STC SA5210SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
October 3, 1983
Applied
August 17, 1983
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 40/50 single and two axis automatic flight guidance system Model ST-188-40/50.

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.

fcratrd grata of anrrica Bepartmcnt of transportation — jf edcral atiiation administration Supplemental 'Cgpe Certificate SA5210SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 A^&Mt^rri^m&iftfiJw^ ^ j&Jn*.' v>'»' ' nil <sl£aM£a/u> BEECH H35, J35, K35, M35, N35, AND P35 'rkae- • Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-188-40/50, according to Bulletin No. 288, dated 7-20-83 and Master Drawing List No. 92216, dated 7-20-83 and/or later FAA Approved Revisions of the above data (14 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89256, dated 10-3-83 is required for S-TEC System 40 and/or later FAA Approved revisions of the above supplement.

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

^W . ,«. x? _« / j x .. -«. / -* / . / j./ j , /? . , / / /s , . ^M ^ j. j ^^cfa^^^£n^rvMa^'^a^aM^Affr^'u^^£rif> £Xtvn^vni&J?a£pr-*]fan*>' 8-17-83 10-3-83 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW

This certificate may be transferred in accordance with FAR ?1A7.

United $tatrs of SUntrira Btpartment of toansportation— federal aoiation administration Supplemental ICgpe Certificate(dondnuadon £heet) SA5210SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89257, dated 10-3-83 is required for S-TEC System 50 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.

.!•:; ..':• r-.'.':.. •: nf this certificate is punishable by a Jim of not exceeding Si. 000, i>r imfirisnnment not exceeding 3 years, i>r h'i/h ano-2-1 ,10-69) 7/,,f certificate may be t'-ir-ffrrtd in accordance with 1-'AI< -7 / PAGE2 Qp2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of 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, State, and ^1P code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579

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