STC SA8387SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
May 16, 1994
Applied
May 9, 1994
Product
Aircraft · Single-Engine
Certification basis
Part 1, 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 40/50 single and two axis automatic flight guidance systems, Model ST-530-40/50.

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Anita Smas d 2ama Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 5A838754-0 This certificate issued to: S-TEC Corporation 946 Pegram Mineral Wells, TX 76067 Certifies that the change in the type design for the following product with the limitations and conditions shamefor as specifed hereon meets the airworthiness requiremonis of Port 3 sp the CiVIl Air Regulations Original Product -Typo bontificator Numbon: 2A13 Make: PIPER Model: PA-28-161, PA-28-181, PA-28-2017 Description of Type Design Change: and PA-28-236 Installation of S-TEC 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-530-40/50, according to Bulletin No. 630, dated 5-06-94 and Master Drawing List No. 92679, dated 5-06-94, or later FAA Approved revisions of the above data (28 Volt System).

1. FAA/DAS Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual Supplement, P/N 891062, dated 5-16-94 is required for Piper Models PA-28-161, PA-28-181, and PA-28-236 for S-TEC System 40 or later FAA Approved revisions of the above supplement.

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

Thomas DAS Staff Coordinator, DAS 5 SW (Title)

FAA 1O86 8110-2 (10-68)

*mired Scares of Alerica Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number S83875N-D Limitations and Conditions: (con't) FAA/DAS Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual Supplement, P/N 891063, dated 5-16-94 is required for Piper Model PA-28-201T for S-TEC System 40 or later FAA Approved revisions of the above supplement.

3. FAA/DAS Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual Supplement, P/N 891064, dated 5-16-94 is required for Piper Models PA-28-161, PA-28-181, and PA-28-236 for S-TEC System 50 or later FAA Approved revisions of the above supplement.

FAA/DAS Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual Supplement, P/N 891065, dated 5-16-94 is required for Piper Model PA-28-201T for S-TEC System 50 or later FAA Approved revisions of the above supplement.

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

11l :1.17.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number - to (Name of transferee) _ (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) - (Address of grantor) (Number and street) (City, State, and ZIP code) Extent of Authority (if licensing agreement): _ Date of Transfer:

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 · 4

MakeModelData sheet
The New Piper Aircraft Inc.PA-28-1612A13
The New Piper Aircraft Inc.PA-28-1812A13
The New Piper Aircraft Inc.PA-28-201T2A13
The New Piper Aircraft Inc.PA-28-2362A13