# STC SA164SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Riley Turbostream Corp
- Description: Installation of sNM-Lpt vertical tail, wing tips and elevator (STC SA303CE-A is prerequisite to this STC); in- stallation of Lycoming IO-720-A1A engines (STC SE163CE-A) and Hartzell HC-A3VK-2/V8433-4R propellers.
- Status date: August 6, 1974
- Data sheets: A-807, A-807, A-807, A-807
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0D55897B0F4DADC885256CC100821507.0001
- Page: https://openairdocs.org/stc/SA164SO

## ADs that name it

- [AD 70-15-18](https://openairdocs.org/ad/70-15-18): Automatic Pilot and Automatic Aileron Stabilizer Instruments · Mitchell Industries Auto Pilot Systems Instruments. Effective Aug 31, 1970

## Approved models (4)

- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 1A (TCDS A-807)
- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 2A (TCDS A-807)
- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 5A (TCDS A-807)
- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 6A (TCDS A-807)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.