# STC SA5735NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aviation Technical Services, United States
- Description: Installation of Provisions Only - Honeywell Windshear Computer(P/N 4061048-903).
- Applied: April 30, 1992
- Status date: October 24, 2018
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/26/17/26176d561e2d3fcfa562980fa616299de8857fbefde93fb277daf051e85861f7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/14F5CC4196F18FC786258335004C0875.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5735NM

## 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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SA5735NM

This certificate, issued to Aviation Technical Services 3121 109th Street SW Everett, WA 98204-3500

Part 25 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A16WE Make: Boeing Model: 737-100, -200

Description of the Type Design Change: Installation of Provisions Only – Honeywell Windshear Computer (P/N 4061048-903) per Tramco Top Drawing 92-108 Rev. “D”, dated 6/29/92, or later, FAA-approved version.

Limitations and Conditions: All AC & DC breakers installed shall be collared with stow clips. The a pproval of this change in type design applies to Boeing 737-200 airplanes and should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

Date of application: April 30, 1992 Date reissued: October 24, 2018 Date of issuance: July 2, 1992 Date amended: November 30, 1993

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Manager, Seattle ACO Branch (Title)

## Every issue (2)

- October 24, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/26/17/26176d561e2d3fcfa562980fa616299de8857fbefde93fb277daf051e85861f7)
- November 30, 1993: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/eb/db/ebdb7e529df071fad0b833bd035763c110357daf1bda25691f15670caa5d915d)

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