# STC SA4218NM-D

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International, United States
- Description: Reconfiguration of interior seating. (A300 B4 SERIES -622R)
- Applied: May 11, 1993
- Status date: June 19, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU)
- Certificate PDF: https://openairdocs.org/files/sha256/ad/6c/ad6c57688feee8dc0d5588fc910981e28d2ad718d73accd38a4d3abf4d94242d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DCA5A0B4221778EE8625760F006BABCB.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4218NM-D

## ADs that name it (0)

None.

## Approved models (2)

- Airbus A300 B4 Series ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A300B4-622R ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))

## 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: SA4218NM-D This certificate issued to: Hollingsead International CertiFicate 2226 Goodyear Avenue SURRENDERED Ventura, California 93003 6-19-09 Certifies that the change in the type design for the following product with le limitations and conditions therefor as specified hereon meet's the airworthiness requirement's of Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number A35EU Make: AIRBUS Model: A300 B4-622R Description of Type Design Change: Reconfiguration of interior seating in accordance with Deutsche Aerospace, and Flight Equipment & Engineering Ltd. documentation:

DA-25-062 Service Bulletin dated 4 June 1993 AWA 004 93A Engineering Order dated 4 June, 1993 25-20-1303 Service Bulletin Basic Rev. Dated April 1993

• 25-20-1304 Service Bulletin Basic Rev. Dated April 1993

• 25-20-1306 Service Bulletin Basic Rev. Dated May 1993, or later FAA approved revisions.

Limitations and Conditions: This approval should not be incorporated on any certificated product of this model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated modifications will not introduce any adverse effect upon the airworthiness of the certificated product. No findings of compliance with FAR 25.853 were required by this modification. 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: May 11, 1993 Date Reissued: April 12, 1995; December 16, 1996;

April 1, 1998; August 1, 2005; July 31, 2006 Date of Issuance: June 10, 1993 Date Amended:

By Direction of the Administrator Calta K. Woo (Signature) AOMNISTRA Nor Staff, Los Angeles Aircraft Certification Office Manager, Technical & Administrative Support (Title)

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer)_ (Number and street) (City, State, and Zip code) trom (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 (3)

- June 19, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/ad/6c/ad6c57688feee8dc0d5588fc910981e28d2ad718d73accd38a4d3abf4d94242d)
- July 31, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/dc/c1/dcc18c56699293c2e0f3bd3b68022c7f92d1a1b8d76a54314289885c75482a52)
- August 1, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a3/59/a3596dee3b9ce0ce7633055fa41dec00d9b901cd371a113ff8fe5b781c85eb3d)

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