# STC SA103NW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aviation Technical Services, United States
- Description: Installation of modified lower interior sidewall.
- Applied: April 1, 1974
- Status date: October 24, 2018
- 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/sha256/4b/51/4b513d2e073c15f380ac580a8b396e21d4d4eb84f6b434d33d29288a30a10243
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/83BEB25D02E45C0986258335004B4055.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA103NW

## 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 SA103NW

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: 737-200

Description of the Type Design Change: Installation of modified lower interior sidewall in accordance with Drawing No. AR-010 to increase service life and maintaining appearance of the interior of the aircraft.

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 previousl y approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approve modifications will introduce no adverse effect on the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft.

Date of application: April 1, 1974 Date reissued: May 13, 1977; October 24, 2018 Date of issuance: April 12, 1974 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 (2)

- October 24, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4b/51/4b513d2e073c15f380ac580a8b396e21d4d4eb84f6b434d33d29288a30a10243)
- May 13, 1977: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/58/2f/582f0107dd20d4c8b14d9a4dea02dae2b6da7a4e5220ac0d212546b492750c70)

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