# STC ST00361LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: Installation of Honeywell HUD-2020 heads-up display system for Category II approach criteria. - Applied: December 19, 1994 - Status date: March 19, 2020 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA) - Certificate PDF: https://openairdocs.org/files/sha256/3f/29/3f2953ebe881bf639a214af3a5aa20ea5c1f0f260064ce26d4d13ba9da746e9c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7A650230E580E1B786258616006B306F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST00361LA ## ADs that name it (0) None. ## Approved models (1) - Gulfstream Aerospace Corporation G-IV ([TCDS A12EA](https://openairdocs.org/tcds/A12EA)) ## 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: ST00361LA 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: Gulfstream Aerospace A12EA Model: G-IV Description of Type Design Change: Installation of Honeywell HUD-2020 Head Up Display system on the Gulfstream G-IV airplane for Category II approach criteria in accordance with FAA approved Master Data List Spec. No. 5220-0697, revision G dated July 26,1997 or later FAA approved revision. This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configurations will not introduce any adverse effect upon the airworthiness of the aircraft. Provisional STC(s), listed in the Master Data List Spec. No. 5220-0697, must be installed prior to this installation on each airplane. A copy of this STC must be included in the permanent record of the modified 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: December 19, 1994 Date Reissued: July 1, 1997; February 27, 2009; March 19, 2020 Date of Issuance: April 30, 1997 Date Amended: August 19, 1997 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 19, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3f/29/3f2953ebe881bf639a214af3a5aa20ea5c1f0f260064ce26d4d13ba9da746e9c) - February 27, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ca/08/ca08a95c3d54fe1dc3f46ce5d3d46b11b3c377b580be0db932ce33dcc15698f7) --- 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.