STC SA00864WI

Supplemental type certificate · Garmin International Inc

Holder
Garmin International Inc · United States
Status
Current · Amended
Status date
November 22, 2004
Applied
November 10, 1998
Product
Aircraft · Single-Engine
Certification basis
Part 3, 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 GNS 530 or GPS 500 for (1) Installation Data referenced on Sheet 2, and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Sheet 2.

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.

Olathe, KS 66062

Part 3 of the Civil Air Regulations.

Original Product--Type Certificate Number : A3S0 Make : Piper Model : PA-32

Description of Type Design Change: Installation of the Garmin GNS 530, 530A, or GPS 500 (GNC 500 Series TAWS Option) in accordance with the installation data and FAA Approved Airplane Flight Manual Supplements (AFMS) listed on the Continuation Sheet (See page 2 of 2).

Limitations and Conditions : Compatibility of this design change with previously approved modifications must be determined by the installer If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application : November 10, 1998

Date of issuance : March 21, 2000 Date reissued :

Date amended : April 13, 2001; July 25, 2002;

November 22, 2004

( Signature) Harvey E. Nero Program Manager Wichita Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

Number SA00864WI

Configuration 1

Installation Data A F M S

Installation of Garmin GNS 530 or GNS 530A in accordance with GARMIN Master Drawing List No.

005-C0097-00, Revision H, dated April 26, 2002, or later FAA approved revision.

FAA Approved Airplane Flight Manual Supplement for Piper PA32 with GARMIN GNS 530, Drawing No. 190-00181-03, Revision A, signed 04/04/00, or later FAA Approved revision.

Configuration 2

Installation Data A F M S

Installation of the GARMIN GPS 500 in accordance with Garmin Master Drawing List No. 005-C0097-00, Revision H, dated April 26, 2002, or later FAA approved revision FAA Approved Airplane Flight Manual Supplement for Piper PA32 with GARMIN GPS 500, Drawing No. 190-00181-63, Revision A, signed 03/15/01, or later FAA Approved revision.

Configuration 3

Installation Data A F M S

Installation of the GARMIN GNS 530, GNS 530A, or GPS 500 (GNC 500 Series TAWS Option) in accordance with Garmin Master Drawing List No.

005-C0097-00, Revision P, dated 11/17/2004, or later FAA approved revision.

FAA Approved Airplane Flight Manual Supplement for Piper PA32 with GARMIN GNS 530, Drawing No. 190-00181-03, Revision C, signed 11/19/2004, or later FAA approved revision.

Or

FAA Approved Airplane Flight Manual Supplement for Piper PA32 with GARMIN GPS 500, Drawing No. 190-00181-63, Revision B, signed 11/19/04, or later FAA approved revision.

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 · 1

MakeModelData sheet
The New Piper Aircraft Inc.PA-32-260A3SO