# STC SA2972WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Braniff International, United States
- Description: Modification of lower deck aft cargo compartment restraint system to accommodate NAS 3610 Size A aircraft unit load devices. (747-127)
- Applied: November 22, 1974
- Status date: December 27, 1974
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE)
- Certificate PDF: https://openairdocs.org/files/sha256/05/a9/05a9ac8606b52cbfa56361f0918d82c97b5f06761f4f455c4c74d0016c182ed7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9F5C1C8354F8334385256CC20008CB59.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2972WE

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 747 ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))

## 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 / 10 Supplemental Type Certificate Number: SA2972WE This certificate issued to: Braniff International Punt 25 of the Federal Aviation Regulations. (See I.C. Data Sheet AZOW) Original Product -TypeCertificate Number: A2OWE Make: Boeing Model: 747-127 Description of Type Design Change: Modification of the Boeing 747-127 airplane lower deck aft cargo compartment restraint system to accommodate NAS 3610 Size A aircraft unit load devices in accordance with FAA sealed United Air Lines Drawing List COA &-166!

Limitations and Conditions: The approval of this change in type design applies basically to the Boeing 747-127 airplane only. aircraft of this model on which other previously approved modifications are incorpo- This approval should not be extended to other rated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce include consideration of significant changes in weight distribution such as an increas no adverse effect upon the airworthiness of that aircraft. This determination should in the fixed disposable weight in the fuselage.

Date of Application: NOV. 22, 1974 Date Reissued:

Date of Issuance: December 27, 1974 Date Amended:

EDERAL AVIATION By directions/ the SAdministra ( Signatur

**TAMINISTRAIO**

47.

## Every issue (1)

- December 27, 1974: Issued, Current. [certificate](https://openairdocs.org/files/sha256/05/a9/05a9ac8606b52cbfa56361f0918d82c97b5f06761f4f455c4c74d0016c182ed7)

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