# STC SA5515NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Requirements for the installation of Honeywell Standard windshear systems.
- Applied: February 11, 1991
- Status date: April 20, 2020
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE)
- Certificate PDF: https://openairdocs.org/files/sha256/e3/c2/e3c21f8ba59ac5a760a2aca6a6932a66a52f88930b8ad6d0da0f6ab1015c27cc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EBEB38132ADE96E98625861C0063EE19.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5515NM

## ADs that name it (0)

None.

## Approved models (5)

- The Boeing Company 747-100 Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))
- The Boeing Company 747-200B Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))
- The Boeing Company 747-200C Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))
- The Boeing Company 747-200F Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))
- The Boeing Company 747-300 Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))

## 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: SA5515NM 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 A20WE Model: 747-100, -200, -200F, -300 Description of Type Design Change:

Requirements for the installation of Honeywell Standard Windshear System are contained in Honeywell Master Data List Number ML4076176, Revision "-", or later FAA approved revisions. 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 FAA Approved 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 configuration will not introduce any 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: February 11, 1991 Date Reissued: January 15,2009; April 20, 2020 Date of Issuance: December 20, 1991 Date Amended: November 28, 1995 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 (2)

- April 20, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e3/c2/e3c21f8ba59ac5a760a2aca6a6932a66a52f88930b8ad6d0da0f6ab1015c27cc)
- January 15, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/7e/10/7e10c78c2bf7efea70f22dad7a3544361cc7649b46191f743845e4b7767eb814)

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