# STC SA03006CE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Embraer Engineering & Technology Center - USA Inc., United States - Description: Installation of a Medical Evacuation Configuration (Medevac) - Applied: July 5, 2016 - 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/sha256/22/17/22174b0f3babbdd7c2e74ceb3967a9fc4840658e7ebabbdd721a5528d3ad6621 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/ECC33F695DF871C9862585CB003B2314.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA03006CE ## 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 c ertificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possessio n of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, s pecifications, flight manual supplements, etc.) is the property of the ST C holder. FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA03006CE 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 a Medical Evacuation Configuration (Medevac) in model EMB -505 airplanes, in accordance with Master Document List Number ESCCCD009, Revision H, dated May 05, 2017, or later FAA approved revision. STC was originally issued as a validation of Brazilian CST (STC) No. 2012S02-15. (11/02/2016). 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: 07/05/2016 Date Reissued: 05/13/2019 Date of Issuance: 11/02/2016 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 the property o f the STC holder. FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number: SA03006CE 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 the property o f the STC holder. FAA Form 8110-2 (5/14) Page 3 of 3 STC No. SA03006CE Limitations and Conditions: (Continued from Page 1) 3. Operation must be performed in accordance with ANAC approved Airplane Flight Manual Supplement (AFMS), document number H.02-3692-0/ANAC/2012, Revision IR, dated February 28, 2012, or later FAA approved revision. 4. Instructions for Continued Airworthiness (ICA), document number ESCMTD008, Revision D, dated May 05, 2017, or later FAA accepted revision is required for this installation. 5. Required Markings and Placards must be installed in accordance with Master Drawing List, document number ESCCCD014, Revision D, dated February 09, 2012, or later FAA approved revision. 6. Electromagnetic compatibility (EMC) ground testing must be performed in accordance with Ground Test Proposal, report number ESCMSP003, Revision IR or later FAA approved revision. 7. Qualification of carry-on medical devices used for sustaining patients in-flight, including incubators, not listed in the Installation Manual, document number ESCMSD006, Revision E, dated May 05, 2017, or later FAA approved revisions, will require separate approval. 8. A copy of this Certificate and the Supplement referred to in item 3 above shall be maintained as part of the permanent records of the modified aircraft. 9. 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/sha256/22/17/22174b0f3babbdd7c2e74ceb3967a9fc4840658e7ebabbdd721a5528d3ad6621) - November 2, 2016: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/12/90/1290325e2f216430cc40fbc612f117d11a62a3f45ccb851b8e9808febfa30039) --- 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.