# STC SR01573SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Evergreen Helicopters Inc, United States - Description: Installation of Pulselite and Whelen Landing Light. - Applied: May 24, 2005 - Status date: November 28, 2005 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H1IN](https://openairdocs.org/tcds/H1IN) - Certificate PDF: https://openairdocs.org/files/sha256/0a/1d/0a1db6fe3b7d09cc071ada7ca669aa0c7545c41313c58fa0b295c4efd5bf96ae - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/97CA45C3C8083CF2862570CA006DA46A.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR01573SE ## ADs that name it (0) None. ## Approved models (1) - Eurocopter France SA.315B Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN)) ## What the certificate says Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers. Number: SR01573SE This certificate issued to: Evergreen Helicopters, Inc. 3850 Three Mile Lane McMinnville, OR 97128 Part 6 of the Civil Air Regulations. Original Product ⎯Type Certificate Number: H11N Make: Eurocopetr France Model: SA.315B Alouette III Description of Type Design Change: Installation of Pulselite and Whelen Landing Light, manufactured and installed in accordance with Evergreen Helicopters Drawing Number L315-1-227MCM05, Revision 2, dated June 9, 2005, or later Federal Aviation Administration (FAA) approved revision. The Landing Light Housing must be maintained in accordance with David J. Hastings Document Number L315-1-227-ICA, Revision IR, dated June 23, 2005, or later FAA approved revision. Limitations and Conditions: Precise Flight, Inc., STC SH3319NM, must be concurrently installed with this STC. Approval of this change in type design applies to the rotorcraft models listed above only. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. Rotorcraft modified in accordance with this STC must be operated in accordance with the FAA approved copy of the Rotorcraft Flight Manual Supplement, David J. Hastings Document L315-1-227-09, FAA approved June 27, 2005, or later FAA approved revision. A copy of this Certificate must be maintained as part of the permanent records of the modified rotorcraft. 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: May 24, 2005 Date reissued: November 28, 2005 Date of Issuance: July 7, 2005 Date amended: (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - November 28, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0a/1d/0a1db6fe3b7d09cc071ada7ca669aa0c7545c41313c58fa0b295c4efd5bf96ae) - July 7, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/0c/35/0c35619a93377b4d93d27c3011efef41eb8d4758671745f24bcb0410a99d1d58) --- 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.