# STC SA04132SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Western Aircraft, United States - Description: Installation of the MAX-VIZ EVS-1000. - Applied: July 28, 2003 - Status date: May 3, 2006 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) - Certificate PDF: https://openairdocs.org/files/sha256/04/0c/040cf83f932cabc955cff96cd5849624c2493dc7566f2cadae26765a8b6b945a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/56D937D46A7DE90C86257179004CB7A4.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA04132SE ## ADs that name it (0) None. ## Approved models (3) - Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) ## 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. Number SA04132SE This certificate, issued to Western Aircraft, Inc. 4300 S. Kennedy St. Boise, ID 83705 Part 23 of the Federal Aviation Regulations. Original Product⎯Type Certificate Number: A78EU Make: Pilatus Model: PC-12, PC-12/45, PC-12/47 Description of the Type Design Change: Installation of the MAX-VIZ EVS-1000 in accordance with Western Aircraft, Inc. Master Drawing List No. W6516-001 Revision 4, dated February 28, 2006, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to the above aircraft models only. A copy of this certificate and the FAA approved Airplane Flight Manual Supplement (AFMS), document number W6516-AFMS dated May 3, 2006 must be maintained as part of the permanent records for the modified aircraft. This approval should not be extended to other aircraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This installation must be maintained in accordance with the Instructions for Continued Airworthiness referenced in the Master Drawing List. 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: July 28, 2003 Date reissued: Date of issuance: July 16, 2004 Date amended: May 3, 2006 Original signed by Kenneth Fairhurst (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - May 3, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/04/0c/040cf83f932cabc955cff96cd5849624c2493dc7566f2cadae26765a8b6b945a) - July 16, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/eb/08/eb089918a895c4ee0992e4396b45d328071be9dc2670a8386782d339be3493ed) --- 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.