STC SA4317SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
June 17, 1982
Applied
March 5, 1981
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS1A15

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC system 60 two axis automatic flight guidance system, Model ST-021 with optional autotrim 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.

lirotcd grates of arnica Bepartmcnt of tonsportation—federal 2toiation administration Supplemental ICgpe Certificate SA4317SW S-TEC Corporation Rt. 4, Bldg, 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ^&^yfy^wde&A<p#t'f<^^<n^ft>tCc>u>vn^Jwwctu^Mfi& ^-*y^*^&«£X«7«<>^xm<5<f^-<$i^<z«»w«>»'^i«^^ 3 j^J&e' Civil Air <Sleat&iadu>nA/.

~ " 1A15 Piper See Limitations and Conditions Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-021, with Optional Autotrim System according to Bulletin No. 124, Revision 5, dated 3-12-82 and Master Drawing List No. 9239, Revision E, dated 3-12-82 with Optional Flight Director Steering Horizon; or according to later FAA approved revision. (14 Volt System) See Continuation Sheet, page 2, of this STC.

: March 5, 1981 !3L&****u~t '.• 1/8/82; 6/17/82 Revision 2 March 26, 1981 on P. Watson Manager, Aircraft Certification Division (TitU)

This certificate may bt transferred in accordance with FAR 21.47.

FAA FotM 8110-2 (10-48)

flitted £tatu of amtrira Bcpartment of transportation— federal aoiation administration Supplemental t^pe Certificate(Continuation £heet) SA4317SW Revision 2 Limitations and Conditions:

1. Eligible on Piper Models PA-24 (PA- 24- 180), PA- 24-250, and PA- 24-260, S/N 24-4803 and Below (Except S/N 24-4783) and the above models when modified by STC SA4-1351, or STC SA4-1235 as applicable (Wing Tip Tanks)

2. FAA Approved Airplane Flight Manual Supplement P/N 8943 dated Karch 26, 1981, is required for Piper Models PA-24 (PA-24-180) and PA-24-250, S/N 24-2843 and Below; OR, Airplane Flight Manual Supplement P/N 8943-1 dated January 8, 1982, is required for Piper Models PA- 24- (PA- 24- 180), PA- 24-250 and PA- 24-260, S/N 24-4803 and Below (Except S/N 24-4783); OR, FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8943-2 dated 6-17-82, is required for Piper Models PA-24 (PA- 24-180), FA-24-250, PA- 24-260, S/N 24-4803 and Below (Except S/N 24-4783) and the above models when modified in accordance with STC SA4-1351 or STC SA4-1235 as applicable (Wing Tip Tanks) with S-TEC System 60 Two Axis Automatic Flight Guidance System (with 0105-R9Roll Servo) installed.

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

FAA FORM 8110-2-1 (io-69) 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, Stale, and gIP 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 · 3

MakeModelData sheet
Piper Aircraft Inc.PA-241A15
Piper Aircraft Inc.PA-24-2501A15
Piper Aircraft Inc.PA-24-2601A15