# STC SA00732SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Empire Airlines Inc, United States
- Description: Installation of tail stand support fitting.
- Applied: August 10, 1999
- Status date: September 7, 1999
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE)
- Certificate PDF: https://openairdocs.org/files/sha256/95/8a/958a258695464e95a3c9857003130c763b010e22198b3601003528482e80ce0e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C379E57C1CBD605B85256CC1007E00FD.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00732SE

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- Cessna Aircraft Company 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))

## What the certificate says

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

## Every issue (1)

- September 7, 1999: Issued, Current. [certificate](https://openairdocs.org/files/sha256/95/8a/958a258695464e95a3c9857003130c763b010e22198b3601003528482e80ce0e)

---
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.