# STC SA3424WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Telair International LLC, United States
- Description: Installation of Transequip, Inc. BMA Main Deck Baggage Container, P/N 302928
- Applied: March 28, 1977
- Status date: July 27, 2015
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE)
- Certificate PDF: https://openairdocs.org/files/sha256/08/17/08178fdb06a40ab307d912e0c52e93b589650c88eec8f02a29b379b92fd2ba36
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0B6CEA69EBAE559C86257E9D006417C4.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3424WE

## ADs that name it (0)

None.

## Approved models (2)

- The Boeing Company 747-100 Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))
- The Boeing Company 747-200B Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))

## 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.

This Certificate issued to Telair International, LLC 2220 E. Cerritos Avenue Anaheim, California 92806

Part 25 of the Federal Aviation Regulations Original Product Type Certificate Number :

A20WE Boeing 747-100 and 200B

Description of Type Design Change: Installation of Transequip, Inc. BMA Main Deck Baggage Container, P/N 302928 in accordance with FAA Approved Transequip Drawing List No. 303085, Issue I, or later FAA approved revision.

Limitations and Conditions: The approval of this change in type design applies to the above aircraft models when equipped with a Main Deck Handling System as reflected in Master Change 40353 (series).

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any other of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant change in weight distribution such as an increase in the fixed disposable weight of 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 permission.

Date of application : March 28, 1977

Date of issuance : June 9, 1977

Date reissued : September 12, 1991; June 28, 2000;

November 2, 2000; January 10, 2012; May 12, 2015: July 27, 2015

(Signature) Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

## Every issue (4)

- July 27, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/08/17/08178fdb06a40ab307d912e0c52e93b589650c88eec8f02a29b379b92fd2ba36)
- May 12, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ed/96/ed96e5f0b3ca3c9f49bb9a7f9c5c0098c0d271f52ce0e18cc0f1fa33070472e7)
- January 10, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/cd/92/cd92ce422be5af275ac85a3b3ecf0a4cccd90300b827b7a83d0ba62a9eeb082b)
- November 2, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/00/bf/00bfdae2555ded1ebdd5989966946e2fa404913ae39f53930ded9c5fbf44fd21)

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