# STC SA2823SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Phillips Harry L, United States
- Description: Reinforcement of vertical tail spar.
- Applied: October 19, 1977
- Status date: July 31, 1978
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3)
- Certificate PDF: https://openairdocs.org/files/sha256/7c/bc/7cbcca42b48f447bbfc8f5383ab94e504e3d64798f71d19415280932dec9ab79
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0B139E024A300CCB85256CC20008C9A5.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2823SW

## ADs that name it (0)

None.

## Approved models (2)

- Mooney International Corporation M20 ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney International Corporation M20A ([TCDS 2A3](https://openairdocs.org/tcds/2A3))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

mnittd grates Df;

BEpartmtnt of ^transportation-federal SUriation administration supplemental HTpe Certificate SA2823SW

•^/Stt&f&rtt&Gate; 4dA46&e&A Harry L. Phillipa Route 3, Box 420F Fort Worth, Texas 76140 A3899SW-S RTW-212 v^fo^ufa*ieAj;ffMj^w^fo^i>ttw'iewfiwr£^w CiVll ALF iSleiaida&&ttA/.

2A3 Moemey M20. M20A Reinforcement of Vertical Tall Spar according to Drawing Nwnbar 12-77-oi, RevUion 1 datad April 3, 1978, or later FAA approved revision.

Compatibility of this modification with other previously approved modification* mitt be determined by the installer.

Jfar"??te>n4i&4tw October 19, 1977 July 31, 1978 (Signature) Don P. Wation Chief, Engineering and Manufacturing Branch (Title)

FAAFon-anO-2(10-68)

## Every issue (1)

- July 31, 1978: Issued, Current. [certificate](https://openairdocs.org/files/sha256/7c/bc/7cbcca42b48f447bbfc8f5383ab94e504e3d64798f71d19415280932dec9ab79)

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