STC SA4414SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
May 12, 1982
Applied
May 5, 1981
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 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.

United States of amenta Bepartment of transportation—federal aoiation administration Supplemental 'Cgpe Certificate <yKwm&€w SA4414SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 v*fytSi&;ebeAjjiawf^*£n^f(>ftc>t*ftM^Jw*>du^M>tJ&^ 3 Civil Air <slea<da£&n&.

3A15 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, G33, F33A, S/N CE-315 and Below Installation of S-TEC System 60 Pitch Stabilization System, Model ST-051, with Optional Autotrim System, according to Bulletin No. 154, Revision 1, dated 3/26/82 and Master Drawing List No. 9246, Revision A, dated 3/26/82, or later FAA approved revision. (14 Volt System) See Continuation Sheet, page 2, of this STC.

Jewni<nJa& S&c&nimibfaa&r-dj&e' May 5, 1981 July 14, 1981 May 12, 1982 Revision 1 Don P. Watson /(**'«>">")Acting Chief, Aircraft CertificationDivision - Southwest Region (Title)

This certificate may he transferred in accordance with FAR 21.47.

FAA Fow 8110-2 (10-68)

Hinted &tatu of America Bepartmcnt of transportation— federal SOiation administration upplemental l^jpe Certificate(Continuation £heet) SA4414SW Revision 1 Limitations and Conditions:

1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8952 dated 7/14/81, is required with Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, 633, and F33A, S/N CE-315 and Below with S-TEC System 60 Pitch Stabilization System.

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 89121 dated 5/12/82, is required for Models 35-33, 35-A33, and 35-B33 with S-TEC System 60 Pitch Stabilization System.

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

FAA FORM siio-2-1 (1O-69) 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 %1P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Slate, and £//> 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