# STC ST10353SC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Pyka Aerospace Corp - Description: Installation of a TCAS II with dual Mode S Transponder system. - Status date: May 24, 2005 - Data sheets: A16SW - Certificate PDF: https://openairdocs.org/files/sha256/95/2e/952eb22919861381615534e8b7f2712016cb46a9eac4c70bf1f42e00cbf9b202 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5FD54EA315E983F88625701F0065222E.0001 - Page: https://openairdocs.org/stc/ST10353SC ## ADs that name it None. ## Approved models (1) - Raytheon Aircraft Company 400 (TCDS A16SW) ## 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. United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project No. ST7876SC-T KC 11216 Disco San Antonio, TX 78216 Part 25 of the Federal Aviation Regulations. Original Product Type Certificate Number : A16SW Make : Raytheon Aircraft Company Model : 400 Description of Type Design Change: Installation of a TCAS II with dual Mode S Transponder system in accordance with Pyka MDL 1B05-DL-001-501 Rev. F dated November 17, 2004, or later FAA approved revision. Airplane Flight Manual Supplement 1B05-FM-001 Rev. IR dated November 05, 2004, or later FAA approved revision is required. Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer. 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. Date of application : June 10, 2004 Date of issuance : November 19, 2004 Date reissued : May 24, 2005 ( Signature) Fred Stellar Acting Manager, Special Certification Office Southwest Region (Title) FAA Form 8110-2-1(10-69) Page 2 of 2 Number ST10353SC Date of Issuance: May 24, 2005 Certification Basis: The certification basis for this installation is per Type Certificate Data Sheet A16SW, plus the following: Regulations that meet amendment 25-41 25.305(a) & (b), 25.1309(a),(b),(c), 25.1321(a), 25.1331(a)(3) Regulations that meet amendment 25-42 25.1501(b) Regulations that meet amendment 25-46 25.603(a)& (b), 25.605(a) Regulations that meet amendment 25-54 25.1529 Regulations that meet amendment 25-72 25.307(a), 25.625(a)(1)&(2), 1307(c), 1351(a), 25.1381(a),(b), 25.1581(a),(b)&(d) Regulations that meet amendment 25-86 25.305(a) & (b), 25.321(a) Regulations that meet amendment 25-87 25.365(a) & (d), Regulations that meet amendment 25-91 25.561(b)(3), 25.561(c) Regulations that meet amendment 25-112 25.613(a) & (b) Regulations that meet amendment 25-113 25.1353(a), 25.1431(a),(c) ## Every issue (1) - May 24, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/95/2e/952eb22919861381615534e8b7f2712016cb46a9eac4c70bf1f42e00cbf9b202) --- 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.