# STC SA03001CE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Embraer Engineering & Technology Center - USA Inc., United States - Description: Installation of Honeywell High Frequency (HF) Communication System, model KHF1050HF, and AvTec Selective Calling (SELCAL), model CSD-714 - Applied: February 20, 2014 - Status date: May 13, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A60CE](https://openairdocs.org/tcds/A60CE) - Certificate PDF: https://openairdocs.org/files/sha256/11/d0/11d0609ad914400c89be8498fd2604ec65c33fb34ea4e60e31cf02efcba7239b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F796496F7556116D862585CB003B2242.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA03001CE ## ADs that name it (0) None. ## Approved models (1) - Embraer S.A. EMB-505 ([TCDS A60CE](https://openairdocs.org/tcds/A60CE)) ## 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 This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21 .47. The STC’s supporting documentation (drawings, i nstructions, specifications, flight manual supplements, etc.) is the property of the ST C holder. FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA03001CE This certificate issued to: Embraer Engineering & Technology Center, USA, Inc. 1400 General Aviation Drive Melbourne, FL 32935 Part 23 of the Federal Aviation Regulations. Original Product – Type Certificate Number: A60CE Make: Embraer S.A. Model: EMB-505 Installation of Honeywell High Frequency (HF) Communication System, model KHF1050HF, and AvTec Selective Calling (SELCAL), model CSD-714, in accordance with Master Document List Number ESCCCD029, Revision E, dated June 06, 2018, or later FAA approved revision. STC was originally issued as a validation of Brazilian CST (STC) No. 2012S03-03 (07/07/2014). STC transferred to United States based Design Approval Holder (DAH) on May 07, 2019. 1. 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. 2. 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. Continued on Page 3 Date of Application: 02/20/2014 Date Reissued: 05/13/2019 Date of Issuance: 07/07/2014 Date Amended: By Direction of the Administrator Signature Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number: SA03001CE To (Name and address of transferee) From (Name and address of grantor) The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. FAA Form 8110-2 (5/14) Page 3 of 3 STC No. SA03001CE Limitations and Conditions: (Continued from Page 1) 3. Required Markings and Placards must be installed in accordance with Master Drawing List Document Number ESCCCD030, Revision B, dated March 22, 2018, or later FAA approved revision. 4. This installation (HF and SELCAL System) is only applicable to the Embraer Model EMB-505 aircraft model equipped with structural and electrical provisions approved under the original Type Certificate. 5. Instructions for Continued Airworthiness (ICA), Document Number ESCMTD015, Revision C, dated March 22, 2018, or later FAA accepted revision is required for this installation. 6. A copy of this Certificate shall be maintained as part of the permanent records of the modified aircraft. 7. Prior ANAC and/or FAA accepted or approved versions of the aforementioned documents can be used to sustain existing installations. ## Every issue (2) - May 13, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/11/d0/11d0609ad914400c89be8498fd2604ec65c33fb34ea4e60e31cf02efcba7239b) - July 7, 2014: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/a0/6c/a06ce9abb573310771e58a403d7a4e95fe384c7b214d5c1cd6d41ddac175d530) --- 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.