STC SA4400SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
April 5, 1982
Applied
May 18, 1981
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 60 pitch stabilization system Model ST-055 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.

tSleaMta& United $tatu of amrrica Bepartmcnt of transportation—federal Htriation administration Supplemental 'Cgpe Certificate iStsurrvvev' SA4400SW S-TEC Corporation Rt. 4, Bld§. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 j^jA^^e>M^ ^M'MAi*uwi^uw£^ 3 jf^^nf Civil Air 3A15 Beech H35, J35, K35, M35, N35, P35 Installation of S-TEC System 60 Pitch Stabilization System, Model ST-055 with Optional Autotrim System according to Bulletin No. 158, Revision 1, dated 1-26-82 and Master Drawing List No. 9253, Revision A, dated 1-26-82, or later FAA approved revision. (14 Volt Sy*t«n) See Continuation Sheet, page 2, of this STC.

JeeLini^^ SXcJniini&foaler-djke' May 18, 1981 June 30, 1B81 April 5, 1982 Revision 1 / ^Signature) Don P. Watson Acting Chief, Aircraft Certification Division ——————————————————— (Title)

FAA FO«M 8110-2 (10-68)

Unitrd #tatu of America Bepartment of transportation— federal attation administration Supplemental t:gpe Certificate(Continuation SA4400SW Revision 1 Limitations and Conditions :

1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, P/N 8955, dated June 30, 1981, is required for Beech Models H35, J35, K35, M35, N35, P35, P/N 8955, with S-TEC System 60 Pitch Stabilization System, Model ST-055 without optional trim; OR FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8955-1 dated April 5, 1982, is required for Beech Models H35, J35, K35, M35, N35, and P35 with S-TEC System 60 Pitch Stabilization System with Optional Trim.

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

FAA FORM siio-2-1 (1O-69) PAGE2 OF2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number _ to (Name of transferee) (Address of transferee) (Number and street) (City, Stale, and <Y/> 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):.

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 · 6

MakeModelData sheet
Beechcraft CorporationH353A15
Beechcraft CorporationJ353A15
Beechcraft CorporationK353A15
Beechcraft CorporationM353A15
Beechcraft CorporationN353A15
Beechcraft CorporationP353A15