STC SA5353SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
November 28, 1984
Applied
October 17, 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 single axis automatic flight guidance system, Model ST-248.

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.

Hnitrd £tat« of amrrita Bepartment of transportation —federal atiiation administration Supplemental 'Cuje Certificate SA5353SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 nae i .' 4jf ^/Za LI VI I Air .'leMt 'a*n 1 A 1 0 PIPER PA-23-250 AND PA-E23-250 Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-248, according to Bulletin No. 348, dated 10-04-84 and Master Drawing List No. 92290, dated 10-04-84 and/or later FAA Approved revisions of the above data (14 Volt System).

Only eligible on Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-7554172.

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

Continuation Sheet, Page 2, a part of this STC), SSMrnArnjA .^i'^uSt *f*A 10-17-84 11-28-84 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title) _ i - ••— /

This Cfiif.f'ii' may bt trarufrrrtj in s^corJanet with FAR 21.47.

FAAFo«« 81 10-2(10-68)

tlnittd £tatu of amenta Bepartmcnt of transportation— ^federal a&iation administration Supplemental HTjipe Certificate(Continuation £heet) SA5353SW-D Limitations and Conditions (con't)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89537, dated 11-28-84 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.

1- . /.''•.' I'mn of this certificate is punishable by a Jint >]/ not excelling 31,000, or imprisiwwfr.! not exceeding 3 \e/ir>. nr b-'t>

• •: I ;.RM 8110-2-1 (10-69) This certificate ma) he l<•.:•:.SerreJ i's ^c.

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 and streetJ (City, State, and <7/> cade) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

US. 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