# STC SA130GL

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: North Central Airlines, Inc, United States
- Description: Installation of Systron-Donner Model 8160-20-P10 angular rate sensor in lieu of presently installed rate gyros in pitch- axis computer, roll-axis computer, and stability augmentation computers.
- Status date: July 23, 1976
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5BBE55148729B16085256CC100820E9F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA130GL

## ADs that name it (0)

None.

## Approved models (1)

- McDonnell Douglas Corporation DC-9-30 Series ([TCDS A6WE](https://openairdocs.org/tcds/A6WE))

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