# STC ST09649DS - Type: Supplemental type certificate - Status: Current, Issued - Holder: Flight Program Operations - Description: Installation of ADS-B 1090ES OUT Transponder System - Status date: February 13, 2019 - Data sheets: A21EA - Certificate PDF: https://openairdocs.org/files/sha256/50/e3/50e3a157b932b1ca2d0a0091373e712b64362bea6e47f60158f9811644dbf7ac - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E334D098224F6282862585C900544AFB.0001 - Page: https://openairdocs.org/stc/ST09649DS ## ADs that name it None. ## Approved models (1) - Bombardier Inc. CL-600-2B16 (CL-601-3R) (TCDS A21EA) ## 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. Un i t ed S t a t e s o f A m er i ca Department of Transportatio n Federal Aviation Administration Supplemental Type Certificate Number : ST09649DS FAA Form 8110-2 (5/14) Page 1 of 3 This certificate, issued to: Flight Program Operations 6500 S. MacArthur Boulevard Oklahoma City, OK 73169 Part 25 of the Federal Aviation Regulations. A21EA Make: Bombardier Inc. Model: CL-600-2B16 (CL-601-3R) Installation of ADS-B 1090ES OUT Transponder System in the Air Traffic Control (ATC) Transponder No. 1 position with a previously installed Mode A/C/S non ADS-B OUT capable ATC Transponder in the No. 2 position. This alteration is to be made in accordance with data list D09649, dated February 13, 2019, or later approved FAA revision. E-Systems STC ST00226WI-D, “Installation of a Pro Line 4 Avionics System and partial Flight Inspection Avionics Equipment and Provisions,” date reissued March 21, 2003 must be accomplished prior to this STC. Aviation System Standards STC ST09475AC-D, “Installation of UNS-1F Flight Management System (FMS),” date of issuance February 28, 2003 must be accomplished prior to this STC. Date of Application: February 2, 2018 Date Reissued: Date of Issuance: February 13, 2019 Date Amended: Signature TitleODA Administrator-Alternate, ODA-700576-SW Un i t ed S t a t e s o f A m er i ca Department of Transportation Federal Aviation Administration Supplemental Type Certificate ..ST09649AC FAA Form 8110-2 (5/14) Page 2 of 3 To (Name and address of transferee) From (Name and address of grantor) Un i t ed S t a t e s o f A m er i ca Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number : ST09649AC FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change (Continued): Aviation System Standards STC ST09091AC-D, “Installation of Identification Friend or Foe (IFF) System,” date amended September 30, 2004 must be accomplished prior to this STC. ATC #2 Transponder may only be selected for Flight Inspections. Only one transponder may be active at any time. Compatibility of the alteration with other approved alterations is to be determined by the installer. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft. 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. FAA approved airplane flight manual supplement, “ADS-B 1090ES OUT Transponder System,” dated February 11, 2019, or later approved FAA revision, is required. Instructions for continued airworthiness, “Installation of the ADS-B 1090ES Transponder System,” M09649, dated December 11, 2018, or later accepted FAA (AEG) revision, is a required part of this modification. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. 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 of the Bombardier Model CL-600-2B16 (Cl-601-3R) series installation of ADS-B 1090ES OUT transponder system is as follows: a. The type certification basis for the Bombardier Model CL-600-2B16 (Cl-601-3R) series airplane is shown on TCDS A21EA for parts not changed or affected by the modification. b. The certification basis for parts changed or affected by the modification since the reference date of application, February 2, 2018, is based upon the TCDS A21EA. 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: Regulations at the amendment level 25-0 through 25-46 25.23, 25.301(a), 25.303, 25.305(a), 25.307(a), 25.561(c), 25.603; 25.605(a), 25.609, 25.613, 25.789(a), 25.1301, 25.1307(c), 25.1309(a)(b)(c)(d)(g), 25.1322, 25.1351(a), 25.1353(a)(b), 25.1357(a)(c)(d)(e), 25.1431(a)(c), 25.1529, 25.1541, 25.1555(a), 25.1581, 25.1583, 25.1585 ----------------------------------------------------------- END ------------------------------------------------------------- ## Every issue (1) - February 13, 2019: Issued, Current. [certificate](https://openairdocs.org/files/sha256/50/e3/50e3a157b932b1ca2d0a0091373e712b64362bea6e47f60158f9811644dbf7ac) --- 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.