# STC SA12420IB

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: AEROSPACE COMPOSITES GmbH, Germany
- Description: Battery Installation
- Applied: July 2, 2026
- Status date: July 2, 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/dd/86/dd86d62e3c6fb2476504412ffc623f9c3e688c5007414c67143d2f149b4a661c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169032780220260707173342.0001
- DRS record last changed: July 7, 2026
- Page: https://openairdocs.org/stc/SA12420IB

## 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 SA12420IB 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 all serial numbers for the applicable models.

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

1. Battery Installation in accordance with Aerospace Composites Project Document List PDL-KOD100-2430-01, Rev.: --, dated October 16, 2020 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-KOD100-2430-01, Issue 0-0, dated October 16, 2020, or later EASA accepted revision.

3. Operation in accordance with Aerospace Composites Aircraft Flight Manual Supplement AFMS-KOD100-2430-01, Issue 0-0, dated October 9, 2020, 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. The installer must determine whether this design change is compatible with previously approved modifications.

5. 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)

- July 2, 2026: Issued, Current. [certificate](https://openairdocs.org/files/sha256/dd/86/dd86d62e3c6fb2476504412ffc623f9c3e688c5007414c67143d2f149b4a661c)

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