STC SA2823SW

Supplemental type certificate · Phillips Harry L

Holder
Phillips Harry L · United States
Status
Current · Issued
Status date
July 31, 1978
Applied
October 19, 1977
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS2A3

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Reinforcement of vertical tail spar.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Mooney International CorporationM202A3
Mooney International CorporationM20A2A3