STC SA5173SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
June 29, 1983
Applied
April 22, 1983
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 pitch stabilization system ST-051 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.

Hnitri goto of 3«rrica Bepartment of transportation— federal atnation Administration Supplemental t:gpe Certificate , sl£*a*da dp*aina4 \Ji*x/uc£ SA5173SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wo Hers Industrial Complex Mineral Wells, TX 76067 3 Civil Air 3A15 BEECH 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, G33, AND F33A, S/N CE-315 AND BELOW.

Installation of S-TEC System 60 Pitch Stabilization System, Model ST-051 with Optional Automatic Electric Trim System according to Bulletin No. 154, Revision 2, dated 2-14-83 and Master Drawing List No. 9246, Revision B, dated 2-14-83 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8952-1, dated 6-29-83 is required for Beech Models 35-C33, 35-C33A, E-33, E33A, F33, F33C, E33C, G33 and F33A, S/N CE-315 and below.

(See Continuation Sheet, Page 2, a part of this STC) .- 4-22-83 6-29-83 (Signahoi) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (TitU)

Tkit ttrtificatt may h trtoaftmd in aceorjonct with FAR 21.47.

FAA FOMI •! 10-2 (10-M)

ttratrd Stow of 2ncrto Bepartmtnt of Transportation— .federal Soiation administration Supplemental ^Cgpe Certificate(Continuation £heet) SA5173SW-D (Con't) 2 FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89121-1, dated 6-29-83 is required for Beech Models 35-33, 35-A33, and 35-B33 and/or later FAA Approved revisions of the above supplement.

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

FAA FORM stio-2-1 (1O-69) This ctrtifcalt may bt transferred in accordance with FAR 21.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee) (Address of transferee) (Number and street) (City, Slate, and ^IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Z.IP 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