# STC SA746NW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: C & P Aircraft, United States
- Description: Installation of steel reinforcement angles on nose gear attach casting
- Applied: March 6, 1979
- Status date: April 6, 1979
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19)
- Certificate PDF: https://openairdocs.org/files/sha256/f6/0f/f60fb7489043345276ab080e2a9af15aa02ee26801ec047f5c25e67dd73b0393
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C00BB5ADDA5938FF86257A44006B94CB.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA746NW

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company 150A ([TCDS 3A19](https://openairdocs.org/tcds/3A19))

## What the certificate says

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

## Every issue (1)

- April 6, 1979: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f6/0f/f60fb7489043345276ab080e2a9af15aa02ee26801ec047f5c25e67dd73b0393)

---
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.
