# STC SA3074WE

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: J D Smith Air Export Inc, United States
- Description: Installation of 96 x 125 inch animal containers.
- Applied: April 25, 1975
- Status date: March 18, 2008
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 21, Part 21, Part 21, Part 21, Part 21
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE)
- Certificate PDF: https://openairdocs.org/files/sha256/ff/da/ffdac7bcc735a28980eb977e44bfd95fdc3fa6107133e3c98c8fe6f25634ee29
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155924860720230405211607.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3074WE

## 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 747-200C 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.

Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA301LUE Certificate

SURRENDERED This certificate issued to: J. Do Smith Air Export, INC.

on . 3-18-08 Part 25 of the Federal Aviation gulation 58 25 1 cod an a lot 2-350 the 9252-151 325-17, 25-18, 25-20 and Original Product -Type lertificate Number: AZOWE Make: Boeing Model: 147-200 and us serres 747-100 Series * Description of Type Design Change: Installation of 96x125 inch Animal Containers in accordance with FAA sealed CAE Master Dwg. List SMI-9011 and Loading Schedule SMT-→2=30 * 747-100 Series modified to the cargo configuration per Boeing Drawing

• 63B12053-1 and STC SA976CE-D.

Limitations and Conditions: The approval of this change in type design applies basically to the 747100, -200C and -200F Series only. 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 of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution Pich age increase in tiny fated verst this persora shall remainin fict until sur vendered, suspended, verked, on a termination date is otherwise established by the ildminist rates of the Federal Aviation Administration .

Late s$ applicatin: Apro 25g 1975 I'ule reissued:

Date of Issuance: Augo 6, 1975 Date Amended: Dec. 3, 1975; Nov. 30, 1977 FEDERAL AVIATIO By Direction of the Administrator ( Signatate ) OMINISTRATIDO Chief, Aircraft Engineering Division (Tille)

This certificate montres

## Every issue (1)

- March 18, 2008: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/ff/da/ffdac7bcc735a28980eb977e44bfd95fdc3fa6107133e3c98c8fe6f25634ee29)

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