# STC SA2913SO

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Gulfstream Aerospace Corporation, United States
- Description: Modification of the tailcone to install a fiberglass section.
- Applied: March 6, 1990
- Status date: January 25, 1991
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA)
- Certificate PDF: https://openairdocs.org/files/sha256/6d/81/6d810485e834e711c0ff9bea9375b446f162ce8e9ac76e99e86d6ca8726906bf
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174111465620231130182758.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2913SO

## ADs that name it (0)

None.

## Approved models (2)

- Gulfstream Aerospace Corporation G-1159A ([TCDS A12EA](https://openairdocs.org/tcds/A12EA))
- Gulfstream Aerospace Corporation G-IV ([TCDS A12EA](https://openairdocs.org/tcds/A12EA))

## What the certificate says

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

## Every issue (1)

- January 25, 1991: Issued, Current. [certificate](https://openairdocs.org/files/sha256/6d/81/6d810485e834e711c0ff9bea9375b446f162ce8e9ac76e99e86d6ca8726906bf)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
