STC SA5209SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
September 28, 1983
Applied
August 29, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A15

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 system Model ST-186-40/50.

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.

Hnitri 3tato Bepartmtnt of Transportation— .federal atriarion administration Supplemental l^pe Certificate SA5209SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 y^^^^^^ 3 4&4n*/ ClVl I Air JAlb BEECH S35, V35, V35A, AND V35B Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-186-40/50, according to Bulletin No. 286, dated 7-18-83 and Master Drawing List No. 92214, dated 7-18-83 and/or later FAA Approved revisions of the above data, (14 Volt System).

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1. Also eligible on the above models when modified by STC SA1035WE (Turbocharged Engine).

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

: 8-29-83 9-28-83 StXdrni#i4&&a£>r-j3f.£n+ff r (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

Tku certificate may tx transferred in accordance with FAR 21.17.

FAA FtMM tl 10-2 (10-«l)

United Staffs of amenta Bepartment of transportation— federal Sttriation administration upplemental tlgpe Certificate(Continuation £heet) SA5209SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89250, dated 9-28-83 is required for S-TEQ .System 40 and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89251, dated 9-28-83 is required for S-TEC System 50 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.

/Irn alteration of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding, .3 years, or both FAA FORM Biio-2-1 (1O-69) This certificate may be transferred in accordance with 1'AR -V.V.7 PAGE 2 OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and %IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street j (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 · 4

MakeModelData sheet
Beechcraft CorporationS353A15
Beechcraft CorporationV353A15
Beechcraft CorporationV35A3A15
Beechcraft CorporationV35B3A15