STC SA6044SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
December 4, 1985
Applied
November 27, 1985
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS3A16

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-283.

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.

ttmtri £tatt« of amrriea Bcpartmcnt of TCransportarion — Jfedcral atriation administration Supplemental 'Cgpe Certificate iSbu#n<vevt' SA6044SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 riaf * 3 Civil Air £sfia*ruL{ <Jfcau*S —— -^ 3A16 BEECH 95, B95, B95A, D95A AND E95 nae- :17 Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-283, according to Bulletin No. 383, dated 10-17-85 and Master Drawing List No. 92341, dated 10-17-85 and/or later FAA Approved revisions of the above data (28 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89627, dated 12-04-85 is required for Beech Models 95 and B95 and/or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part of this STC.)

11-27-85 12-04-85 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Till,)

Tkii crrtiJuAti may kt trtaafemd in accordant with FAR 21,47.

fAA fo«. ( 1 1 ft-J ( 1 &-«!)

ttnittd gtatts of amtrira Bcpartment of transportation— federal a&iation administration Supplemental HDgpe Certificate(Continuation £heet) SA6044SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89643, dated 12-04-85 is required for Beech Models B95A, D95A and E95 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.

' i .il'••ration of this certificate is punishable by a fine of not exceeding SI,OOP, or imprisonment not exceeding 3 \rars, M b^th

••\ I ORM eiio-2-1 (10-69) This certificate may be trantjerrtd in accordance ititti J-'Ali .'/ •/."

1 he appropriate FAA Regional Office of the Iranifer of thit Supplemenul Type Certificate.

The FAA will reissue the certificalc in the name of che transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of transferee). strut) . Stall, fiut ZIP **** I from (Nome of grantor) (Print or type).

(Address of grantor) (Xumkf tnJ ttrtilj 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 · 5

MakeModelData sheet
Beechcraft Corporation953A16
Beechcraft CorporationB953A16
Beechcraft CorporationB95A3A16
Beechcraft CorporationD95A3A16
Beechcraft CorporationE953A16