# STC SA2329CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Bendix/King 4-tube EFS-10 EFIS, dual Bendix/King KFC 400 automatic flight control systems, dual Bendix/King series III VHF COMM/NAV, dual Bendix/King RMS 555 radio management system, Bendix/King DFS 43A, DMS 44A, MST 67A mode S transponder , KRA 405 radar altimeter, Motorola ARC-164 UHF COMM, Bendix/King KRT-707 TACAN, RDS 82 VP radar, MLS 21 MLS, CAS 81A TCAS, KHF 950 HF, KNS 660 FMS with KLN 670 GPS.
- Applied: May 16, 1991
- Status date: February 28, 2000
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A18SW](https://openairdocs.org/tcds/A18SW)
- Certificate PDF: https://openairdocs.org/files/sha256/51/e7/51e773f7d8be316ce68d443001ce37ed4cbac509ff50b74be7196e6150d88b4d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C50F792396FB478D85256CC200015CB3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2329CE-D

## ADs that name it (0)

None.

## Approved models (2)

- M7 Aerospace LLC SA227-CC ([TCDS A18SW](https://openairdocs.org/tcds/A18SW))
- M7 Aerospace LLC SA227-DC (C-26B) ([TCDS A18SW](https://openairdocs.org/tcds/A18SW))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2329CE-D This certificate issued to: Honeywell International Inc.

23500 W. 105" Street Olathe, KS 66061 Part 23 of the Federal Aviation Regulations Original Product - Type Berlificate Number: A 18SW Make: Fairchild Aircraft, Inc.

Model: SA227-CC and SA227-DC (C-26B) Description of Type Design Change:

CONFIGURATION A: Installation of Bendix/King 4-tube EFS 10 EFIS, dual Bendix/King KFC 400 Automatic Flight Control Systems, dual Bendix/King Series III VHF COMM/NAV, dual Bendix/King RMS 555 Radio Management Systems, Bendix/King DFS 43A, Bendix/King DMS 44A, Bendix/King MST 67A Mode S Transponder, Bendix/King KRA 405 Radar Altimeter, Motorola ARC-164 UHF COMM, Bendix/King KRT 707 TACAN, Bendix/King RDS 82 VP Radar, Bendix/King MLS 21 MLS, Bendix/King CAS 81A TCAS, Bendix/King KHF 950 HF and Bendix/King KNS 660 FMS with KLN 670 GPS.

(Continued on Continuation Sheet) Limitations and Conditions:

1. A standby (third) attitude indicator must be installed and operational. (Applies to Configuration A

2. An emergency COMM control head must be installed and operational. (Applies to Configuration A only.)

(Continued on Continuation Sheet) 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.

Master Drawing List 155-09625-0000, Rev. B, dated 12-20-91.

2. Airplane Flight Manual Supplement for RMS 555, 006-00808-0000, Rev. 0, dated 12-26-91.

3. Airplane Flight Manual Supplement for MLS 21, 006-00809-0000, Rev. O, dated 12-26-91.

4. Airplane Flight Manual Supplement for CAS 81A, 006-00810-0000, Rev. O, dated 12-26-91.

5. Airplane Flight Manual Supplement for EFS 10, 006-00811-0000, Rev. 0, dated 12-26-91.

6. Airplane Flight Manual Supplement for KNS 660, 006-0812-0000, Rev. O, dated 12-26-91.

7. Airplane Flight Manual Supplement for KFC 400, 006-00813-0000, Rev. 0, dated 12-26-91.

Later FAA approved revisions to number 1, 2, 3, 4, 5, 6, or 7 are incorporated and approved herein without further revision to this document.

CONFIGURATION B:

Installation of a single Bendix/King KFC 400 Automatic Flight Control System with Electromechanical Flight Instruments.

DATA REQUIRED, CONFIGURATION B:

1. Master Drawing List 159-08131-0001, Rev. 0, dated 7-18-94

2. Airplane Flight Manual Supplement 006-00813-0001, Rev. 0, dated 8-24-94.

Later FAA approved revisions to 1 or 2 are incorporated without further revision to this Supplemental Type Certificate.

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. (Applies to Configurations A and B.)

## Every issue (1)

- February 28, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/51/e7/51e773f7d8be316ce68d443001ce37ed4cbac509ff50b74be7196e6150d88b4d)

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