# STC SA8039NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States
- Description: Installation of Galley, G4A.
- Applied: July 18, 1994
- Status date: July 17, 2014
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/64/8f/648fc86605471e6eabfa9df547bf0f26efaced010408e8ddac638e63c9ea065c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/73A5FE917D21CA3B86257D50005BC3C7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA8039NM

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 727-200 Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE))

## 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 Driessen Aircraft Interior Systems, Inc.

DBA: Zodiac Galleys USA Inc.

17311 Nichols Lane Huntington Beach, California 92647 P art 4b of the Civil Air R egulations . *Certification basis is set forth in Type Certificate Data Sheet A3WE Original Product Type Certificate N umber :

M ake :

M odel :

A3WE The Boeing Company 727-200 Series Description of Type Design Changes : Installation of Galley, G4A, in accordance with FAA Approved Driessen Aircraft Interior systems, Inc. Master Data List No. MDL-101637, dated October 10, 1994, or later FAA approved revisions.

Limitations and Conditions : The approval of this modification applies to the above noted airplane model series only. This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. Note: All of the components installed by this STC meet the Heat Release Requirements (65/65) and the smoke emission requirement

(200) of FAR 25.853 (a-11), amendment 25-66. A copy of this STC must be included in the permanent records of the modified 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.

Date of application : July 18, 1994

Date of issuance : October 26, 1994

Date reissued: July 17, 2014

B y direction of the A dministrator

(Signature) Haifa Haj-Eid Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Ti l )

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.**

N umber (STC No.)

## Every issue (1)

- July 17, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/64/8f/648fc86605471e6eabfa9df547bf0f26efaced010408e8ddac638e63c9ea065c)

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