# STC SA6083NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of standard windshear systems.
- Applied: January 14, 1993
- Status date: March 19, 2020
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/a9/1a/a91a0c110f6fef0d9c544c6178768894c18a3a3df58b243dd69d085ec11677fc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/045356C9F38C714086258629007B0DFC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA6083NM

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 737-300 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))

## 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: SA6083NM This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 25of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Boeing Model:

A16WE B737-300

Requirementsfor the installation of Honeywell Standard Windshear Systemsare contained in Honeywell Master Data List Number ML4077604, Revision “B”, dated November 17, 1993, or later FAA approved revision. To determine which configuration(s) of the Standard Windshear System have been approved, including the required FAA Approved Airplane Flight Manual supplement, if applicable, refer to appropriate appendixes on the approved Master Data List..

This installation should not be incorporated in any aircraft unlessit isdetermined that the interrelationship between this installation and any of those other previously approved configuration will introduce no adverse effect upon the airworthinessof the aircraft. Refer to the appropriate appendixes in the FAA Approved Master Data List for any other limitations. 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: January 14, 1993 Date Reissued: March 2, 2009, March 19, 2020

Date of Issuance: November 19, 1993 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 19, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a9/1a/a91a0c110f6fef0d9c544c6178768894c18a3a3df58b243dd69d085ec11677fc)
- March 2, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ac/4a/ac4a3d470f90de80b49589b9f8d20ac832bdde824bb0fe5e485f44d82c84f776)

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