# STC SA03010CE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Embraer Engineering & Technology Center - USA Inc., United States - Description: Installation of a Lacobucci HF Electronics Nespresso Machine PIN HFE96-28T-10 and/or Monogram System -TIA Division Wavejet Microwave Oven PIN 400-1860-01 - Applied: October 1, 2018 - Status date: October 2, 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/f3/99/f399e90b6304481920fdde8780e498447c72f7d91cc9f22e05bb7da3f83cd96e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CC7434D2A4003A74862585D10052EB33.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA03010CE ## 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 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 1 of 3 Number: SA03010CE 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 Description of Type Design Change: Installation of an Iacobucci HF Electronics Nespresso Machine P/N HFE96-28T-10 and/or Monogram System - TIA Division Wavejet Microwave Oven P/N 400-1860-01, in accordance with Master Document List number ESCCCD012, Revision I, dated April l, 2019, or later FAA approved revision. This STC was originally issued as a validation of Brazilian CST (STC) No. 2012S06-07 (April 19, 2019), and transferred to a United States based Design Approval Holder (DAH) on October 02, 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: 10/01/2018 Date Reissued: 10/02/2019 Date of Issuance: 04/19/2019 Date Amended: By Direction of the Administrator Signature Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not const itute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. 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: SA03010CE To (Name and address of transferee) From (Name and address of grantor) Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not const itute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. 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 Number: SA03010CE Limitations and Conditions: (Continued from Page 1) 3. Required markings and placards must be installed in accordance with Master Drawi ng List document number ESCCCD013, Revision E, dated June 5, 2012, or later FAA approved revision. 4. Instruction for Continued Airworthiness (ICA), document number ESCMTD007, Revision B, dated April 1, 2019, or later FAA accepted revision is required for this installation. 5. A copy of this Certificate shall be maintained as part of the permanent records of the modi fied aircraft. 6. Prior ANAC and/or FAA accepted or approved versions of the aforementioned documents can be used to sustain existing installations. ## Every issue (2) - October 2, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f3/99/f399e90b6304481920fdde8780e498447c72f7d91cc9f22e05bb7da3f83cd96e) - April 19, 2019: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/ec/bc/ecbc4e9019a1f87c364cb8ef43b3cc14f609d6d228ae5d25a1e3a06680cf981b) --- 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.