# STC SA5458NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Honeywell Standard windshear systems.
- Applied: August 14, 1989
- Status date: March 20, 2020
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/e2/5e/e25efeae424b0b2da9aaadc19d5ff59bdf678557d6f2e75cd421656057fa30a4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F079B58792FC855E8625889A0063074B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5458NM

## ADs that name it (0)

None.

## Approved models (2)

- The Boeing Company 737-100 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-200 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.

FAA Form 8110-2 (5/14) Page 1 of 2 Number: SA5458NM This certificate issued to: Honeywell International Inc.

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

Original Product – Type Certificate Number: Make: Boeing A16WE Model: B737-100, -200 Description of Type Design Change:

Requirements for the installation of Honeywell Standard Windshear Systems are contained in Honeywell Master Data List Number ML4074983, Revision "A", 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 in the approved Master Data List Limitations and Conditions:

This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any of those other previously approved configuration will introduce no adverse effect upon the airworthiness of 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: Aug 14, 1989 Date Reissued: March 2, 2009; March 20, 2020 Date of Issuance: August 5,1991 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 (3)

- March 20, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e2/5e/e25efeae424b0b2da9aaadc19d5ff59bdf678557d6f2e75cd421656057fa30a4)
- April 20, 2020: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/e2/5e/e25efeae424b0b2da9aaadc19d5ff59bdf678557d6f2e75cd421656057fa30a4)
- March 2, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a2/5f/a25f6b86a64b26a1d1f4c97a02e31e4cb546a002ab83280395c10bc138620ee8)

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