# STC SA12131IB

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Diamond Aircraft Industries GmbH, Austria
- Description: Increase of Maximum Take-Off Weight to 5202 lbs (2360 kg)
- Applied: October 24, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Foreign approvals: EASA 10083990
- Data sheets: [TCDS A00012NY](https://openairdocs.org/tcds/A00012NY)
- Certificate PDF: https://openairdocs.org/files/sha256/e8/22/e822f7144f3ea160293b9d83f7df627b4286bdbc1424544b30578eaeaa8bb84f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136003736120250902201426.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA12131IB

## ADs that name it (0)

None.

## Approved models (1)

- Diamond Aircraft Industries Inc DA 62 ([TCDS A00012NY](https://openairdocs.org/tcds/A00012NY))

## 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 SA12131IB Diamond Aircraft Industries GmbH Nikolaus-August-Otto-Strasse 5 2700 Wiener Neustadt Austria Part 23 Title 14 Code of Federal Regulations A00012NY Diamond Aircraft Industries Inc.

DA 62

1. This STC is applicable to all serial numbers for these Diamond Aircraft Industries Inc. DA 62.

(See Continuation Sheet 3) 10/24/2024 08/27/2025 John Yoo Manager, International Validation Branch, AIR-730 Compliance & Airworthiness Division Aircraft Certification Service 3 Increase of Maximum Take-Off Weight to 5202 lbs (2360 kg) in accordance with Master Drawing List, STC 62-005, Rev. f, or later EASA approved revision. The Maximum Landing Weight and Maximum Zero Fuel Weight are not changed.

Operation in accordance with AFM Supplement STC-62-005, Rev. 0 to Doc. No. 7.01.25-E /

11.01.05-E and AFM Supplement STC-62-005-S03, Rev. 0 to Doc. No. 7.01.25-E / 11.01.05-E or later EASA approved revision.

Maintenance in accordance with AMM Supplement 7.02.25-STC 62-005, Rev. 0, dated September 24, 2024 or later EASA approved revision.

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

3. The aircraft must be operated in accordance with the limitations section of AFM Supplement STC-62-005 Rev. 0 to Doc. No. 7.01.25-E / 11.01.05-E and AFM Supplement STC-62-005-S03 Rev. 0 to Doc. No. 7.01.25-E / 11.01.05-E or later EASA approved revisions.

4. 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:

The Type Certification Basis for the original product remains applicable to this certificate.

This certificate involves a change with an impact on noise. The noise standards are amended as follows:

14 CFR part 36, as amended by Amendments 36-1 through 36-32.

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## Every issue (1)

- Undated: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e8/22/e822f7144f3ea160293b9d83f7df627b4286bdbc1424544b30578eaeaa8bb84f)

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