# STC SA03008CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Embraer Engineering & Technology Center - USA Inc., United States
- Description: Installation of a Honeywell HF Communication System
- Applied: October 10, 2018
- Status date: July 17, 2019
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A59CE](https://openairdocs.org/tcds/A59CE)
- Certificate PDF: https://openairdocs.org/files/sha256/e2/85/e285f205899cf74f07860256ab5e12e268d68bae0df7b922635a312404c6b819
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8BE419F81816722B862585D0004B6A4C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA03008CE

## ADs that name it (0)

None.

## Approved models (1)

- Embraer S.A. EMB-500 ([TCDS A59CE](https://openairdocs.org/tcds/A59CE))

## 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.

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SA03008CE

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: A59CE Make: Embraer S.A.

Model: EMB-500

Installation of a Honeywell HF Communication System, model KHF 1050, and optionally the Avtech Corporation SELCAL decoder, model CSD-714 in accordance with Master Document List Number TR0116, Revision J, dated November 7, 2018 or later FAA approved revision. This STC was originally issued as a validation of Brazilian CST (STC) No. 2009S05-14 (May 29, 2009), and transferred to a United States based Design Approval Holder (DAH) on July 17, 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: 10/10/2018 Date Reissued: 07/17/2019 Date of Issuance: 12/11/2018 Date Amended:

By Direction of the Administrator Signature

Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch

FAA Form 8110-2 (5/14) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number: SA03008CE

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

STC Number: SA03008CE

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.02-2921-0/ANAC/2009, Revision I.R., dated May 29, 2009 or later FAA approved revision.

4. Instructions for Continued Airworthiness (ICA), Document Number ICA-006, Revision B, dated November 6, 2018 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 TR0118, Revision E, dated July 24, 2009 or later FAA approved revision.

6. 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.

7. Prior ANAC and/or FAA accepted or approved versions of the aforementioned documents can be used to sustain existing installations.

## Every issue (2)

- July 17, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e2/85/e285f205899cf74f07860256ab5e12e268d68bae0df7b922635a312404c6b819)
- December 11, 2018: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/e1/c8/e1c81e1028057978f4f7bb74ac3931dce406dc7cb85add0a3ee6d6e8ff4333be)

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