STC SA1567CE-D

Supplemental type certificate · Honeywell International Inc

Holder
Honeywell International Inc · United States
Status
Current · Reissued
Status date
May 30, 2020
Applied
March 8, 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.

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA1567CE-D This certificate issued to: Honeywell International Inc.

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

Original Product – Type Certificate Number: Make: Piper A3SO Model: PA-32-301, PA-32-301T Description of Type Design Change:

Install 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.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of 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: 3-8-82 Date Reissued: 2-28-95; 2-28-00, 3-30-20 Date of Issuance: 6-8-82 Date Amended: 4-27-84; 5-24-85 By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1567CE-D

FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change: (continued) REQUIRED DATA:

KAP 100 Single Axis Flight Control System la. Master Drawing List 155-9209-00, Rev. 1, dated 4-30-82 for Field Installation.

lb. Master Drawing List 155-9209-01, Rev. 1, dated 4-30-82 for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0406-00, dated 6-8-82.

KAP 150 and KFC 150 Two Axis Flight Control System la. Master Drawing List 155-9209-00, Rev. 1, dated 4-30-82 for Field Installation.

1b. Master Drawing List 155-9209-01, Rev. 1, dated 4-30-82 for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0406-01, dared 6-8-82.

Optional KAS 297B Vertical Speed and Altitude Selector 1a. Master Drawing List 155-9209-00, Rev. 4, dated 4-27-84 for Field Installation.

1b. Master Drawing List 155-9209-01, Rev. 3, dated 5-21 -85 for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0406-02, dated 4-27-84.

Later FAA approved revisions to 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 · 2

MakeModelData sheet
The New Piper Aircraft Inc.PA-32-301A3SO
The New Piper Aircraft Inc.PA-32-301TA3SO

Every issue · 2

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

DateStatusFiles
May 30, 2020Reissued, currentCertificate
February 28, 2000Reissued, earlier issueCertificate