# STC ST00054LA-D

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International, United States
- Description: Installation of a video control center.
- Applied: July 11, 1995
- Status date: June 23, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 25
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE)
- Certificate PDF: https://openairdocs.org/files/sha256/79/92/7992e060917344dc519e15df47c08cd5720a7ac3b88984290c17a1d8180ec66e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A1C6F538187E628786257608006C6084.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST00054LA-D

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 747-400 Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE))

## 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: ST00054LA-D Certificate This certificate issued to: Hollingsead International SURRENDERED 2226 Goodyear Avenue on 6-23-09 Ventura, California 93003 Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number A20WE Make: Boeing Model: 747-400 Description of Type Design Change:

Installation of a video control center in accordance with C & D Interiors documentation:

C & D Interiors:

Drawing List 8471000, Rev. NC, Dtd 9/1/95 or Rev. A, dated December 12, 1995, Video Control Center Canadian International Airlines B747-400.

Elsinore LP:

Master Data List Document No. 4011-3, Rev. N/C, dated February 5, 1996, or later FAA approved 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. This approval meets the flammability requirements of § 25.853(a)(b) Amendment 32, the heat release requirements of § 25.853(a-1) and part 25 appendix F, Part IV Amendment 66 and the smoke density requirements of § 25.853(a-1) and part 25 appendix F, Part V Amendment 66. 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: July 11, 1995 Date Reissued: February 9, 1996; April 1, 1998;

June 13, 2005; July 31, 2006 Date of Issuance: September 19, 1995 Date Amended: February 9, 1996 FEDERAL AVIATION By Direction of the Administrator Carlton K. W00 (Signature) Manager, Technical & Administrative Support TOMNISTRATOS Staff, Los Angeles Aircraft Certification Office (Title)

TRANSFER ENDORSEMENT Transter 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 23, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/79/92/7992e060917344dc519e15df47c08cd5720a7ac3b88984290c17a1d8180ec66e)
- July 31, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/14/8c/148cd06da80afcbc0cea10351a317dec29a56a9db733414b7b54c1602ac5f125)
- June 13, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/3c/e2/3ce2bcc2a8dde4ca1d8f2afa3958ee816450aa0b91350405be44bcfbd57af691)

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