STC SA8376SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
December 6, 1993
Applied
November 11, 1993
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA-649

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 two axis automatic flight guidance system, Model ST-512.

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.

SSosa if 3Kria Btpartrarnt of transportation — jfttoal Station administration Supplemental 'Cgpe Certificate i/u*m009t' SA8376SW-D S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 -^,£^-ai^M^/^ 23 y^- Federal Aviation : A-649 BEECH

- D17S (UC-43, UC-43B, 6-1, G-2), AND SD17S Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-512, according to Bulletin No. 612, dated 11-09-93 and Master Drawing List No.

92602, dated 11-09-93 with Optional Flight Director/Steering Horizon or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible on the above models when modified with IR-985-APS-4 Engine.

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

.^^.<!^^ SZc/m*nt* 11-11-93 12-06-93 Mil flam J. Thomas DAS Staff Coordinator. DAS 5 SU (Tiilt) Any alteration oflhit uitifieatt it punishablt by a.fint of not ticttJinf 11,000, or imprisonment not txcetding 3j#ars, at both.

TAo ttrtifitalt may 6* tivafmid in tenrJtiia wttk FAR 21.17.

tlmtrd Skaos af 3nmf3 Btpartmtnc of transportation — jftdtral Sttnation administration Supplemental Ttgpc Certificate(Continuation SA8376SW-D Limitations and Conditions (con't.)

2. FAA/DAS Approved Supplemental Flight Manual, P/N 891042, dated 12-06-93 is required for Beech Models D17S (UC-43, UC-43B, 6-1, 6-2) and SD17S And The Above Models When Modified With IR-985-APS-4 Engine or later FAA Approved revisions of the above supplement.

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

.I'M aitrrittiun af this certificate is punishable by afiiu of not exceeding 11,000, or imprisonment not exceeding 3 years, or h^ih *AA FORM (110.2.1 (io-4») Tliii ttitiftaii may bi ttmtfrtrtd in Mcardanit wil/t I'A It .'/./'.

FACE 2 OF 2 PACES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number __ to (Name of transferee) (Address of transferee) (Number and street) (City, Slate, and <XP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF—205-579

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 · 5

MakeModelData sheet
Raytheon Aircraft CompanyD17S (Army UC-43)A-649
Raytheon Aircraft CompanyD17S (Army UC-43B)A-649
Raytheon Aircraft CompanyD17S (Navy GB-1)A-649
Raytheon Aircraft CompanyD17S (Navy GB-2)A-649
Raytheon Aircraft CompanySD17SA-649