# STC SA1529CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of King KAS 297 altitude selector option
- Applied: February 15, 1980
- Status date: March 20, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS A20SO](https://openairdocs.org/tcds/A20SO)
- Certificate PDF: https://openairdocs.org/files/sha256/55/fe/55fe3a7dc7b72fa79095d34f934e8c0f28b9c875e0ff5bdd7141af0e43b3ea8e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/63B04588934945978625861C00464261.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1529CE-D

## ADs that name it (0)

None.

## Approved models (3)

- Piper Aircraft Inc. PA-31 ([TCDS A20SO](https://openairdocs.org/tcds/A20SO))
- Piper Aircraft Inc. PA-31-325 ([TCDS A20SO](https://openairdocs.org/tcds/A20SO))
- Piper Aircraft Inc. PA-31-350 ([TCDS A20SO](https://openairdocs.org/tcds/A20SO))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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: SA1529CE-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:

A8EA PA 31, S/N 31-712and up; PA 31-325and PA 31-350

Installation of King Model KAS297 Altitude Selector Option in airplanesequipped with the KFC200 Flight Control System with Flight Director.

REQUIRED DATA: 1. King Master Drawing List 155-9161-00, Rev. 0 dated 2-15-80and 2. Airplane Flight Manual Supplement 006-0309-03, Rev. 0, dated 2-19-80or later FAA approved revision to 1 or 2.

This airplane must have the KFC200 Flight Control System with Flight Director installed in accordance with STC SA1166CE. 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.

Date of Application: 2-15-80 Date Reissued: 2-28-95, 2-28-00, 3-20-20

Date of Issuance: 2-19-80 Date Amended:

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: SA1529CE-D

Limitationsand Conditions: (continued) 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.

------------------------------------------------------------------------------------END--------------------------------------------------------------------------------

## Every issue (2)

- March 20, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/55/fe/55fe3a7dc7b72fa79095d34f934e8c0f28b9c875e0ff5bdd7141af0e43b3ea8e)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/80/f6/80f6ae552e4b7c447af497ebe846ed9cabf611f454e7e4fb9ef0f77ed5f98c12)

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