# STC SA4190NM-D

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International, United States
- Description: Reconfiguration of the Boeing Model 767-284ER airplane. (767-284ER)
- Applied: October 26, 1990
- Status date: June 18, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 21, Part 21, Part 21, Part 21, Part 21
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM)
- Certificate PDF: https://openairdocs.org/files/sha256/ce/7d/ce7dd7e40b7052575f0dfc17398a56f7c464a3fffd40ba3996629678f3c26423
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/74B6D03AB000CDB8862575EC0067BFEF.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4190NM-D

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 767 ([TCDS A1NM](https://openairdocs.org/tcds/A1NM))

## 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: SA4190NM-D Certificate This certificate issued to: Hollingsead International SURRENDERED 2226 Goodyear Avenue Ventura, California 93003 on 6-18-09 Certifies that the change in the type design for the following product with the limitations and conditions therofor as specified hereon meets the airworthiness requirement's of Part 25 of the Federal Aviation Regulations.

Original Product Type Cerlificate Number AINM Make: Boeing Model: 767-284ER Description of Type Design Change: Reconfiguration of the Boeing Model 767-284ER airplane in accordance with Tracor Aviation Inc. Master Drawing List, R14-1, Revision N/C, dated 5/6/91, or later FAA approved revision.

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 modification will not introduce any adverse effect upon the airworthiness of the certificated product. 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: October 26, 1990 Date of Issuance: May 6, 1991

**SEAL AVARI**

TOHINSTRATD Date Reissued: June 20, 1991; April 12, 1995;

December 16, 1996; April 1, 1998; August 1, 2005 May 7, 2007 Date Amended:

By Direction of the Administrator alto K. Woo (Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (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) 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 (3)

- June 18, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/ce/7d/ce7dd7e40b7052575f0dfc17398a56f7c464a3fffd40ba3996629678f3c26423)
- May 7, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a7/2c/a72c53761c8edd221efd1bd794ac20f3d06f78dc0b721ca0295cae1d06861979)
- August 1, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/80/fb/80fb774f49ed39a63dd226ed841499b7fbe49814b5bd1946e305d748809c66a4)

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