# STC ST00032LB

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States
- Description: Installation of galley module.
- Applied: July 11, 1994
- Status date: July 17, 2014
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM)
- Certificate PDF: https://openairdocs.org/files/sha256/e0/a0/e0a0414b7a730af814ffaa151fe32510c6fe09e0cd7ce2dbb0280098f9ee0643
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1D1A996704A2DFCF86257D500057750A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00032LB

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 757-200 Series ([TCDS A2NM](https://openairdocs.org/tcds/A2NM))

## 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 *25 of the F ederal A viation R egulations . *Certification basis is see Type Certificate Data Sheet A2NM Original Product Type Certificate N umber :

M ake :

M odel :

A2NM The Boeing Company 757-200 Series Description of Type Design Changes : Installation of Galley Module in accordance with FAA Approved Driessen Aircraft Interior Systems Master Drawing List MDL-101636, Revision NC” dated December 6, 1994, or later FAA approved revisions.

Limitations and Conditions : This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is found by the installer that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the aircraft’s airworthiness. Note: The components installed by the STC have been demonstrated to meet the Heat Release Requirements (65/65) and the Smoke Emission Requirement (200) of FAR 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

Date of application : July 11, 1994

Date of issuance : February 6, 1995

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 (Titl )

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/e0/a0/e0a0414b7a730af814ffaa151fe32510c6fe09e0cd7ce2dbb0280098f9ee0643)

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