STC SA7214SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
September 15, 1995
Applied
April 14, 1990
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA51EU

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 40/50, single and two axis automatic flight guidance systems, Model ST-462

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.

tf Stain Btpartmtnt of Transportation— jfotaal Station administration Supplemental 'Cgpe Certificate isuvmvev SA7214SW-D <;_T[rr Corporation 946 Pegram Mineral Wells, TX 76067 /^fftr^ ryrr.rBmund r/^Sr/ 23 ^ Federal Aviation A51EU SOCATA TB 9, TB 10, TB 20, and TB 21 (Groupe

AEROSPATIALE) Installation of S-TEC System 40/50, Single and Two Axis Automatic Flight Guidance Systems, Model ST-462, according to Bulletin No. 562, Revision 5, dated 9-06-95 and Master Drawing List No. 92510, Revision E, dated 9-06-95 or later FAA Approved revisions of the above data (28 Volt System).

1. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89857, dated 5-09-90 is required for System 40 in SOCATA Model TB 10 or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part of this STC. ) £&/m*nt 4-14-90 5-09-90 : 9-15-95, Revision 1 Wi "Priam J. Thomas DAS Staff Coordinator, DAS 5 SVJ (Tiilt)

TAu tatifitatt may kt traiuftrrej m ttnrdaittt untk FAR 21.17.

Uratd £tatn of amain Bepartment of Transportation— .federal Station administration Supplemental Itgpe Certificate(Continuation .Sheet) SA7214SW-D, Revision 1 Limitations and Conditions (con't.)

2. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89858, dated 5-09-90 is required for System 40 in SOCATA Models TB 20 and TB 21 or later FAA Approved revisions of the above supplement.

3. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89859, dated 5-09-90 is required for System 50 in SOCATA Model TB 10 or later FAA Approved revisions of the above supplement.

4. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89860, dated 5-09-90 is required for System 50 in SOCATA Models TB 20 and TB 21 or later FAA Approved revisions of the above supplement.

5. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89857-1, dated 9-15-95 is required for System 40 in SOCATA Models TB 9 and TB 10 or later FAA Approved revisions of the above supplement.

6. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89859-1, dated 9-15-95 is required for System 50 in SOCATA Models TB 9 and TB 10 or later FAA Approved revisions of the above supplement.

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

.I'M alterattun nf this certificate is punishable by afint aj not exceeding Sl,000, or imprisonment not exceeding 3 Years, or bnth.

FAA FORM aiio-2-i (io-«») T/tit catifeatt may It tramfrr'tJ in accordant! with FAR .7.•//"•.

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 (O^ame of transferee) (Address of transferee) (ffym&er andstreet) (City, State, antCZlf cade) from CHamt of grantor) (Trint or type) (Address of grantor) (%lum6er and street) (City, State, atutZVS code) Exent of Authority (if licensing agreement) :

Signature of grantor (In 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 · 4

MakeModelData sheet
SOCATA - Groupe AerospatialeTB10A51EU
SOCATA - Groupe AerospatialeTB20A51EU
SOCATA - Groupe AerospatialeTB21A51EU
SOCATA - Groupe AerospatialeTB9A51EU