# STC SA1368NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Safran Cabin Inc., United States
- Description: Installation of C&D Interiors P/N 1441002.
- Applied: August 19, 1982
- Status date: July 18, 2025
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE)
- Certificate PDF: https://openairdocs.org/files/sha256/be/19/be19285e9db05b5dea42d23ea26e99ba5a87823804c79fbb598344c199471713
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173582827620260107191636.0001
- DRS record last changed: January 7, 2026
- Page: https://openairdocs.org/stc/SA1368NM

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company DC-10-30 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))

## 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: SA1368NM This certificate issued to: Safran Cabin Inc.

7330 Lincoln Way Garden Grove, CA 92841 Part 25 of Title 14, Code of Federal Regulations Type Certificate Number: A22WE Original Product Make: McDonnell Douglas Corporation Description of Type Design Change: Model: DC-10-30 Installation of P/N 1441002 per FAA approved Drawing List No. 144-1000, Revision "A," dated October 6, 1982, or later FAA sealed revision.

The approval of this change in type design applies to the McDonnell Douglas DC-10-30 aircraft model 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 these airworthiness of these aircraft. This determination should include consideration of significant changes in weight distribution such as in the fixed disposable weight of the fuselage. 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: 08/19/1982 Date Reissued: 11/04/1982 11/12/1993 12/29/2005 Date of Issuance: 10/15/1982 Date Amended:

Title: ODA Administrator, ODA-606394-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1368NM Effective Date: 07/18/2025

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number. _ To (Name and address of transferee):

From (Name and address of grantor);

The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STO holder.

United States of America HEN AVATO Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1368NM Effective Date: 07/18/2025 Date Reissued: - cont.: 12/03/2018; 07/18/2025 ---END---

## Every issue (2)

- July 18, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/be/19/be19285e9db05b5dea42d23ea26e99ba5a87823804c79fbb598344c199471713)
- December 29, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ec/95/ec95cb58a073cec89fad939fbb752898cd92337f9c2d39fb204644933732de6b)

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