STC SA6092SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
October 15, 1986
Applied
October 9, 1986
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 65 two axis automatic flight guidance system, Model ST-387.

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.

Umtrd 3tatei of ammca Bcparrmcnt of transportation -federal aoiation administration Supplemental TCpe Certificate SA6092SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 a^ 3 ^at Znt Li VI I Air ..flfaij fJr^at rui/ ijroauc/ —— •^'uJis~(ji4'p6jUca4e'iSu*rnue>r- oAlD BEECH 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C AND G33 s/ufi* -J seAjja-r Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System, Model ST-387, according to Bulletin No. 487, dated 10-06-86 and Master Drawing List No.

92397, dated 10-06-86 and/or later FAA Approved revisions of the above data (14 Volt System).

1. Only eligible on Beech Model F33A, S/N CE-315 and Below. •1 •»

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA-.,Approved Airplane Flight Manual, P/N 89706, dated- 10-15-86 is required for Beech Models 35-33, 35-A33, 35-B33 and/or later FAA Approved revisions of the above supplement.

(See Coi»*4riuation Sheet, Page 2, a part of this STC.)*—r— fAvm*um'An'^U4c/<jvn&6A v^e^rntn^A^r^^£a^^^nervfiAf'^^£a^fi^A^a^ 10-09-86 10-15-86 (Sirnaturi) Did W.Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

Tkii certificate may be trmsfrmj in •ccfr^ana with FAR 21AT.

»AA FOM • 110-2 (l o-A«)

tinted States of 2Uncrira Btpartment of ^transportation— .federal Station administration Supplemental H$$t Certificate(Condnuadon «Sheet) SA6092SW-D Limitations and Conditions (con't)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89707, dated 10-15-86 is required for Beech Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, S/N CE-315 and Below F33C and G33 and/or later FAA Approved revisions of the above supplement.

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

.I'n ultnntiun of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or /><>//•

• AA f ORM eno-2-1 (10-69) This ctrttfeatt may be transferred in accordance trtlli 1-'AI< -I ^~ PAGE 2 OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemenul Type Certincate Number to (Name of transferee).

(Address of transferee). I Mumtxr tnd Oral) (City. Stall. *nd y? nJt y from (Name of grantor) (Print or type).

(Address of grantor) t Hi j itt. Slflt, Extent of Authority (if licensing agreement):.

Signature of grantor (In ink):

• it « r. » n i«««-««»-(>«>

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
Raytheon Aircraft Company35-333A15
Raytheon Aircraft Company35-A333A15
Raytheon Aircraft Company35-B333A15
Raytheon Aircraft Company35-C333A15
Raytheon Aircraft Company35-C33A3A15
Raytheon Aircraft CompanyE333A15
Raytheon Aircraft CompanyE33A3A15
Raytheon Aircraft CompanyE33C3A15
Raytheon Aircraft CompanyF333A15
Raytheon Aircraft CompanyF33A3A15
Raytheon Aircraft CompanyF33C3A15
Raytheon Aircraft CompanyG333A15