# STC SA1187CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc
- Description: Installation of King Model KCS 55A pictorial navigation (compass) system with optional KA 52 autopilot adapter.
- Status date: March 31, 2020
- Data sheets: A20SO, A20SO, A20SO, A20SO, A8EA
- Certificate PDF: https://openairdocs.org/files/sha256/5b/af/5baf9f9036e176836bb9232c7da950ccb59370ec0faf6a7e4dc9bc4166991bea
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/064189DE6FF29F118625861C007B4CDA.0001
- Page: https://openairdocs.org/stc/SA1187CE

## ADs that name it

None.

## Approved models (5)

- The New Piper Aircraft Inc. PA-31 (TCDS A20SO)
- The New Piper Aircraft Inc. PA-31-300 (TCDS A20SO)
- The New Piper Aircraft Inc. PA-31-325 (TCDS A20SO)
- The New Piper Aircraft Inc. PA-31-350 (TCDS A20SO)
- The New Piper Aircraft Inc. PA-31P (TCDS A8EA)

## 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: SA1187CE 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, PA 31P, PA 31-300, PA 31-325and PA 31-350

Installation of King Model KCS55A Pictorial Navigation (Compass) System, with optional KA 52 autopilot adapter, in accordance with King Drawings 155-9021-00, sheets 1 through 7, revision 3 of 5-16-74with ECONo. 12845and 155-9047-00/01, sheets 1 through 13, revision 3 of 12-8-75or later approved revisions.

The installation data approved under this STCcovering the optional autopilot adapter islimited to coupling with the Mitchell Century II and Century III autopilotsand the Piper Altimatic III Cautopilot using both the Mithcell 1C-388-3radio coupler and the King KA 52 Adapter.

NOTE: Piper Altimatic II autopilot or any other "RFsensing design" autopilot system is not approved.

Date of Application: 12-10-75 Date Reissued: 1-31-95; 2-28-00; 3-31-20

Date of Issuance: 1-5-76 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: SA1187CE

Limitationsand Conditions: (continued) 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.

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

## Every issue (2)

- March 31, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5b/af/5baf9f9036e176836bb9232c7da950ccb59370ec0faf6a7e4dc9bc4166991bea)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/61/3d/613d4b116fd5f4171df12a526771d2803d6c6affc39dcc3c435b92b6bb70159e)

---
From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.