# STC SA2895WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Hermes Enterprises, United States
- Description: Installation of Hermes LD-3 Koolflite refrigerated cargo container.
- Applied: May 31, 1974
- Status date: June 12, 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/sha256/95/87/95877089b066f55a880c9843a80d33443f1dfefbc22637fed023c6096b01cb82
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F76815FD774489A185256CC20008CA6E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2895WE

## ADs that name it (0)

None.

## Approved models (4)

- 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))
- 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: SA2895WTB This certificate issued to: Hermes Enterprises Purt 25 of the Federal Aviation Regulaions. (See I.C. Data Sheet AZOWE) Original Product -Iype bertificate Number: AZOWE Make: Boeing Model: 747-100, -200B, -200C and -200F Description of Type Design Change: Installation of Hermes ID-3 Koolfite refrigerated requirements for ISO C90/NAS-3610, Revision No. 2, 2K1C cargo unit load devices. Part No. 3000-1. cargo container in accordance with FAA sealed Hermes Drawing List for container This container has met the minimum performance design and test Limitations and Conditions: Maximum gross 10ad 2830 1bs. type design applies basically to the Boeing 747-100, -200B, -200C and -200F airplanes The approval of this change in 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 hensusel weight distribution such as an increase in the fixed disposable weight in icate and the supporting dalu which is the basis for appr vat shall remain in effect until surrendered, suspended, revcked, or a termination date is therwise established by the Administratur of the Federal Aviation Administration .

Date of Application: MAY 31, 1974 Date Reissued:

Late ef issueance: JUN 12 1974 Date Amended:

EDERAL AVIATION By directin dminiatra cas (Signature )

TOMINISTRAIO Chief, Aircraft Engineering Division (Title)

## Every issue (1)

- June 12, 1974: Issued, Current. [certificate](https://openairdocs.org/files/sha256/95/87/95877089b066f55a880c9843a80d33443f1dfefbc22637fed023c6096b01cb82)

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