STC SA3673WE

Supplemental type certificate · Global Aerospace Technology Corporation

Holder
Global Aerospace Technology Corporation · United States
Status
Current · Reissued
Status date
January 20, 2009
Applied
April 10, 1978
Product
Aircraft · Large Airplane
Certification basis
Part 21
Data sheet
TCDSA3WE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

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.

What the certificate saysOCR

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.

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
The Boeing Company727-100C SeriesA3WE
The Boeing Company727-200 SeriesA3WE