STC SA4158SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
March 19, 1982
Applied
July 15, 1980
Product
Aircraft · Small Airplane
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 60 two axis automatic flight guidance system, Model ST-009 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.

Unitri grates of amcrica Bcpartmcnt of transportation —.federal 3toiation administration Supplemental t^gpe Certificate <yKuyryW€w SA4158SW Project A5696SW-DS S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 &wf^jA&j[ic>6U>^^ jifi*&ft^Jie>rt*7n'/mc*&JfoJa^^ 3 <slea*da&<mA'.

£J>*iai-na/ iJrcctuef —— Civil Air 3A15 Beech

35.33 35-A33, 35-B33, 35-C33, 35-C33A, E33,E33A, E33C, F33, F33A, S/N CE-115 and below, F33C, G33 of s-TEC System 60 Two /xis Automatic Flight Guidance System, Model ST-009 with Optional Autotrim System, according to Bulletin No. 109, Revision 5, dated 2-25-82 and Master Drawing List No. 9213 Revision E, dated 2-25-82 with Optional Flight Director Steering Horizon;

or later FAA approved revision. (14 Volt System) See Continuation Sheet, page 2 of this STC.

;£cMri^ S%drru#uAJr<z£>^J(p^ihe<

• July 15, 1980 July 29, 1980 . 2/3/81; 4/3/81; 3/19/82 Revision 3 (Signature) ^ Don P. WatsonActing Chief, Aircraft Certification

FAA FCMM 8110-2 (10-68)

ttnittd Starts of arnica Bepartment of transportation— federal Striation administration topplemtntal t:jp Certificate(Continuation £heet) tSVMWlWeW SA4158SW Revision 3 Limitations and Conditions :

1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, P/N 8910 dated July 29, 1980, is required for Beech Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, G33, F33A S/N CE-315 and Below with S-TEC System 60 (Two Axis) Flight Guidance System, Model ST-009.

2. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, P/N 8910-1 dated 4/3/81, is required for Beech Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, G33, F33A S/N CE-315 and Below with S-TEC System 60 (Two Axis) Flight Guidance System, Model ST-009 and Optional Autotrim System.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89119 dated March 19, 1982, for Beech Models 35-33, 35-A33, and 35-B33 with S-TEC System 60 Two Axis Automatic Flight Guidance System.

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

FAA FORM Biio-2-1 (1O-69) PAGE 2OF 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 <?/> code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ?JP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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 · 12

MakeModelData sheet
Beechcraft Corporation35-333A15
Beechcraft Corporation35-A333A15
Beechcraft Corporation35-B333A15
Beechcraft Corporation35-C333A15
Beechcraft Corporation35-C33A3A15
Beechcraft CorporationE333A15
Beechcraft CorporationE33A3A15
Beechcraft CorporationE33C3A15
Beechcraft CorporationF333A15
Beechcraft CorporationF33A3A15
Beechcraft CorporationF33C3A15
Beechcraft CorporationG333A15