# STC SA3953NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Bridport-Air Carrier Inc., United States
- Description: Installation of thru access buckles in barrier net assembly, Air Cargo Equipment Corporation p/n 43275-102.
- Applied: July 21, 1988
- Status date: June 14, 2001
- 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/d6/6b/d66bcb7eef23cbb69da4fea4e316adf758773de7d8c293fe78696040e6e29074
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DB9CE8A0FF12804D85256CC2000C5BFB.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3953NM

## ADs that name it (0)

None.

## Approved models (3)

- The Boeing Company 747-200B Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))
- The Boeing Company 747-200C Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))
- The Boeing Company 747-200F Series ([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 Supplemental Type Certificate Number: SA3953NM This certificate issued to: BRIDPORT-AIR CARRIER, INC.

22645 76" AVENUE SOUTH KENT, WASHINGTON 98032-1992 Certifies that the change in the type design for the following product with the limitations and conditins therefor as specified hereon meets the airvorthiness requirement's of Part 25 of the Federal Priation Regulations.

Original Product Type Berlificate Number: A20WE Abatte: BOEING Model: 747-200B, C, F Description of Type Design Change: Installation of through access buckles in Barrier Net Assembly, Air Cargo Equipment Corporation Part Number 43275-102, in accordance with FAA-sealed drawing no. MDL-1, Revision "N/C", dated September 13, 1988, or later FAA-approved revision.

Limitations and Conditions: . This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the 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.

July 21, 1988 Date Reissued: June 28, 2000, June 14, 2001 Date of Issuance: October 7, 1988 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Nubal U. Murph Signature) / Manager, Technical & Administrative Support TOMNISTRATIO Staff, Los Angeles Aircraft Certification Office (Title)

FAR Form 8110-2 (10-68) Page 1 of 2

## Every issue (1)

- June 14, 2001: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d6/6b/d66bcb7eef23cbb69da4fea4e316adf758773de7d8c293fe78696040e6e29074)

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