Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
June 26, 1997
Applied
June 24, 1997
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 6, 2025.

What it approves

Installation of S-Tec System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-703-20/30.

What the certificate saysOCR

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA09251 AC-D This certificate issued to: S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specifed horon meets the airmorthiness regurements of Part 3 of the Civil A i Regulations.

Original Product I ype Cerlipcate Number: 2A13 Make: Piper Model: PA-28-151, PA-28-161, PA-28-181, PA-28-236, AND PA-28-201T Description of Type Design Change:

Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-703-20/30, according to Bulletin No. 803, dated 6-23-97 and Master Drawing List No. 921009, dated 6-23-97 or later FAA Approved revisions of the above data (14 Volt System).

Also eligible on Model PA-28-151 When Modified Per STC SA2969SW (160 H.P. Engine Conversion).

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

Date of Application: 6-24-97 Date Reissued:

Date of Issuance: 6-26-97 Date Amended:

By Direction of the Administrator FEDERAL AVIATION Wice Do Themes TOMMISTFATOR William J. Thomas DAS Staff Coordinator, DAS 5 SW (Title)

PAA Form 8110-2 (10-68) Page 1 of 2

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA09251 AC-D Limitations and Conditions: (con't.)

2. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891438, dated 6-26-97 is required for Piper Models PA-28-151, S/N 28-7615001 And Up;

PA-28-161, PA-28-181, and PA-28-236; and PA-28-151, S/N 28-7615001 And Up When Modified Per STC SA2969SW (160 H.P. Engine Conversion) for S-TEC System 20 or later FAA Approved revisions of the above supplement.

3. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891439, dated 6-26-97 is required for Piper Model PA-28-151, S/N 28-7515449 And Below And The Above Model When Modified Per STC SA2969SW (160 H.P. Engine Conversion) for S-TEC System 20 or later FAA Approved revisions of the above supplement

4. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891440, dated 6-26-97 is required for Piper Model PA-28-201T for S-TEC System 20 or later FAA Approved revisions of the above supplement.

5. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891441, dated 6-26-97 is required for Piper Models PA-28-151, S/N 28-7615001 And Up;

PA-28-161, PA-28-181, and PA-28-236; and PA-28-151, S/N 28-7615001 And Up When Modified Per STC SA2969SW (160 H.P. Engine Conversion) for S-TEC System 30 or later FAA Approved revisions of the above supplement.

6. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891442, dated 6-26-97 is required for Piper Model PA-28-151, S/N 28-7515449 And Below And The Above Model When Modified Per STC SA2969SW (160 H.P. Engine Conversion) for S-TEC System 30 or later FAA Approved revisions of the above supplement.

7. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891443, dated 6-26-97 is required for Piper Model PA-28-201T for S-TEC System 30 or later FAA Approved revisions of the above supplement.

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

FAA Porm 8110-2-1(10-69) Page 2 of 2

The FAA will reissue the certificate in the name of the transferee and forward it

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 & street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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 · 5

MakeModelData sheet
Piper Aircraft Inc.PA-28-1512A13
Piper Aircraft Inc.PA-28-1612A13
Piper Aircraft Inc.PA-28-1812A13
Piper Aircraft Inc.PA-28-201T2A13
Piper Aircraft Inc.PA-28-2362A13