STC SA3011SW-D

Supplemental type certificate · Century Flight Systems Inc

Holder
Century Flight Systems Inc · United States
Status
Current · Reissued
Status date
August 1, 1984
Applied
July 19, 1974
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA3SO

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Mitchell automatic flight system model AK488 consisting of a Piper altimatic IIIC Autopilot with optional command/automatic electronic pitch trim system, radio coupler and glide slope coupler.

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA30115W-D This certificate issued to: Century Flight Systems, Inc.

F.M. 1195 P. O. Box 610 Mineral Wells, TX 76067 Purt 3 of the CIVII Air Regulations.

Original Product -Type Certificate Numben: A3SO Make: Piper Model: PA-32-260, PA-32-300 and PA-32S-300 Description of Type Design Change:

Installation of Mitchell Automatic Flight System Model AK488 consisting of a Piper Altimatic IIIC Autopilot with Optional Command/Automatic Electronic Pitch Trim System, Radio Coupler and Glide Slope Coupler according to Drawing No. 69El101, Revision H, dated 8-15-78 and Master Drawing List No. 87A731, Revision 1, dated 8-15-78 (14 Volt System) and/or later FAA Approved Revisions of the above data.

Limitations and Conditions: Ellgible only on Piper Model PA-32-300, S/N 32-7940000 and Berore. Eligible only on Piper Model PA-32S-300, S/N 32-7940000 and Before (Landplane Configuration Only). FAA/DAS Approved Airplane Flight Manual Supplement, P/N 68S185-2, dated 11-7-77 is required for Piper Models PA-32-260, S/N 32-7600024 and below, PA-32-300, S/N 32-7640130 and below and PA-32S-300, S/N 32S-7140045 and below (Landplane Configuration Only) See Continuation Sheet, Page 2, a part of this STC vendered, suspended, revoked, or a termination dale is shervise es labdished by the Adri nis trater f the Federal Aviation Administration .

Date of Application: 7-19-74 Jule wissued: 3-31-75; 8-8-75; 12-6-76; 5-18-77;

11-7-77; 8-28-78; 8-1-84, Date of Issuance: 7-24-74 Date Amended: Revision 7

FEDERAL AVIATION -Don P. Watson (Signature ) OMINISTRA Manager, Aircraft Certification Division Southwest Region (Title)

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA30115W-D, Revision 7, dated 8-1-84 Limitations and Conditions:

FAA/DAS Approved Pilot's Operating Handbook Supplement, P/N 68S477-1, dated 11-7-77 is required for Piper Model PA-32-250, S/N 32-7700001 and Up FAA/DAS Approved Pilot's Operating Handbook Supplement, P/N 68S478-2, dated 8-28-78 is required for Piper Model PA-32-300, S/N 32-7740001 through S/N 32-7940000 and/or later FAA Approved Revisions of the above Supplements A Placard stating "Conduct trim check prior to flight (See AFM)" is required for owners with Airplane Flight Manuals.

A Placard stating "Conduct trim check prior to flight (See POH)" is required for owners with Pilot's Operating Handbooks.

FAA FORM 8110-2-1 (10-69) 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 ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP 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-32-260A3SO
Piper Aircraft Inc.PA-32-300A3SO
Piper Aircraft Inc.PA-32S-300A3SO