Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
June 30, 1997
Applied
June 26, 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 5, 2025.

What it approves

Installation of S-TEC System 30 ALT Altitude Hold System, Model ST-704.

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: SA09252AC-D This certificate issued to: S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 Part I of the Cind Is Regulations.

Original Product Type Certificate Number: ZAIS 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 30 ALT Altitude Hold System, Model ST-704, according to Bulletin No.

804, dated 6-25-97 and Master Drawing List No. 921010, dated 6-25-97 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: 6-20-97 Date roosted:

Date of ascence: 6-30-97 Date Amended:

By Direction of the Administrator FEDERAL AVIATION Wein th TOMINISTRATO 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: SA09252AC-D Limitations and Conditions: (con't.)

2 FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891444, dated 6-30-97 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) 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 891445, dated 6-30-97 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) 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 891446, dated 6-30-97 is required for Piper Model PA-28-201T 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.

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

The FAR will reissue the certificate in the name of the transferee and forward it to sim.

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