# STC SA5030NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: Addition of Honeywell GPS sensor unit to FAA approved Honeywell FMS installation. - Applied: August 16, 1990 - Status date: March 20, 2020 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Data sheets: [TCDS A9NM](https://openairdocs.org/tcds/A9NM) - Certificate PDF: https://openairdocs.org/files/sha256/af/4a/af4a9780a71de0217876827c2f1bb50599e5c2afe4290376add04c1f26cb7615 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/64534592AB4EC3AC862586170068D727.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA5030NM ## ADs that name it (0) None. ## Approved models (1) - The Cessna Aircraft Company 650 ([TCDS A9NM](https://openairdocs.org/tcds/A9NM)) ## 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: SA5030NM 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: Cessna Aircraft Company A9NM Model: 650 Description of Type Design Change: Addition of Honeywell GPS Sensor Unit to FAA approved Honeywell FMS installation in accordance with FAA Honeywell Document No. 1500-0689, Revision "C", or later FAA approved revision of this document. Honeywell Airplane Flight Manual Supplement, Document No. 1500- 0691, Revision N/C, FAA approved on March 8, 1991, or later FAA approved revision is required as part of this installation. This approval applies only to the above listed Cessna model when the aircraft has been modified by STC SA3461NM. This approval should not be extended to other aircraft of this 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 effects 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. Date of Application: August 16, 1990 Date Reissued: January 20, 2009; March 20, 2020 Date of Issuance: March 2 1, 1991 Date Amended: 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 20, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/af/4a/af4a9780a71de0217876827c2f1bb50599e5c2afe4290376add04c1f26cb7615) - January 20, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/dd/e4/dde4eed3f0d3c3aaf4e5630873456e38be07ace7cf3e6f5cd09daca1be3a8f74) --- 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.