# STC SA1160SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: C J Aviation, United States
- Description: Installation of Weldon, P/N 6005-2A, aircraft engine driven fuel pump in lieu of diaphram type pump.
- Status date: October 21, 2002
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A23](https://openairdocs.org/tcds/3A23)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/82FB77F6C6DE3F2A85256CC10080DF1D.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1160SO

## ADs that name it (0)

None.

## Approved models (2)

- Maule Aerospace Technology Inc. Bee Dee M-4-220C ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. Bee Dee M-5-220C ([TCDS 3A23](https://openairdocs.org/tcds/3A23))

---
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.
