# STC SA00487WI - Type: Supplemental type certificate - Status: Current, Issued - Holder: Phoenix Aerospace, Inc, United States - Description: Installation of Phoenix Aerospace Inc (PAI) solid state DC voltage regulator assembly P/N VR-1010-24-24A - Applied: November 7, 1996 - Status date: December 12, 1996 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A12CE](https://openairdocs.org/tcds/A12CE) - Certificate PDF: https://openairdocs.org/files/sha256/d5/99/d599e9b07d2f9c09bc7aeb530a9394706facfad8b1f3de0a66763b63afd6d99b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/91598178549C9AD385256CC1007DC962.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00487WI ## ADs that name it (0) None. ## Approved models (3) - Raytheon Aircraft Company 60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE)) - Raytheon Aircraft Company A60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE)) - Raytheon Aircraft Company B60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00487W1 This certificate issued to: Phoenix Aerospace Inc. 220 W. 80th Terrace Kansas City, MO 64114 Purt 23 of the Federal Aviation Regulations. Original Product - - Type Certificato Number : AI2CE Make: Beech Model: 60; A60; B60 Description of Type Design Change: Installation of Phoenix Aerospace Inc. (PAI) Solid State DC Voltage Regulator Assembly P/N VR-1010-24-2A, in accordance with (1) PAI Installation Instructions for Installing Phoenix Aerospace Model VR- 1010-24-2A Solid State DC Voltage Regulator in Beechcraft Duke Model 60, S/N P-4 thru 126 except S/N 123; A60, S/N P-123 and P127 thru P-246; B60, S/N P-247 thru P-465, dated November 6, 1996, and (2) Phoenix Aerospace Top Assembly Drawing No. 095027, Rev. Q, dated September 20, 1991, or later FAA Approved revisions to (1) or (2). Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer Date of Application: November 07, 1996 Date Reissued: Date of Issuance: December 12, 1996 Date Amended: FEDERAL AVIATION By Direction of the Administrator ames N11 ยท (Signature) ames M. Peterson TOMNISTRATO Associate ACO Mgr., Systems & Propulsion Wichita Aircraft Certification Office (Title) ## Every issue (1) - December 12, 1996: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d5/99/d599e9b07d2f9c09bc7aeb530a9394706facfad8b1f3de0a66763b63afd6d99b) --- 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.