STC SA5286SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
March 13, 1984
Applied
March 10, 1984
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA18EU

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 automatic flight guidance systems Model ST-184-40/50.

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.

Uritri gtora of 2tamca Bepartmtnt of Transportation— Jfataral 2toiation administration Supplemental t^pe Certificate SA5286SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 £^4< tn^otJin* ASutrvof'A ^&j si£<atda/ Air AlotU

REIMS-CESSNA Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-184-40/50, according to Bulletin No. 284, Revision 1, dated 3-09-84 and Master Drawing List No. 92212, Revision A, dated 3-09-84 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 89420, dated 3-13-84 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), M#^ ;£ei*vrii/n*a£u>wd^ S&*mAruAjra£c+-4)p-a f 3-10-84 3-13-84 (Signalart) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (TM.)

This ctrtifimtt may In transfrntd in accordant* with FAR 21.47.

FAAPo*M tnO-2(IO-6«)

Bnitrfl $tatts of America Bepartment of transportation—federal Sltriation SWministration Supplemental HTjipe Certificate(Continuation £heet) tSVMWlVeW- SA5286SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89423, dated 3-13-84 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.

:V alteration nf this certificate is punishable by a fine of not exceeding Si,000, or imprisonment not exceeding .3 years, or both FAA FORM ano-Z-l (1O-69) This certificate may be transferred in accordance with I'AK ^1 47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ^JP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^IP 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 · 1

MakeModelData sheet
Cessna Aircraft CompanyFR172KA18EU