STC SA5185SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
October 7, 1991
Applied
July 7, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS2A13

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 systems, Model ST-176-40/50.

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.

•Department of transportation— federal 3triation administration Supplemental l^pe Certificate */U*m0er' SA5185SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 3 Civil Air : 2A13 . PIPER PA-28RT-201 and PA-28RT-201T Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-176-40/50, according to Bulletin No. 276, Revision 1, dated 4-16-91 and Master Drawing List No. 92204, Revision A, dated 4-16-91 and/or later FAA Approved revisions of the above data (14 Volt System).

1. Only eligible on Models PA-28RT-201, S/N 28R-7918070 & Up and PA-28RT-201T, S/N 28R-7931100 & Up

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89226, dated 8-03-83 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.)

7-07-83 8-03-83 4-29-91, 10-07-91, Revision 2 WilliarrrJ. Thomas DAS Staff Coordinator, DAS 5 SW (Title) Any alteration ofthil certificate it fntnithable fy a. fine of ml exceeding SlflOO, or imprisonment not exceeding 3ytont or both.

Tkit errtiftttt m*y tt tiuufentd in «nr«bw» willt FAX 21.47.

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ttratrd Skatu Bcpartmcnt of Transportation— .federal 3tnaoon administration ^Supplemental ICgpe Certificate(Continuation Sheet) SA5185SW-D, Revision 2 Limitations and Conditions (con't.)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89226-1, dated 4-29-91 is required for S-TEC System 40 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 89227, dated 8-03-83 is required for S-TEC System 50 and/or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89227-1, dated 4-29-91 is required for S-TEC System 50 and/or later FAA Approved revisions of the above supplement.

6. Compatibility of this modification with other previously approved modifications must be determined by the installer.

•I HI alteration of this certificate is punishable by a fait of not exceeding SI,000, or imprisonment not exceeding 3 years, or bnih.

AA FORM itio-J-i (to-M) Tlai cettifeatt may bt trmsftmd in aetatdaati with FAR -'/.^* PAGE 2 OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, Slate, and £IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Stale, and <7/> code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):.

U.S. GOVERNMENT PRINTING OFFICE : I 96« 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 · 2

MakeModelData sheet
Piper Aircraft Inc.PA-28RT-2012A13
Piper Aircraft Inc.PA-28RT-201T2A13