# STC SA12425IB

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: AEROSPACE COMPOSITES GmbH, Germany
- Description: Installation of Single Hatch
- Applied: February 11, 2026
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A00007SE](https://openairdocs.org/tcds/A00007SE)
- Certificate PDF: https://openairdocs.org/files/sha256/b0/4d/b04d1ffbac135e1a7bbf6b48210d1af3c20a4be69a391973131d501b57860162
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147569141920260707173838.0001
- DRS record last changed: July 7, 2026
- Page: https://openairdocs.org/stc/SA12425IB

## ADs that name it (0)

None.

## Approved models (1)

- Daher Aircraft Design LLC Kodiak 100 ([TCDS A00007SE](https://openairdocs.org/tcds/A00007SE))

## 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 SA12425IB AEROSPACE COMPOSITES GmbH BERBLINGERSTR. 18 88471 LAUPHEIM

GERMANY Part 23 Title 14 Code of Federal Regulations A00007SE Daher Aircraft Design, LLC Kodiak 100

1. This STC is applicable to serial numbers up to and including 100-0274 for the applicable make and model.

(See Limitations and Conditions Continued on Page 3 of 3) 02/11/2026 07/01/2026 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

1. Installation of Single Hatch in accordance with Aerospace Composites Engineering Order EO-KOD100-9506-01, Rev.: --, dated August 30, 2023 or later EASA approved revisions.

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

2. Maintenance in accordance with Aerospace Composites Maintenance Manual Supplement MMS-KOD100-9506-01, Issue 0-0, dated September 18, 2023, or later EASA accepted revision.

3. Operation in accordance with Aerospace Composites Aircraft Flight Manual Supplement AFMS-KOD100-9506-01, Issue 0-0, dated September 22, 2023, or later EASA approved revision.

2. Maintenance must be in accordance with the "Airworthiness Limitation" Section of the Maintenance Manual Supplement listed in the Description of Type Design section of this STC.

3. Operation must be in accordance with the Limitation Section of the Flight Manual Supplement listed in the Description of Type Design section of this STC.

4. This STC is not compatible with the optional External Cargo Compartment (ECC).

5. This STC is not compatible with the optional TKS Ice Protection System.

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

7. 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.

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## Every issue (1)

- Undated: Issued, Current. [certificate](https://openairdocs.org/files/sha256/b0/4d/b04d1ffbac135e1a7bbf6b48210d1af3c20a4be69a391973131d501b57860162)

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From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.