# STC SR02630LA - Type: Supplemental type certificate - Status: Current, Issued - Holder: Diagnostic Solution International LLC, United States - Description: Installation of Honeywell Model 15175VXP Health Monitoring System - Applied: June 19, 2014 - Status date: March 15, 2017 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) - Certificate PDF: https://openairdocs.org/files/sha256/31/16/311692a0e66f2d8a8ecd62825143816da360ab3d1922a74b05ca7d08ebb9e814 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/80B386500075434D862580ED0066E779.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02630LA ## ADs that name it (0) None. ## Approved models (2) - Airbus Helicopters AS-350B1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Airbus Helicopters AS-350B2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) ## 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 Diagnostic Solutions International, LLC. 2580 East Philadelphia Street, Unit C Ontario, CA 91761 Part 27*of the Federal Aviation Regulations. *See Page 3 Make : H9EU Airbus Helicopters AS350B1 and AS350B2 Description of Type Design Change: Installation of Honeywell Model 15175VXP Health Monitoring System in accordance with Diagnostic Solutions International Master Drawing List, Document Number 25715, Rev. “A”, dated December 15, 2016, or later FAA approved revision. Instructions for Continued Airworthiness (ICA) 860-25711, Rev. “A”, dated January 30, 2017, or later FAA accepted revision must be made available to the operator at the time of installation. Limitations and Conditions: The installation should not be incorporated in any rotorcraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the rotorcraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. Date of application : June 19, 2014 Date of issuance : March 15, 2017 (Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title) Number SR02630LA Certification Basis: The aircraft certification basis for this modification is 14 CFR part 27 through Amendment 27-47 dated January 30, 2012, for compliance of components and areas affected by the modification. Amendment 27-47 was the amendment in effect on date of STC application. -END- ## Every issue (1) - March 15, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/31/16/311692a0e66f2d8a8ecd62825143816da360ab3d1922a74b05ca7d08ebb9e814) --- 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.