# STC SA1311CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Engineering Plating & Processing, Inc., United States
- Description: Chrome plated brake disc installation.
- Status date: June 20, 1977
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/51F682B1CFA2015585256CC100820EAA.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1311CE

## ADs that name it (0)

None.

## Approved models (6)

- The Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172H (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12))

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