# STC SA7060NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: Installation of Honeywell/Racal Aeronautical satellite communications system. - Applied: October 29, 1991 - Status date: March 9, 2020 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) - Certificate PDF: https://openairdocs.org/files/sha256/49/29/4929b33a68ad3f703cdb70319ba96d063357b3ef4fc700ae02127e41274d8812 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E89C42765DA4E26486258602006986D8.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA7060NM ## ADs that name it (0) None. ## Approved models (3) - Airbus A300 B4-600 Series ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus A300 B4-600R Series ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus A310 300 Series ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) ## 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 (5/14) Page 1 of 2 Number: SA7060NM This certificate issued to: Honeywell International Inc. 21111 N 19th Ave Phoenix, Arizona 85027 Part 25 of the Federal Aviation Regulations. Original Product – Type Certificate Number: Make: Airbus Industrie A35EU Model: A310-300 Series, S300B4-600, -600R Series Description of Type Design Change: Installation of Honeywell/Racal Aeronautical Satellite Communication System in accordance with FAA Approved Honeywell Master Data List, Engineering Specification ML4078642, Revision “-”, dated December 17, 1993, or later FAA approved revisions of this specification. 1) The approval of this change in type design applies only when the installation provisions have been installed and approved by the manufacturer. 2) The approval should not be ex tended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is found 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. 3) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the person written evidence of that permission. Date of Application: October 29, 1991 Date Reissued: February 9, 2009, March 9, 2020 Date of Issuance: February 8, 1994 Date Amended: December 6, 1996 By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM FAA Form 8110-2 (5/14) Page 2 of 2 To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): ## Every issue (2) - March 9, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/49/29/4929b33a68ad3f703cdb70319ba96d063357b3ef4fc700ae02127e41274d8812) - February 9, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d7/72/d772461ea3a921756da962a990ed90344f9e69762f43727b874a283d34d86353) --- 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.