# STC SA3659NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: LMI Aerospace, United States
- Description: Installation of a windscreen/cabinet assembly.
- Applied: July 17, 1986
- Status date: November 28, 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/sha256/1c/0a/1c0ad3bff314c4e581dadc5d083e66a0d4c2f5684e12034908da31bbd2ee4261
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/51A4DAF049F83E4E862583580053D2A7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3659NM

## ADs that name it (0)

None.

## Approved models (1)

- 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 SA3659NM

This certificate, issued to LMI Aerospace 1910 Merrill Creek Parkway Everett, WA 98203

Part 25 of the Federal Aviation Regulations. (See Type Certification Data Sheet A16WE for complete certification basis.)

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

Description of the Type Design Change: Installation of Windscreen/Cabinet Assembly in accordance with FAA approved TRAMCO Top Drawing Number 86-115, Sheet 1, Revision D, dated November 21, 1986 or later FAA approved revisions.

Limitations and Conditions: Approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. The resulting interior arrangement, along with the required placarding has not been evaluated and is not part of this STC. A copy of this Certificate and FAA approved TRAMCO Drawing 86-115, Sheet 1, shall be maintained as part of the permanent records for 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: July 17, 1986 Date reissued: April 12, 2002; November 2, 2018;

November 28, 2018 Date of issuance: April 9, 1987 Date amended:

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

(Signature)

Manager, Seattle ACO Branch (Title)

## Every issue (3)

- November 28, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/1c/0a/1c0ad3bff314c4e581dadc5d083e66a0d4c2f5684e12034908da31bbd2ee4261)
- November 2, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ef/e2/efe206d6741fd8c09cb96981dd53506123cfd9fd85e94634d23003d4bb9126f2)
- April 12, 2002: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b5/2e/b52e75acf0b752986d582366bb513352a61a0f22afc21cfd51ff15a57ea545da)

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