STC SA5328SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
August 1, 1984
Applied
June 4, 1984
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 5, 2025.

What it approves

Installation of S-TEC yaw damper system, model ST-251.

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.

ltaM Hiritri States of ararrita Bepartmtnt of 'Crausportation— Jpcdtral 2toiation administration Supplemental 'Cgpe Certificate i/u&mver' SA5328SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 *fcta*a1U4 1A10 PIPER PA-23-250 AND PA-E23-250 ClVll Air i/um *x ^/.-ufie —£ ^e&ian Installation of S-TEC Yaw Damper System, Model ST-251, according to Bulletin No.

351, Revision 1, dated 7-20-84 and Master Drawing List No, 92280, Revision A, dated 7-20-84 and/or later FAA Approved revisions of the above data (14 Volt System).

1. Eligible only on Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 thorugh S/N 27-7554172.

2. Also eligible on the above models when equipped with Approved Turbocharged Engines (250 H.P.) and/or Wing Tip Tanks per STC SA1480WE.

CqatinuaUon Sheet, Page 2, a part of this STC)<yt£&teMna^/i*-A4jstsi&^4M^jza/&Mjfu4WJ&Jf/i&&iA^'J^ ^e^7ntna£M^ £xdm&ni&£ra£e>r-,€&4&0 8-1-84, Revision 16-04-84 6-27~84 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)———————— ___ ___ __ \ *----/___

FAAFo«* 8110-2(10-48)

Unitrd Starts of SLntnra Bepartment of tensportation— federal Station administration Supplemental t:gpe Certificate(Continuation £heet) SA5328SW-D, Revision 1 Limitations and Conditions (con't) 3 FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89474, dated 6-27-84 is required for Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-7554172 and the above models when equipped with Approved Turbocharged Engines (250 H.P.) and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89474-1, dated 8-1-84 is required for Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-7554172 and the above models when equipped with approved Turbocharged Engines (250 H.P.) and/or Wing Tip Tanks per STC SA1480WE and/or later FAA Approved revisions of the above supplement.

5. Compatability of this modification with other previously approved modifications must be determined by the installer, . I' ; :il(fin>inn oj this certificate is punishable by a fine of not exceeding 51,000, or imprisonment not exceeding 3 years, nr />o/A <AA FORM 8MU-2-I (10-69) This certificate may be trans/trrtci in accordance ii'ilh I'AR ;.'/.•/."" PAGE 2 OF 2

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee) (Address of transferee) (Number and street) (City, Slate, and <7P cade) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and QP 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 · 2

MakeModelData sheet
Piper Aircraft Inc.PA-23-2501A10
Piper Aircraft Inc.PA-E23-2501A10