# STC SA1777CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of KAP 150 two-axis or KFC 150 two-axis flight control system with optional third (yaw) axis and optional KAP 297B Vertical Speed and Altitude Selector.
- Applied: August 8, 1983
- Status date: April 9, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE)
- Certificate PDF: https://openairdocs.org/files/sha256/f2/62/f26227186c36300884c77f482d816d68db9073838225f60859878a45fe273d20
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7FD1B7EA83F255F98625860D004C9885.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1777CE-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 (1)

- Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))

## 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 2 FAA Form 8110-2 (5/14)

Number: SA1777CE-D This certificate issued to: Honeywell International Inc.

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

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

A17WE PA-60-700P

Install KAP150 two axis or KFC150 two axis Flight Control System with optional third (yaw) axisand optional KAP297B Vertical Speed and Altitude Selector.

REQUIRED DATA: 1. King Master Drawing List 155-9292-00dated 8-8-83 for field installations or 2. King Master Drawing List 155-9292-01Rev. 3 dated 10-18-83for factory installations, or later FAA approved revisionsto 1 or 2.

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: 8-8-83 Date Reissued: 2-28-95; 2-28-00; 4-9-20

Date of Issuance: 10-24-83 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 2 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- April 9, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f2/62/f26227186c36300884c77f482d816d68db9073838225f60859878a45fe273d20)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ef/09/ef09a432d58ba4a02a3d98a25d6a97b2f76ee4f624223a3a3b3251e51f445c4d)

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