STC SA7217SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
June 11, 1990
Applied
May 3, 1990
Product
Aircraft · Single-Engine
Certification basis
Part 1, Part 21
Data sheet
TCDSA51EU

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

What it approves

Installatin of S-TEC system 60 pitch stabilization system, model ST-461, with optional automatic electric trim 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.

Bcpartmrnt of Transportation —.federal atrian'on administration Supplemental 'Cgpe Certificate ^/Uvrrdev SA7217SW-D ^ft/L^A. ^*.rrt//~ S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 23 Federal Aviation : A5 1 EU . SOCATA . TB 10, TB 20 and TB 21 (Groupe AEROSPATIALE) Installation of S-TEC System 60 Pitch Stabilization System, Model ST-461, with Optional Automatic Electric Trim System, according to Bulletin No. 561, dated 4-27-90 and Master Drawing List No. 92514, dated 4-27-90. (28 Volt System)

1. Optional Automatic Electric Trim System not eligible on SOCATA Model TB 10 (Groupe AEROSPATIALE).

(See Continuation Sheet, Page 2, a part of this STC.)

i^^-£»»^^£ia^.^«*a^C?..Uj/yi<^ * ^f^^T^ : 5-03-90 6-11-90 (SifnalHrtJ Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW (Till*)

TAtt ctrlifiealt may It ttanifrrrttt in tccmJanu with FAR 21.17.

United gtatts of 3ntnca Bepartmtnt of Transportation— federal Nation administration ^upplcmtntal t:gpt (Eertificatt(Continuation .Sheet) SA7217SW-D Limitations and Conditions (con't.)

2. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89865, dated 6-11-90 is required for SOCATA Model TB 10 (Groupe AEROSPATIALE) WITHOUT TRIM and/or later FAA Approved revisions of the above supplement.

3. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89866, dated 6-11-90 is required for SOCATA Models-TB 20 and TB 21 (Groupe AEROSPATIALE) and/or later FAA Approved revisions of the above supplement.

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

•I'M' alteration of this certificate is punishable by a fine of not exceeding 11,000, or imprisonment not exceeding 3 years, or bmh.

FORM SI 10-2-1 do-«») This cirtijuati may bi transfrrnJ in accordant! with FAR :'1.47 PAGE 2 OF 2 PAGES

INSTRUCTIONS : The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferre and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (blame of transferee) (iAddrtss of transferee) (ffumBer and street) (City, State, andZVP code) from (blame of grantor) (Print or type) (Address of grantor) (%(um6er and street) (City, State, andZlf code) Exent of Authority (if licensing agreement) :

Signature of grantor (IninQ: __ Page 2 of 2

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 · 3

MakeModelData sheet
SOCATA - Groupe AerospatialeTB10A51EU
SOCATA - Groupe AerospatialeTB20A51EU
SOCATA - Groupe AerospatialeTB21A51EU