# STC SA3014WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Rockwell Collins Inc, United States - Description: Installation of floor game table assembly. - Applied: March 19, 1975 - Status date: August 10, 2016 - 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/sha256/8a/11/8a110d4f0425b3324249ccd3eb736124324e2279361d79dca0807f65499c8cca - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4891E73B11ABB27B8625801B00562976.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA3014WE ## ADs that name it (0) None. ## Approved models (2) - McDonnell Douglas Corporation DC-10-10 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE)) - McDonnell Douglas Corporation DC-10-10F ([TCDS A22WE](https://openairdocs.org/tcds/A22WE)) ## 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. FAA Form 8110-2(10-68 Page 1 of 2 Number SA3014WE This Certificate issued to Rockwell Collins, Inc. 1733 Alton Parkway Irvine, California 92606 Part 25* of the Federal Aviation Regulations. *(FAR 25 dated February 1, 1965, with Amendments 1 thru 22 “Airworthiness Standards: T t C t Ai l ”) Original Product Type Certificate Number : A22WE McDonnell Douglas DC-10-10; DC-10-10F Description of Type Design Change: Installation of Floor Game Table Assembly in accordance with FAA sealed Bell & Howell Drawing List 484431. Limitations and Conditions: The approval of this change in type design applies basically to DC-10-10 and DC-10-10F aircraft only. This approval should not be extended to other aircraft of theses model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no 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: March 19, 1975 Date of issuance: May 3, 1975 Date reissued: Nov. 10, 1982; June 17, 1985; Feb. 18, 1992; Jan. 23, 1998; May 30, 2006; August 10, 2016 Date amended: January 20, 1976 (Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title) The FAA will reissue the certificate in the name of the transferee and forward it to him. 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 (2) - August 10, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8a/11/8a110d4f0425b3324249ccd3eb736124324e2279361d79dca0807f65499c8cca) - May 30, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b0/48/b0483a0305c39109fa20ec47202710acf9db43d1d363077342ce9c3dc0540284) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.