# STC SA2328CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of the Bendix/King KLN 88 Loran C system.
- Applied: January 2, 1991
- Status date: April 1, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A60EU](https://openairdocs.org/tcds/A60EU)
- Certificate PDF: https://openairdocs.org/files/sha256/50/fe/50fe029e23a3fa5add7c3705ae08552fcfea6440754ba4b9c87f8c2ba92f9f0a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6FC6DACC86EA992E862585DD0071C959.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2328CE-D

## ADs that name it (0)

None.

## Approved models (1)

- SOCATA - Groupe Aerospatiale TBM 700 ([TCDS A60EU](https://openairdocs.org/tcds/A60EU))

## 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 SA2328CE-D Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Federal Aviation Regulations.23 Installation of the Bendix/King KLN 88 LORAN C System.

REQUIRED DATA: 1. Master Drawing List 155-09621-0000, Rev. 0, dated 1-2-91 and 2. Airplane Flight Manual Supplement 006-00807-0000, Rev. 0, dated 1-21-91 or later FAA approved revision to 1 or 2.

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 previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

(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.

Richard B. Sleigh ODA Administrator, ODA-602216-NM Socata TBM 700 2-28-95; 2-28-00; 4-1-201-2-91 1-21-91 A60EU

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)

2. When the KLN 88 LORAN C is installed and intended for use as a primary navigation source, additional equipment required for each specific type of airplane operation must be installed and operable.

3. The KLN 88 LORAN C has been evaluated as a navigation input source for the KFC 325 Automatic Flight Control System and found to be compatible; the interface of these two systems is approved.

------------------------------------------------------------------------------------END------------------------------------------------------------------------------------ SA2328CE-D

## Every issue (2)

- April 1, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/50/fe/50fe029e23a3fa5add7c3705ae08552fcfea6440754ba4b9c87f8c2ba92f9f0a)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/8a/71/8a71fbb3f95938626f1cf5e6448917f32e1b0ad2fe61fce447ca158892ecd77d)

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