# STC SA12195SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Absolute Solutions LLC, United States
- Description: Installation of Absolute Solutions LLC Gear Warning System Upgrade
- Applied: November 7, 2023
- Status date: December 4, 2025
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/3d/77/3d77c8ec548b25d78acf4e8da36353e99ff8ce89d2904007437a07e7f48312db
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156269179520260106160959.0001
- DRS record last changed: January 6, 2026
- Page: https://openairdocs.org/stc/SA12195SE

## ADs that name it (0)

None.

## Approved models (1)

- Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## 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.

SA12195SE Absolute Solutions LLC 13565 S Carus Road Oregon City, OR 97045 Part 23 Title 14 CFR 2A13 Piper Aircraft, Inc.

PA-28R-200 This STC is applicable to serial numbers 28R-7235193 and up.

This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change (Continued on page 3.)

11/07/2023 12/04/2025 for Manager, West Certification Branch 3 Installation of Absolute Solutions LLC Gear Warning System Upgrade in accordance with the Master Drawing List (MDL) No. GWUPA-28-MDL-000, Rev. IR, dated July 2, 2024, and Installation Manual (IM) No. GWUPA-28-IM-000, Rev. IR, dated July 2, 2024, or later Federal Aviation Administration (FAA) approved revisions. (Continued on page 3.)

SA12195SE 3

SA12195SE Description of Type Design Change: (Continued from page 1.)

Maintained in accordance with the Instructions for Continued Airworthiness (ICA) No.

GWUPA-28-ICA-000, Rev. IR, dated July 2, 2024, or later FAA-accepted revision. Operated in accordance with the AFMS, No. GWUPA-28-AFMS-000, Rev. IR, dated October 3,02025 or later FAA-approved revision.

Limitations and Conditions: (Continued from page 1.)

and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, ICA, Installation Manual, and AFMS, must be maintained as part of the permanent records of the modified aircraft.

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

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## Every issue (1)

- December 4, 2025: Issued, Current. [certificate](https://openairdocs.org/files/sha256/3d/77/3d77c8ec548b25d78acf4e8da36353e99ff8ce89d2904007437a07e7f48312db)

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