# STC SA2310CE-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.
- Applied: April 15, 1988
- Status date: March 27, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/ec/9c/ec9c2963fda172f16fcf734b29059d1846debaf99e13172a69eade5990664a20
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/25BA564E5963DFA3862585CF0046C4B9.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2310CE-D

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 200CT ([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.

FAA Form 8110-2 (5/14) Page 1 of 2 Number: SA2310CE-D This certificate issued to: Honeywell International Inc.

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

Original Product – Type Certificate Number: Make: Beech A24CE Model: A200, A200CT Description of Type Design Change:

Installation of Bendix/King KNS 660 Multi-Sensor Flight Management System.

REQUIRED DATA: 1. Bendix/King Master Drawing List 155-9510-00, dated 4-14-88 and 2. Airplane Flight Manual Supplement 006-0485-00 dated 5-25-88 or later FAA approved revision to 1 or 2.

KNS 660 Pilot’s Guide No. 006-8407-00 dated 12-2-85 or later revision is required. The installation in the Model A200CT is limited to Serial Numbers BP-1 thru BP-45. 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: 4-15-88 Date Reissued: 2-28-95; 2-28-00; 3-27-20 Date of Issuance: 5-25-88 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/ec/9c/ec9c2963fda172f16fcf734b29059d1846debaf99e13172a69eade5990664a20)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/25/ce/25ce0c7584109bf3ca289d4771eea455037b45de23519c7e02ee3348ea948f00)

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