STC SA1572CE-D

Supplemental type certificate · Honeywell International Inc

Holder
Honeywell International Inc · United States
Status
Current · Reissued
Status date
March 25, 2020
Applied
September 17, 1982
Product
Aircraft · Small Airplane
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 KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis flight control system, and optional KAS 297B vertical speed and altitude selector.

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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SA1572CE-D This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 3 of the Civil Air Regulations.

Original Product – Type Certificate Number: Make: Piper Model:

A3SO PA-32R-301, PA32R-301T

Installation of KAP100 single axis, KAP150 two axis, or KFC150 two axis Flight Control System and optional KAS297B Vertical Speed and Altitude Selector.

(See Continuation Sheet for Required Data)

This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change and any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof that airplane.

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: 9-17-82 Date Reissued: 2-28-95, 2-28-00, 3-25-20

Date of Issuance: 11-1-82 Date Amended:

6-21-83, 4-19-84, 5-24-85

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

(Continuation Sheet) Number: SA1572CE-D

Description of Type Design Change: (continued) REQUIRED DATA:

KAP100 Single Axis Flight Control System 1a. Master Drawing List 155-9261-00, dated 10-8-82for Field Installation.

1b. Master Drawing List 155-9261-01, dated 6-21-83for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0414-00, dated 11-1-82.

KAP150 and KFC150 Two Axis Flight Control System 1a. Master Drawing List 155-9261-00, dated 10-8-82for Field Installation.

1b. Master Drawing List 155-9261-01, dated 6-21-83for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0414-01, dated 11-1-82.

Optional KAS297BVertical Speed and Altitude Selector 1a. Master Drawing List 155-9261-00, Rev. 2, dated 4-19-84for Field Installation.

1b. Master Drawing List 155-9261-01, Rev. 1, dated 5-21-85for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0414-02, dated 4-19-84.

Later FAA approved revisionsto above listed data are incorporated without further revision to the Supplemental Type Certificate.

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ADs that name this STC · 1

An AD can apply because an STC is installed, or mention one in its text.

Approved models · 3

MakeModelData sheet
The New Piper Aircraft Inc.PA-32R-301(HP)A3SO
The New Piper Aircraft Inc.PA-32R-301(SP)A3SO
The New Piper Aircraft Inc.PA-32R-301TA3SO

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
March 25, 2020Reissued, currentCertificate
February 28, 2000Reissued, earlier issueCertificate