STC SA03956NY

Supplemental type certificate · MAG Aerospace

Holder
MAG Aerospace · United States
Status
Current · Amended
Status date
February 1, 2022
Applied
April 12, 2017
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 23, Part 23
Data sheet
TCDSA37CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a Becker Digital Audio Management System

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

(for) Christina M. Underwood Manager, Alanta ACO Branch Title: Compliance and Airworthiness Division Aircraft Certification Service

FFAA Form 8110-2 (03/21) Page 1 of ___ SA03956NY MAG Aerospace 7065 Challenger Avenue Titusville, FL, 32780 23 the Federal Aviation Regulations A37CE Textron Aviation Inc.

208, 208B Installation of a Becker Digital Audio Management System in accordance with FAA Approved Aerospace Design & Compliance (1) Master Data List, C208-MDL-0003, Revision A, dated October 21, 2021, or later FAA approved revision. (2) Instructions for Continued Airworthiness (ICA) C208-ICA-0003, Revision C, dated September 06, 2017 or later FAA accepted revision. The ICA and its contents must be incorporated into the operator's maintenance program. (3) Airplane Flight Manual Supplement C208B-AFMS-0003, Revision IR, dated July 11, 2017 or later approved revision.

(See Continuation Sheet 3 of 4) April 12, 2017 October 22, 2017 September 20, 2017 February 1, 2022 4

1. Garmin G1000 Avionics Suite, software level v13.10 or higher is a prerequisites for this alteration, and must be installed either prior to, or in conjunction with this alteration.

2. STC SA01969SE (Installation of a Mid-Continent MD302 Standby Attitude Module) or STC SA04046CH (Installation of a L-3 ESI-500 Electronic Standby Instrument Systems) is a prerequisite for this alteration, and must be installed either prior to, or in conjunction with this alteration.

3. The installer must determine whether this design change is compatible with previously approved modifications.

4. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission.

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 the Textron, Model 208/208B series is as follows:

a. The type certification basis for the Textron, Model 208/208B airplane is shown on TCDS A37CE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, April 12, 2017, is based upon part 23 as amended by Amendment 23-28 with the exception of those above amendment 23-28, listed below.

Regulations at later amendment than 23-28.

14 CFR Part Amendment § 23.1359(c) 23-49 § 23.1431(a) (b) 23-43

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ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Textron Aviation Inc.208A37CE
Textron Aviation Inc.208BA37CE

Every issue · 3

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
February 1, 2022Amended, currentCertificate
February 1, 2022Amended, earlier issueCertificate
October 22, 2017Reissued, earlier issueCertificate