STC SA00209IB

Supplemental type certificate · AVIONIK STRAUBING ENTWICKLUNGS GmbH

Holder
AVIONIK STRAUBING ENTWICKLUNGS GmbH · Germany
Status
Current · Issued
Status date
July 12, 2024
Applied
October 25, 2023
Product
Aircraft · Small Airplane
Certification basis
Part 23
Data sheet
TCDSA1WI
Foreign approvals
EASA 10042753

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

What it approves

Installation of Single Garmin GTN 725(Xi)/GTN 750 (Xi) Unit and optional Garmin Flight Stream FS 510

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.

IMPORT SA00209IB AVIONIK STRAUBING ENTWICKLUNGS GmbH 94348 ATTING

GERMANY Part 23 Title 14 Code of Federal Regulations A1WI Textron Aviation Inc.

525, 525A, 525B Installation of Single Garmin GTN 725(Xi)/GTN 750 (Xi) Unit and optional Garmin Flight Stream FS 510 in accordance with Master Documents List ASR-2022-037-MDL-01-01, dated April 9, 2024, or later EASA approved revision.

Maintained in accordance with Instructions for Continued Airworthiness ASR-2022-037-ICA-11-01, dated April 9, 2024 or later EASA approved revision.

1. This STC is not permitted for use on aircraft modified with EASA STC 10042753.

2. This STC is applicable to all serial numbers for these Textron Aviation Inc. Model 525, 525A and 525B.

(See Continuation Sheet 3) October 25, 2023 July 12, 2024 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

IMPORT SA00209IB 3

IMPORT SA00209IB Date Issued: July 10, 2024

Description of Type Design Change (continued):

Operated in accordance with Flight Manual Supplement ASR-2022-037-FMS-05.1-00 dated June 12, 2023 (for aircraft with the SPZ-5000) or ASR-2022-037-FMS-05.2-00 dated June 12, 2023 (for aircraft with the ProLine 21) or later EASA accepted revisions.

3. The aircraft must be operated in accordance with the limitations section of the flight manual supplement referenced in the Description section.

4. The aircraft must be maintained in accordance with the airworthiness limitations section of the ICA referenced in the Description section.

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

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

Certification Basis:

14 CFR Part 23 as amended by Amendments 23-1 through 23-62

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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 · 3

MakeModelData sheet
Textron Aviation Inc.525A1WI
Textron Aviation Inc.525AA1WI
Textron Aviation Inc.525BA1WI