STC SA3065SW-D

Supplemental type certificate · Century Flight Systems Inc

Holder
Century Flight Systems Inc · United States
Status
Current · Reissued
Status date
August 16, 1984
Applied
July 2, 1975
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS2A13

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

What it approves

Installation of Mitchell automatic flight system AK431 consisting of a Piper autocontrol IIIB autopilot with optional radio couplers

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.

I SStata of arnica department of transportation—Jpederal dotation administration Supplemental Itujc Certificate SA3Q65SW-D '^Century Flight Systems, Inc.

F.M. 1195 P.O. Box 610 Mineral Wells, TX 76067 /J^J/u/fetteu'tnja'JvrwaufJM'iJSi ^n&^rnj^a/t^TiAjzndf&ncuA&nA 3 jd^Ae> Civil Air <sle*aMia&f>nA.

Cktai-nsil\JvctUAet——<-Jy/i»~&e>i&fi<M£e>iSli*rn0e*-: 2A13ts y* ' Piper PA-28-151, PA-28-161, PA-28-181, PA-28-236, PA-28-2Q1T Installation of Mitchell Automatic Flight System Model AK431 consisting of a Piper AutoControl IIIB Autopilot with Optional Radio Couplers according to Bulletin No. 553, Revision 10, dated 1-11^79 and Master Drawing List No, 87A668, Revision K, dated 1-11-79 (14 Volt System) and/or later FAA Approved Revisions of the above data.

FAA/DAS Approved Airplane Flight Manual Supplement, p/N 68S176-2, dated 11-26-76 is required for Piper Models PA-28-151, S/N 28-7615435 and below, FAA/DAS Approved Pilotfs Operating Handbook Supplement, P/N 68S445, dated 11-21-76 is required for Piper Model PA-28-161.

^ .,,_.,,., ^ ,.., ^ ^ * See Continuation Sheet, Page 2. a part of this STCCompatibility of this modification with, otner previously approved modifications must be determined by the installer.

,4Z^^ 11-26-76; 12-22-76; 6-16-78; 7-27-78;

12-19-78; 1-18-79; 8-16-84, Revision 7 P. Watson Manager* Aircraft Certification Division (TitU)

This crrtifieatt may kt trtaifemd in mcatduu* with FAR 21.47.

FAA Fo*M«110-2 (10-««)

jStuu of 3*uta Bcpartmtnt of ^transportation— tftdcral awation administration Supplemental t^pe Certificate(Continuation £hcet) SA3065SW-D, Revision 7, dated 8-16-84 Limitations and Conditions (Cont'd) FAA/DAS Approved Pilot's Operating Handbook Supplement, P/N 68S453, dated 11-26-76 is required for Piper Model PA-28-181, S/N 28-7690001 and Up.

FAA/DAS Approved Pilot's Operating Handbook Supplement, P/N 68S452, dated 11-26-76 is required for Piper Model PA-28-151, S/N 28-7715001 and Up.

FAA/DAS Approved Airplane Flight Manual Supplement, P/N 68S720, dated 6-16-78 is required for Piper Model PA-28-236, FAA/DAS Approved Airplane Flight Manual Supplement, P/N 68S800, dated 12-19-78 is required for Piper Model PA-28-201T aircraft with an Airplane Flight Manual.

Pilot's Operating Handbook and FAA/DAS Approved Airplane Manual Supplement, P/N 68S814, dated 1-18-79 is required for Piper Model PA-28-201T aircraft with a Pilot's Operating Handbook and/or later FAA Approved revisions of the above supplements.

FAA FORM at 10-2-1 (1O40) Thu cirtificati may bt transjtrrid in accordance with FAR 21.47.

CNSTRUCT.ONS: The Tan*, endorsement below may be used u, notify the appropriate FAA lu*H-I Office of the traiufer of thU Supplemenul Type Certificate.

The FAA will rei»ue the certificate in the name of the transferee and forward i, to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemenul Type Certificate Number to (Name of transferee')—— (Address of transferee).

from (Name of grantor) (Print or type).

(Address of grantor) 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 · 5

MakeModelData sheet
Piper Aircraft Inc.PA-28-1512A13
Piper Aircraft Inc.PA-28-1612A13
Piper Aircraft Inc.PA-28-1812A13
Piper Aircraft Inc.PA-28-201T2A13
Piper Aircraft Inc.PA-28-2362A13