STC SA4418SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
February 10, 1982
Applied
May 20, 1981
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 5, 2025.

What it approves

Installation of S-TEC system 60 pitch stabilization system, model ST-050 with optional autotrim system

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.

United States of America Bepartment of transportation—Jfetoal atriation administration Supplemental t^pe Certificate tSUvrnvev SA4418SW S-TEC Corporation Rt. 4, Bldg. 946 Welters Industrial Complex Mineral Wells, Texas 76067 W/.^i«^^ /4««^ei3!!:yi<^^ 3 ^j&v Civil Air <sl*a*6ta&vnA/.

2A3 Mooney M20E Installation of S-TEC System 60 Pitch Stabilization System, Model ST-050, with Optional Autotrim System according to Bulletin Ho. 153, Revision 1, dated 12-29-81 and Master Drawing List No. 9257, Revision A, dated 12-29-81, or later FAA approved revision.

(14 Volt System) Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8961 dated 7-15-81 Is required for Mooney Models M20C and M20E with S-TEC System 60 Pitch Stabilization System with or without optional Autotrim System.

Compatibility of this modification with other previously approved modifications must be determined by the installer.

S$ckrivriiAJra&tr-^fa&e' May 20, 1981 SL^^^^u^: February 10, 1982 Revision 1 July 15, 1981 (Sigdaturej- _... P. Watson,. , ^ x Acting Chief, Aircraft Certification^isiijS^ \ Division (Title)

FAA FOUM 8 11 0-2 (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 CorporationM20C2A3
Mooney International CorporationM20E2A3