STC SA5137SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
June 15, 1984
Applied
December 14, 1982
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDSA3SO

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 60 pitch stabilization system Model ST-099 with optional automatic electric trim system.

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.

United £tatu of amenta Bepartmcnt of TDrausportation — federal 2Uriatfon administration Supplemental t:uj)e Certificate SA5137SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067JySl*/d^^ii ^^ JA^fittt^^n^fi^cdu^/^'i^ J»f*Ja Air Gt*iatnaJ Ctfcauet —— . A3SO PIPER PA-32^301, PA-3^-301T, PA-32R-301 AND PA-32R-301T Installation of S-TEC System 60 Pitch Stabilization System, Model ST-099, with Optional Automatic Electric Trim System according to Bulletin No. 202, Revision 1, dated 6-14-84 and Master Drawing List No, 92163, Revision A, dated 6-14-84 and/or later FAA Approved revisions of the above data (14 Volt System) .

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89180, dated 2-24-83 is required for Piper Models PA-32R-301 and PA-32R-301T and/or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part of this STC) 12-14-82 2-24-83 SxdminiA/ra£>r'^p 6-15-84, Revision 1 (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW (TttU)

Thii certificate may be transferred in accordant* with FAR 21.17.

ttnittd &tatts of Smtrica ©epartment of Transportation—federal atriation administration Supplemental 'Cgpe Certificate(Continuation ^htct) SA5137SW-D , Revision 1 Limitations and Conditions (con't) 2 FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89477, dated 6-15-84 is required for Piper Models PA-32-301 and PA-32-301T and/or later FAA Approved revisions of the above supplement.

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

.In) iilifrafiun of this certificate is punishable by a fine oj not exceeding SI,000, or imprisonment not exceeding 3 years, or bu TAA FORM 8110-2-1 (10-69) This certificate may be transferred in accordance with i'.\R -'/ 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, State, and <7P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^1P code) Extent of Authority (if licensing agreement):

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 · 5

MakeModelData sheet
Piper Aircraft Inc.PA-32-301A3SO
Piper Aircraft Inc.PA-32-301TA3SO
Piper Aircraft Inc.PA-32R-301 (HP)A3SO
Piper Aircraft Inc.PA-32R-301 (SP)A3SO
Piper Aircraft Inc.PA-32R-301TA3SO