STC SA6041SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
October 23, 1985
Applied
October 17, 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 6, 2025.

What it approves

Installation of S-TEC System 40/50,Single and Two Axis Automatic Flight Guidance Systems, Model ST-287-40/50.

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.

ttratri £tattt of 3ntrica jBepartmcnt of tonsportation—jftdtral Station administration Supplemental t:gpe Certificate i/Mvmvw' SA6041SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 »i^ r xzJ AfifryK*" •™e''*f**n /me*& J&£ M^rwtsr&.4/n&&jr*&aAr«rri^n& ** J&ft -J M ^/i^ LI VI I Air 3A1 6 BEECH 95, B95, B95A, D95A AND E95 _/ ^A&an Installation of S-TEC System 40/50, Single and Two Axis Automatic Flight Guidance Systems, Model ST-287-40/50, according to Bulletin No. 387, dated 10-15-85 and Master Drawing List No. 92343, dated 10-15-85 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 89629, dated 10-23-85 is required for S-TEC System 40 in 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.)

n^z^nf Act/tfi*>i^'n^da^'M>fu*w^jA4'4aA^^^;aJukr<n>a£A/ui& >^^Z^^z^<5^<OlC<^^.^>^ Sxdmt*uAJ+a& 10-17-85 10-23-85 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Titlt)

This certificate may be IraniJirmJ in actorfanct with FAR 21.47.

FAA POM (11O-2 (1O-M)

ttnitrd £tatu of 2mtrifa Btpartmtnt of transportation— Jf edtral Sttriation administration Supplemental i;gpt Certificate(Continuation SA6041SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89644, dated 10-23-85 is required for S-TEC System 40 in Beech Models B95A, D95A and E95 and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89630, dated 10-23-85 is required for S-TEC System 50 in Beech Models 95 and B95 and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89645, dated 10-23-85 is required for S-TEC System 50 in Beech Models B95A, D95A and E95 and/or later FAA Approved revisions of the above supplement.

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

.U; ,ii!--Tii/iim fij this certificate is punishable by a fine of not exceeding Si, 000, or imprisonment not exceeding 3 years, «r huf

•-AA r ORM siio-2-1 (to-69) This certificate may be transferrnl in accordance it-illi 1'AR ~'l • PAGE 2 OF 2 PAGES

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

(Address of transferee). ( Mumtxr *nd ttrttt) (City. Stalt, ••xtZlP «">*> from (Nome of grantor) (Print or type).

(Address of grantor) f A'vmA/T mitd Urnl j (City. Suit, 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