# STC SA2330CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Bendix/King KNS 660 Multi-Sensor Flight Management System with ARINC 429 compatibility and ICAO identifiers.
- Applied: January 2, 1992
- Status date: April 1, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/98/26/982623c7ded10a5c10d569de337cbbe2791c0607a71369acef69d026e9f2237b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6CE465804AED3695862585DD0070DF4C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2330CE-D

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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 The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title 3 SA2330CE-D Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Federal Aviation Regulations.23 Installation of the Bendix/King KNS 660 Multi-Sensor Flight Management System with ARINC 429 compatibility and ICAO identifiers.

REQUIRED DATA: 1. Master Drawing List 155-09632-0000, Rev. 1, dated 1-13-92 and 2. Airplane Flight Manual Supplement 006-00816-0000, Rev. 0, dated 1-13-92 or later FAA approved revision to 1 or 2.

1. KNS 660 Pilot’s Guide No. 006-8407-00 or later revision is required.

2. This approval included and evaluation and finding of acceptance of the interface with the Bendix/King EFS 10 EFIS as modified herein.

(See continuation sheet) Richard B. Sleigh ODA Administrator, ODA-602216-NM Beech 300, 300LW 2-28-95; 2-28-00; 4-1-201-2-92 1-13-92 A24CE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

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

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

The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

FAA Form 8110-2 (5/14) Page 3 of 3 Limitations and Conditions: (continued)

3. 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 these 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.

------------------------------------------------------------------------------------END------------------------------------------------------------------------------------ SA2330CE-D

## Every issue (2)

- April 1, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/98/26/982623c7ded10a5c10d569de337cbbe2791c0607a71369acef69d026e9f2237b)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/26/a4/26a46933a58cc126d00adbf1bb92253ca4cebe70831d1f13d4ba55aea83bb354)

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