# STC SA02188AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: F Atlee Dodge Aircraft Service, United States
- Description: Fabrication and installation of p/n 3284 three-inch extended PA-18 type main landing gear, together with p/n 3164-4 extended shock strut assemblies. Applies to those models previously modified by SA148AL, SA543AL, or SA669AL, or for Piper PA-12S models, planes must have been converted to landplane configuration.
- Status date: January 11, 2002
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-780](https://openairdocs.org/tcds/A-780), [TCDS A-797](https://openairdocs.org/tcds/A-797)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9CE621D4A457D60085256CC1007F3951.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02188AK

## ADs that name it (0)

None.

## Approved models (4)

- The New Piper Aircraft Inc. PA-12 ([TCDS A-780](https://openairdocs.org/tcds/A-780))
- The New Piper Aircraft Inc. PA-12 Series ([TCDS A-780](https://openairdocs.org/tcds/A-780))
- The New Piper Aircraft Inc. PA-12S ([TCDS A-780](https://openairdocs.org/tcds/A-780))
- The New Piper Aircraft Inc. PA-14 ([TCDS A-797](https://openairdocs.org/tcds/A-797))

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