# STC SA00276NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Air Research Technology, Inc, Canada
- Description: Reinforcement of wing assemblies and installation of Air Research Technology wing tip extension.
- Status date: January 15, 1999
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7FF93BA34D22A30C85256CC1007DC87A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00276NY

## ADs that name it (1)

- [AD 98-16-04](https://openairdocs.org/ad/98-16-04): Inspect Angle Stiffener Along Lower Spar Cap · Cessna 180, 180A, 180B and 37 more. Effective Sep 21, 1998. Named in the applicability

## Approved models (3)

- The Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

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