STC SA4132SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
November 4, 1981
Applied
May 20, 1980
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, Single Axis, Automatic Flight Guidance System, Model ST-006

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.

mnittd States or America Bepartment of ^transportation—federal 2toiation administration >upplemental t^pe Certificate tyKwmvw' SA4132SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067-9990 ^^ ^s^^i^^ 3 ^5^ Civil Air <-st£&u£a£&n&.

3A15 Beech 36, A36 „. —^—— c«~^. installation of S-TEC System 60, Single Axis, Automatic Flight Guidance System, Model ST-006, according to Bulletin No. 106, Revision 1, dated 8-29-81 and Master Drawing List No. 9207, Revision A, dated 8-29-81, or later FAA approved revision. (14 Volt System) See continuation Sheet, page 2, of this STC.

^ £zdnT*<nt&&a&>r-^jhe' £0 1980 fia&'"fdulMect '.' NOVdnbCr 4, 1981 Revision 1 May 29, 1980 ,. . (Signature)Watson ' * '.cting Chief, Aircraft CertificationDivision (Title)

FAA Fo«M 81 10-2 (10-68)

ttnittd gtatts of America Bepartment of transportation— federal 2ttriation administration Supplemental t^pe Certificate(Continuation &heet) SA4132SW Revision 1 Limitations and Conditions:

1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8906 dated May 29, 1980, is required with S-TEC System 60 Single Axis Automatic Flight Control System.

2. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8906-1, dated November 4, 1981, is required with S-TEC System 60 Single Axis Automatic Flight Control System (using Roll Servo P/N 0105-R9).

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

FAA FORM siio-2-1 (10-69) PAGE « OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name oj 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) (City, Slate, and %IP cade) 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 · 2

MakeModelData sheet
Beechcraft Corporation363A15
Beechcraft CorporationA363A15