# STC ST00278LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Requirements for the installation of the Honeywell FMZ-2000 FMS and the HG2021 12 Channel GPS.
- Applied: June 6, 1995
- Status date: March 20, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE)
- Certificate PDF: https://openairdocs.org/files/sha256/ef/d4/efd48a20ff5a5bdc2db6a706c8d24521d21575d8a27919a664088cf2bf1eb4b8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/560112DD1F06B6AD86258615006F85BD.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST00278LA

## ADs that name it (0)

None.

## Approved models (1)

- Textron Aviation Inc. 560 ([TCDS A22CE](https://openairdocs.org/tcds/A22CE))

## 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 2 FAA Form 8110-2 (5/14)

Number: ST00278LA This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 25 of the Federal Aviation Regulations Original Product – Type Certificate Number: Make: Cessna Aircraft Company Model: 560 A22CE

Requirements for the installation of Honeywell FMZ-2000 Flight Management System (FMS) and the HG2021 12 Channel Positioning System (GPS), are contained in the Honeywell Master Data List No. 1050-0818, Rev. "C" dated October 3, 1996, or later FAA Approved revision. To determine which configurations of the FMS/GPS installation have been approved, including the required FAA Approved Airplane Flight Manual supplement, if applicable, refer to the appropriate appendixes in the FAA Approved Honeywell Master Data List.

This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configurations will not introduce any adverse effect upon the airworthiness of the aircraft. A copy of this STC must be included in the permanent record of the modified aircraft. 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: June 6, 1995 Date Reissued: February 27, 2009; March 20, 2020

Date of Issuance: November 26, 1996 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 2 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- March 20, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ef/d4/efd48a20ff5a5bdc2db6a706c8d24521d21575d8a27919a664088cf2bf1eb4b8)
- February 27, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/94/7d/947d7ea64adf17c88cc9ace360c1068f029e52c618b85abef80e8e7a79151cda)

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