# STC SA228EA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rockwell Collins Inc, United States
- Description: Installation of Inflight Motion Picture system.
- Applied: August 13, 1964
- Status date: June 15, 2016
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25)
- Certificate PDF: https://openairdocs.org/files/sha256/e9/94/e994ceee964cfa21c998e1e3528a1e69a23bbcddd9ad0b861500ade56f05e48a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1A1AB469C05E20BB86257FE0007392D2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA228EA

## ADs that name it (0)

None.

## Approved models (5)

- McDonnell Douglas Corporation DC-8-12 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- McDonnell Douglas Corporation DC-8-21 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- McDonnell Douglas Corporation DC-8-33 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- McDonnell Douglas Corporation DC-8-51 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- McDonnell Douglas Corporation DC-8-52 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

This Certificate issued to Rockwell Collins, Inc.

1733 Alton Parkway Irvine, California 92606 Part 4b of the Civil Air Regulations.

4A25 McDonnell Douglas DC-8-12, -21, -33, -51, -52 Description of Type Design Change: Installation of Inflight Motion Picture System in accordance with Lockheed Aircraft Service Report No. 2989, dated June 24, 1968, Revised January 30, 1969.

Limitations and Conditions: This approval should not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the 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.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: August 13, 1964

Date of issuance: September 24, 1964

Date reissued: 10/24/73; 04/15/88; 11/20/89;

8/30/00; 05/30/06; 06/15/16

Date amended: October 23, 1964;

*(See Page Three)

(Signature)

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

Number SA228EA

Date amended: January 8, 1965; March 11, 1965; June 25, 1965; June 15, 1966;

September 9, 1966; March 20, 1967; May 2, 1967; November 9, 1967;

March 12, 1969; February 26, 1971

- END -

## Every issue (2)

- June 15, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e9/94/e994ceee964cfa21c998e1e3528a1e69a23bbcddd9ad0b861500ade56f05e48a)
- May 30, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/56/8e/568e3489a1150b55ec0224d462639368843fa3273d16de368ec039ed6536e2fc)

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