# STC SA1791CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Install KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis flight control system with optional KAP 297B vertical speed and altitude selector.
- Applied: October 24, 1984
- Status date: March 27, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A31EU](https://openairdocs.org/tcds/A31EU)
- Certificate PDF: https://openairdocs.org/files/sha256/21/5d/215d35189a0bbb88492998539d77708190cc2997aa5aee1fe684266b7a0bec40
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0C3DE035EBA92ADA8625861700518EBD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1791CE-D

## ADs that name it (1)

- [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986. Cited in the text

## Approved models (2)

- Partenavia Costruzioni Aeronauticas S.p.A. P68C ([TCDS A31EU](https://openairdocs.org/tcds/A31EU))
- Partenavia Costruzioni Aeronauticas S.p.A. P68C-TC ([TCDS A31EU](https://openairdocs.org/tcds/A31EU))

## 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.

FAA Form 8110-2 (5/14) Page 1 of 2 Number: SA1791CE-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 21.29 & 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Partenavia A31EU Model: P 68C. P68C-TC Description of Type Design Change:

Install KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis Flight Control System with optional KAS 297B Vertical Speed and Altitude Selector.

REQUIRED DATA: King Master Drawing List 155-9322-00 dated 10-29-84 or later FAA approved revision.

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: 10-24-84 Date Reissued: 2-28-95; 2-28-00; 3-27-20 Date of Issuance: 2-7-85 Date Amended:

By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

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

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

## Every issue (2)

- March 27, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/21/5d/215d35189a0bbb88492998539d77708190cc2997aa5aee1fe684266b7a0bec40)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c3/24/c324152eb57ed2fa2c747847ad90f8a23c4d36937655c0d925df5f73e91b2790)

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