# STC SA3673WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Global Aerospace Technology Corporation, United States
- Description: Installation of cargo restraint system which meets the requirements of a NAS 3610 Class IIA restraint system in a Boeing 727-22C, -100C and -200 series airplane.
- Applied: April 10, 1978
- Status date: January 20, 2009
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/b8/5d/b85d2c7d2f3199bda0dbfe6004cca39edc7f5c5661967ca2b2744ba58359de40
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/04F56AFBF02CA9BB86257A07004B84DA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3673WE

## ADs that name it (0)

None.

## Approved models (2)

- The Boeing Company 727-100C Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE))
- The Boeing Company 727-200 Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA3673WE This certificate issued to: Global Aerospace Technology Corporation 9200 Deering Avenue Chatsworth, California 91311 Tart 4b* of the Civil Air Poegulation. *(Certification basis is set forth in Type Certificate Data Sheet AWE).

Original Product Type Certificate Number : A3WE Молебск : The Boeing Company Model: 727-22C, -100C, -200 (and models listed on PEMCO Engineers Index List Number PB-727) Description of Type Design Change:

Installation of a cargo restraint system which meets the requirements of a NAS 3610 Class ILA restraint system in a Boeing 727-22C, -100C and -200 series airplane in accordance with FAA approved PEMCO Engineers Master Drawing List 70045, Revision G, dated May 14, 1993, or later FAA approved revision or PEMCO Engineers Index List Number PB-727, Revision A, dated June 5, 1997, or later FAA approved revision.

Limitations and Conditions: The approval of this modification applies to the above noted airplane model series only. This approval should not be extended to other specific airplanes of this model series on which other approved modifications are incorporated, unless it is determined 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. This determination should include consideration of changes in weight distribution, such as an increase in the fixed disposable weight in the fuselage. 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: APTil 10, 1978 Bute reinted: October 15, 1997;

Date of Issuance: June 21, 1978 January 20, 2009 Date Amended: June 8, 1983; July 2, 1993;

FEDERAL AVIATION October 16, 1997 By Direction of the Administrator TOMINSTRATO (Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office

47.

## Every issue (1)

- January 20, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b8/5d/b85d2c7d2f3199bda0dbfe6004cca39edc7f5c5661967ca2b2744ba58359de40)

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