# STC SA2438WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Consulting Aerospace Engineers Inc, United States
- Description: Installation of spar reinforcing steel straps, on aircraft previously modified per STC SA1747WE.
- Status date: May 23, 1973
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-807](https://openairdocs.org/tcds/A-807)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7497FB1A7202283F85256CC200015E1F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2438WE

## ADs that name it (2)

- [AD 70-23-02](https://openairdocs.org/ad/70-23-02): Wing Lower Main Spar Cap · Two AiResearch TPE331 series engines and increase in fuselage… (Cal Aero Industries STC SA1554WE or SA1747WE). Effective Jul 3, 1973. Cited in the text
- [AD 72-10-03](https://openairdocs.org/ad/72-10-03): Fatigue Failure Wing Spar Fitting · AiResearch TPE 331 engines, increase in fuselage length (Texas Airplane Mfg STC SA1747WE). Effective Jun 7, 1972. Cited in the text

## Approved models (4)

- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 7A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 7AXC ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 8A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd (England) DH 104 Dove Series 8AXC ([TCDS A-807](https://openairdocs.org/tcds/A-807))

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