# STC SA2487CE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Arthur J and Helen Curtiss, United States
- Description: Installation of rudder, aileron, flap, and stabilator trim tab gap seals
- Applied: December 1, 1988
- Status date: April 20, 1989
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15)
- Certificate PDF: https://openairdocs.org/files/sha256/c9/69/c9694d0ff4bf3d0be2c9a4d8e9d07a72decfb2645142a10fcec2b8c7d55bf938
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/106104B9A9AD5605862580880063BD8B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2487CE

## ADs that name it (0)

None.

## Approved models (1)

- Piper Aircraft Inc. PA-24-250 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))

## What the certificate says

The certificate is a scan without a text layer; open the PDF to read it.

## Every issue (1)

- April 20, 1989: Issued, Current. [certificate](https://openairdocs.org/files/sha256/c9/69/c9694d0ff4bf3d0be2c9a4d8e9d07a72decfb2645142a10fcec2b8c7d55bf938)

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