STC SA5364SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
December 20, 1984
Applied
October 30, 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 6, 2025.

What it approves

Installation of S-TEC System 60 pitch stabilization system, Model ST-266, 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.

lfatt ftae ttnitrd grates of amrrica Bepartmcnt of ^transportation —federal atiiation administration supplemental Itgpe Certificate <L/uvmv&r' SA5364SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 .-4*f J^ 3 *& Jiht ClVI I Air 1 A 1 U PIPER PA-23-250 AND PA-E23-250 jx ^/y/i-e —/ ^eA^a n ~fjsia «<z* • Installation of S-TEC System 60 Pitch Stabilization System, Model ST-266, with Optional Automatic Electric Trim System, according to Bulletin No. 366, dated 10-22-84 and Master Drawing List No, 92300, dated 10-22-84 and/or later FAA Approved revisions of the above data (28 Volt System).

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

(See Continuation Sheet, Page 2 a part of this STC), .^^t& & *A 10-30-84 v7«tf^^^^z^W-^W^^^c<^>^^^^^i^^ £Xdrri4mjA (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW \ ----~/

. 81 1O-2(IO-63J

ttnitrd &taw of 2Lmcnra Bcpartmcnt of "Cransportation—jp cdcral StJiation administration Supplemental ICgpe Certificate(Continuation £heet) SA5364SW-D Limitations and Conditions (con''t)

2. Also eligible on the above listed Models when equipped with Approved Turbocharged Engines (250 H.P.) and/or Wing Tip Tanks per STC SA148QWE.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89544, dated 12-20-84 is required and/or later FAA Approved revisions of the above supplement.

4. Compatabil ity of this modification with other previously approved modifications must be determined by the installer.

/.''•'•/'.'"'i ';/ this certify ate is punishable by a fine of nnt exceeding Si,000, or imprisonment not A.-, f ORM aiio-2-1 (10-69) 7/,,5 certificatt may he transferred ir. acc-'.i.ince it-ills 1M1 -7 I•' 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, Slate, and !JP 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):

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