADs that name it (0) None. ## Approved models (28) - Cessna Aircraft Company 501 ([TCDS A27CE](https://openairdocs.org/tcds/A27CE)) - Cessna Aircraft Company 525 ([TCDS A1WI](https://openairdocs.org/tcds/A1WI)) - Cessna Aircraft Company 525A ([TCDS A1WI](https://openairdocs.org/tcds/A1WI)) - Cessna Aircraft Company 525B ([TCDS A1WI](https://openairdocs.org/tcds/A1WI)) - Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 390 ([TCDS A00010WI](https://openairdocs.org/tcds/A00010WI)) - Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation C90GT ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation C90GTi ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation T-34C ([TCDS A26CE](https://openairdocs.org/tcds/A26CE)) - M7 Aerospace LP SA227-DC (C-26B) ([TCDS A18SW](https://openairdocs.org/tcds/A18SW)) - Piaggio Aero Industries S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU)) ## 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: SA01544W1-D This certificate issued to: Rockwell Collins, Inc. 400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 turt * of the * Raqutations. Original Product Type Certificute Vanter: * See attached FAA Approved Model List (AML) No. SA01544WI-D for list of approved airplane Make: models and applicable airworthiness regulations. Description of Type Design Change: Modification of a Rockwell Collins, Inc. AFD-3010 and AFD-3010E Adaptive Flight Display Installation in Part 23 Aircraft in accordance with Rockwell Collins, Inc. Master Drawing List as listed on AML No. SA01544WI-D, Revision -, or later FAA approved revisions. (1) Prior installation and approval of a Rockwell Collins, Inc. AFD-3010 and AFD-3010E Adaptive Flight Display is a prerequisite to this STC. Reference Table 1 (AFD-3010) or Table 2 (AFD-3010E) of Rockwell Collins, Inc. Installation Instructions, document number RCA-2549, Revision -, dated March 25, 2009, or later FAA approved revision, for approved AFD-3010 and AFD-3010E Adaptive Flight Display substitutions. (2) Compatibility of this design change with previously approved modifications must be determined by the installer. (3) A copy of this Certificate and FAA approved AML No. SA01544WI-D issued February 11, 2010, or later FAA approved revision, 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. suspended. rested, renter sination date is etherwise established by the. Administrater of the Federal Cult of application: March 9, 2009 Jat missed : Jat of iss February 11, 2010 Inte unadet : AVIAT By Direction of the Administrator These (Signature) ADMINIS Steven P. Brune Administrator, ODA-500864-CE (Title) a fine of exceeding $1.000, or impr. sonment not exceeding 3 years, or both icate may be transferred in accordance with FAR 21.47 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01544WID Certification Basts: ..... Based on 14 CPR §$ 21.115 and 21.101. and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for all Models included in AML No. SA01544WI-D is as follows: (1) The type certification basis for all Models included in AML. No. SA01544WI-D is included in the applicable TCDS as listed in the PAA approved AML 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, March 9, 2009, is as 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend. 23.867 (a)(b)(c) 49 23.1309 (a)(b)(c)(d)(e) 49 23.1357 (a)(c) 43 23.1301 (a)b)(c)(d) 20 23.1311 (a) 49 23.1381 (a›(b) Orig 23.1308 (d) 57 23.1351 (a)(C) 49 23.1431 (a)(b) 49 47 ### Sa01544WI-D_AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. **FAA APPROVED MODEL LIST (AML) NO. SA01544WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A ROCKWELL COLLINS AFD-3010 AND AFD-3010E INSTALLATION IN 14 CER PART 23 AIRCRAFT Issue Date: February 11, 2009 **INSTALLATION** **ORIGINAL CERTIFICATION INSTRUCTIONS** TYPE BASIS MASTER AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION LIST NO. AND DATE NUMBER/DATE DATE Hawker C90A 3A20 TCDS 3A20 RCA-0188-001 Rev -, 03/25/09 N/A Beechcraft C90GT Revision 69 Corporation C9OGTi July 8, 2009 2 Hawker 200 A24CE TCDS A24CE RCA-0188-001 Rev -, 03/25/09 N/A Beechcraft 200C Revision 98 Corporation 200CT October 28, 2008 200T B200 B200C B200CT B200T 300 300LW B300 B300C B200GT B200CGT 3 Hawker 390 A00010WI TCDS A00010WI RCA-0188-001 Rev -, 03/25/09 N/A Beechcraft Revision 8 Corporation March 26,2007 4 M7 Aerospace LP SA227-DC (C-26B) A18SW TCDS A18SW Revision 4 RCA-0188-001 Rev -, 03/25/09 N/A August 24, 2004 [1] Or later FAA approved revision Page 1 of 2 **FAA APPROVED MODEL LIST (AML) NO. SA01544WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A ROCKWELL COLLINS AFD-3010 AND AFD-3010E INSTALLATION IN 14 CER PART 23 AIRCRAFT Issue Date: February 11, 2009 **INSTALLATION** ORIGINAL CERTIFICATION INSTRUCTIONS ITEM AIRCRAFT MAKE AIRCRAFT MODEL CERTIFICATE NUMBER TYPE ALTERATION BASIS FOR DRAWING MASTER LIST NO. REVISION NO. AND DATE!! NUMBER/DATE SUPPLEMENT AFM AMENDMENT DATE AML 5 Cessna Aircraft 525A 525 A1WI TCDS A1WI Revision 17 RCA-0188-001 Rev -, 03/25/09 N/A Company 525B April 18, 2007 Cessna Aircraft 501 A27CE Revision 17 TCDS A27CE RCA-0188-001 Rev -, 03/25/09 N/A Company October 11, 2007 7 Industries Piaggio Aero P-180 A59EU TCDS A59EU Revision 18 RCA-0188-001 Rev-, 03/25/09 N/A S.p.A November 15, 2007 [1] Or later FAA approved revision FAA Approved: Heres Mana Administrator, ODA-500864-CE Amended: Page 2 of 2 ## Every issue (1) - February 11, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/70/9a/709a50be449b1b86ad9855d3a538b0040d6c870b9d9b3f88ad050c0d8480bc5a), [Sa01544WI-D_AML.pdf](https://openairdocs.org/files/sha256/a2/75/a275b1bd0341841bb3b8cf127a7e633c6786ab0aa9b074188d146d5676c8dde1) --- 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.