# STC SA2008CE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: University of Kansas, United States
- Description: Tail stinger magnetometer installation.
- Status date: August 9, 1984
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1A275D554BB7675185256CC10083D523.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2008CE

## ADs that name it (0)

None.

## Approved models (1)

- de Havilland Inc. (Canada) DHC-2 (L-20A) MK.I ([TCDS A-806](https://openairdocs.org/tcds/A-806))

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