# STC SA12416IB

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: BERINGER AERO, France
- Description: Installation of Main wheel, Nose wheel, brake assembly, axle, master cylinder and brake lines
- Applied: August 18, 2025
- Status date: June 23, 2026
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/f7/bf/f7bff192dd828569b5a950958b608005ef4ce03dc8de370291029fd149b32574
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166918869120260716160808.0001
- DRS record last changed: July 16, 2026
- Page: https://openairdocs.org/stc/SA12416IB

## ADs that name it (0)

None.

## Approved models (11)

- Textron Aviation Inc. 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. G36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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.

**IMPORT SA12416IB**

**BERINGER AERO**

AEROPOLE 05130 TALLARD, FRANCE Part 23 Code of Federal Regulations.

3A15 Textron Aviation Inc.

F33, F33A, F33C, G33, G36, V35A, V35B, 36, A36, A36TC, B36TC

1) Installation of Main wheel, Nose wheel, brake assembly, axle, master cylinder and brake lines in accordance with Master Data List document MDL-STC-025, Revision 01, dated July 10 or later EASA approved revisions.

(See Description of Type Design Change continued on Page 3 of 3)

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

(See Limitations and Conditions continued on Page 3 of 3) August 18, 2025 June 23, 2026 for John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

**IMPORT SA12416IB 3**

IMPORT SA12416IB Description of Type Design Change: (continued from page 1 of 3)

2) Maintenance is in accordance with Instructions for Continued Airworthiness document, ICA-STC-025, Revision 02, dated July 01, 2025 or later EASA accepted revisions.

Limitation and Conditions: (continued from page 1 of 3)

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

3) This STC is applicable to all serial numbers of models F33, F33A, F33C, G33, G36, V35A, V35B, 36, A36, A36TC and B36TC.

-----END----- 3 3

## Every issue (1)

- June 23, 2026: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f7/bf/f7bff192dd828569b5a950958b608005ef4ce03dc8de370291029fd149b32574)

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