STC SA8370SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
July 29, 1994
Applied
July 9, 1993
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS1A10

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 40/50 single and two axis automatic flight guidance systems, Model ST-508.

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.

Bcparnrcnt of transportation —jfotoal Station administration Supplemental l^pc Certificate SA8370SW-D S-TEC Corporation 946 Pegram Mineral Wells, Texas 76067 ^ 3 y^ Civil Air : 1A10 PIPER PA-23 AND PA-23-160 Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-508, according to Bulletin No. 608, Revision 2, dated 7-21-94 and Master Drawing List No. 92587, Revision B, dated 7-21-94 or later FAA Approved revisions of the above data (14 Volt System).

1. Also eligible on Models PA-23 and PA-23-160 When Modified Per STC SA461SW, STC SA636SW, STC SA671SW, and STC SA899SW (Geronimo Conversion).

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

7-09-93 7-22-93 J&*^ri4*^ S£/mini& &L& —— u£J: 11-11-93, 7-29-94, Revision 2 William J. Thomas DAS Staff Coordinator. DAS 5 SW(Tilt.)

Any alteration oftkii ttrtificalt ii punishable by a fine of not exceeding SI,OOP, or imprisonment not exceeding 3 years, or both.

TAii ttrtijuatt may te traniferrtJ in accordant with FAR 21.47.

»AA Htm •) 10-2(10-4*1

ftniad Stain of 2ntnn Bepartment of Transportation— federal Nation administration Supplemental ICgpe Certificate(Continuation £heet) SA8370SW-D, Revision 2 Limitations and Conditions (con't.)

2. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891029, dated 7-22-93 is required for S-TEC System 40 for Piper Model PA-23-160 or later FAA Approved revisions of the above supplement.

3. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891029-1, dated 7_29-94 is required for S-TEC System 40 for Piper Models PA-23 and PA-23-160 or later FAA Approved revisions of the above supplement.

4. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891030, dated 7-22-93 is required for S-TEC System 50 for Piper Model PA-23-160 or later FAA Approved revisions of the above supplement.

5. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891030-1, dated 7_29-94 is required for S-TEC System 50 for Piper Models PA-23 and PA-23-160 or later FAA Approved revisions of the above supplement.

6. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891038, dated I-1-11-93 is required for S-TEC System 40 for Piper Model PA-23-160 When Modified Per STC SA461SW, STC SA636SW, STC SA671SW, and STC SA899SW (Geronimo Conversion) or later FAA Approved revisions of the above supplement.

7. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891038-1, dated 7-29-94 is required for S-TEC System 40 for Piper Models PA-23 and PA-23-160 When Modified Per STC SA461SW, STC SA636SW, STC SA671SW, and STC SA899SW (Geronimo Conversion) or later FAA Approved revisions of the above supplement,

8. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891039, dated II-11-93 is required for S-TEC System 50 for Piper Model PA-23-160 When Modified Per STC SA461SW, STC SA636SW, STC SA671SW, and STC SA899SW (Geronimo Conversion) or later FAA Approved revisions of the above supplement,

9. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 891039-1, dated 7-29-94 is required for S-TEC System 50 for Piper Models PA-23 and PA-23-160 When Modified Per STC SA461SW, STC SA636SW, STC SA671SW, and STC SA899SW (Geronimo Conversion) or later FAA Approved revisions of the above supplement,

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

.•IHV alteration of this certificate is punishable by afiru of not exceeding 11,000, or imprisonment not exceeding 3 years, or hnih.

FAA FORM 1110.2-1 UO-M) THit ciriifeati may bt Hansftrnd in aceotdanct u/ilH I'AK .'/.•/*.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ^IP 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 : I9«6 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
The New Piper Aircraft Inc.PA-231A10
The New Piper Aircraft Inc.PA-23-1601A10