# STC SA01792WI - Type: Supplemental type certificate - Status: Current, Amended - Holder: Rockwell Collins Inc - Description: Installation of Rockwell Collins, Inc. Pro Line Fusion - Status date: October 5, 2016 - Data sheets: 3A20 - Certificate PDF: https://openairdocs.org/files/sha256/79/1c/791ca83dffdc71a5ed254ab93b8d7a6caba3bbf519469c46c092ac7eabca043d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BA11B7CDAD9BF033862580CE0074DCAD.0001 - Page: https://openairdocs.org/stc/SA01792WI ## ADs that name it None. ## Approved models (1) - Beechcraft Corporation C90GTi (TCDS 3A20) ## 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. FAA Form 8110-2 (5/14) Page 1 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01792WI 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: 3A20 Make: Beechcraft Model: C90GTi Description of Type Design Change: Installation of Rockwell Collins, Inc. Pro Line Fusion® in accordance with: (1) Master Drawing List RCA-0465, Revision (-), dated August 31, 2015; (2) Airplane Flight Manual Supplement RCA-0494, Revision (-), dated July 31, 2015; (3) Instructions for Continued Airworthiness RCA-0523, Revision (-), dated July 31, 2015; or later approved/accepted revision for items (1), (2), and (3). (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) 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), (a)(7) Amendment 23-49; 14 CFR 23.1549(a), (b), and (c), Amendment 23-45; Refer to ELOS Memo ACE-15-18. (Limitations and Conditions continued on page 3 of 4) Date of Application: June 24, 2014 Date Reissued: February 24, 2016; May 19, 2016 Date of Issuance: August 31, 2015 Date Amended: October 5, 2016 Signature __Original signed by Steve Brune Title STC ODA Administrator, ODA-500864-CE FAA Form 8110-2 (5/14) Page 2 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate To (Name and address of transferee) From (Name and address of grantor) 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: SA01792WI October 5, 2016 (6) C90GTi without (PEP) Configuration, Beechcraft Corporation STC SA10747SC must be installed prior to this modification; a. Engines: Pratt & Whitney Canada Corp. PT6A-135A b. Propeller: HC-E4N-3N Hubs & D8990SK Blades c. Aircraft Serial Number applicability: LJ-1964, LJ-1966, LJ-1968, LJ-1972, LJ-1977 and After (7) C90 GTi (PEP) Configuration, Beechcraft Corporation STC SA10747SC, BLR Aerospace LLC STC SA02054SE, and Raisbeck Engineering STC SA3593NM and SA4010NM must be installed prior to this modification; a. Engines: Pratt & Whitney Canada Corp. PT6A-135A b. Propeller: HC-D4N-3C Hubs & D9510SK Blades c. Aircraft Serial Number applicability: LJ-2101, LJ-2106, LJ-2112, LJ-2113, LJ-2115 thru LJ-2117, LJ-2119 and After (8) 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. 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 Beechcraft C90GTi is as follows: a. The type certification basis for the Beechcraft C90GTi is shown on TCDS 3A20 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 24, 2014, is based upon part 23 as amended by Amendment 23-62. 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 this modification was determined to be: CAR Amend. CAR Amend. CAR Amend. 3.171 (a)(b) 3-0 3.292 3-0 3.307 3-0 3.172 3-0 3.293 3-0 3.386 (d) 3-0 3.173 3-0 3.294 3-0 3.665 3-0 3.174 3-0 3.295 3-0 3.688 3-0 3.197 (a)(b)(c) 3-2 3.296 3-0 3.689 3-0 3.270 (a) 3-2 3.306 3-0 FAA Form 8110-2 (5/14) Page 4 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01792WI October 5, 2016 Certification Basis (Continued): 14 CFR Part Amend. 14 CFR Part Amend. 23.251 (b) 62 23.1327 (a)(1)(2)(b) 20 23.601 Orig. 23.1329 (c)(h) 49 23.613 45 23.1331 (b)(c) 43 23.773 (a)(1)(2) 45 23.1335 20 23.777 (a)(b) 51 23.1351 (a)(1)(2)(i) 49 23.853 (a) 34 23.1353 (h) 49 23.867 (a)(b)(1) 7 23.1357 (a)(b)(c)(d) 43 23.901 (a)(1)(2)(e)(1) 53 23.1359 (c) 49 23.903 (b)(2) 62 23.1365 (a)(b)(c)(d)(e) 49 23.937 (a) 7 23.1367 (a)(b)(c)(d) Orig. 23.1141 (g)(2) 51 23.1381 (a)(b) Orig. 23.1203 (a)(d) 51 23.1431 (a)(b)(c)(e) 49 23.1301 (a)(b)(c)(d) 20 23.1501 (b) 21 23.1303 (a)(b)(c)(e) (f) 49 23.1521 (a)(b)(1)(3)(4)(c)(1)(3) 50 23.1305 (a)(2)(3) (c)(1)(2)(3)(5)(6)(7)(e)(1) 52 23.1525 45 23.1529 26 23.1306 (a)(b) 61 23.1543 (b)(c) 50 23.1308 (a)(b)(c)(d) 57 23.1545 (d) 50 23.1309 (a)(1)(3)(b) (c)(1)(2)(i)(iii)(3)(d)(e) 49 23.1547 (a)(b)(c)(d)(e) 20 23.1549 (a)(b)(c)(d) 45 23.1311 (a)(b)(c) 49 23.1555 (a) 50 23.1321 (a)(b)(c)(d)(e) 49 23.1581 (a)(2)(b)(1)(3)(c)(d)(f) 50 23.1322 (a)(b)(c)(d)(e) 43 23.1583 (b)(h)(m) 50 23.1323 (a)(c) 49 23.1585 (a)(j) 50 -------------------------------------------------------------------- END -------------------------------------------------------------------- ## Every issue (4) - October 5, 2016: Amended, Current. [certificate](https://openairdocs.org/files/sha256/79/1c/791ca83dffdc71a5ed254ab93b8d7a6caba3bbf519469c46c092ac7eabca043d) - May 19, 2016: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f3/7f/f37f1434665fd011cb537b2e559a6242bbab70d130a976e3c150b5972c88ec49) - February 24, 2016: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/39/85/3985ced7359e2151ec85e20a4119dc974cd296abca1b3fb26d116563b33886dd) - August 31, 2015: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/7b/37/7b370759c802a14af3f79c62b58706bc6429a4c4a04fddbb091d4be7863afff8) --- 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.