# STC ST00049LA-D

- Type: Supplemental type certificate
- Status: Historical, Cancelled
- Holder: Hollingsead International, United States
- Description: Installation of a passenger entertainment system.
- Applied: April 10, 1995
- Status date: February 13, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE)
- Certificate PDF: https://openairdocs.org/files/sha256/c7/65/c7659db6d5235ab51cc16fc9885bf15bd621f50ee21dace42fb2652343f72cd2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5847FD9880B7296C86257638004555D0.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST00049LA-D

## ADs that name it (0)

None.

## Approved models (1)

- McDonnell Douglas Corporation MD-11 ([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: ST00049LA-D 2-13509 This certificate issued to: Hollingsead International 10 GE555L 2226 Goodyear Avenue Ventura, California 93003 Certifies that the change in the type design for the following product with the limitation's and conditions therefor as specified hereon meet's the airworthiness requirement's of Part 25 of the Federal Aviation Regulations.

Original Product Type Cerlificate Number: A22WE Make: McDONNELL DOUGLAS Model: MD-11 Description of Type Design Change: Installation of a Passenger Entertainment System in accordance with Elsinore Systems Integration Group Master Drawing List 3117-1, Rev. D, dated 06/03/96 and Index List 3117-2, Rev. D, dated 06/04/96, 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. A copy of this STC and Master Drawing List No. 3117-1, Revision D must be included in the permanent records of the modified aircraft. All of the above interior furnishings meet the flammability requirements of FAR

25.853(b) (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.

Woo (Signature) TOMINSTRATO Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

## Every issue (4)

- February 13, 2009: Cancelled, Historical. [certificate](https://openairdocs.org/files/sha256/c7/65/c7659db6d5235ab51cc16fc9885bf15bd621f50ee21dace42fb2652343f72cd2)
- February 13, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/c7/65/c7659db6d5235ab51cc16fc9885bf15bd621f50ee21dace42fb2652343f72cd2)
- July 31, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c0/44/c04460df5fda04a84e176914c19dcf138c6e4919fdfd19ca174258fa9691d8d4)
- June 13, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f6/21/f6212f64081f9d943df5856184eef1a93c9d1f89462f7a5366e7b795100a4836)

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