# STC SA6052NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States
- Description: Installation of Provisions Only for oven assemblies
- Applied: April 13, 1993
- Status date: May 19, 2015
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE)
- Certificate PDF: https://openairdocs.org/files/sha256/16/6e/166e7cd315f7e9d34fab8582d0f54431b1ccc723a0377138e48a4d8b15714e8f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A8C64EEB8900F44786257E6C005A6BDD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA6052NM

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company DC-9-82 (MD-82) ([TCDS A6WE](https://openairdocs.org/tcds/A6WE))

## 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 Part *4b of the Civil Air Regulations.

*Certification basis is set forth in Type Certificate Data Sheet A6WE.

A6WE The Boeing Company DC-9-82 (MD-82) Description of Type Design Change: Installation of Provisions Only for oven assemblies in accordance with FAA Approved Driessen Aircraft Interior Systems, Inc. Master Data List No. MDL-124028, Revision “B”, dated September 1, 1993, or later FAA approved revisions.

Limitations and Conditions: The approval of this modification applies to the above noted aircraft 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 the STC meet the Heat Release Requirement (65/65) and the Smoke Emission Requirement (200) of Title 14, Code of Federal Regulations 25.853 (a-1), 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 : April 13, 1993

Date of issuance : September 13, 1993

Date reissued : July 17, 2014, May 19, 2015

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

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (2)

- May 19, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/16/6e/166e7cd315f7e9d34fab8582d0f54431b1ccc723a0377138e48a4d8b15714e8f)
- July 17, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a8/20/a8204a123e2b2c168354844ba83429cb1bee5bb4d535fccba80e1f4b1bcbe286)

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