# STC SR01373SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Aerometals, United States - Description: Installation of an engine air filter. - Applied: June 2, 2003 - Status date: August 15, 2014 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) - Certificate PDF: https://openairdocs.org/files/sha256/49/5c/495c6d65159d6017901712b80d7169682bd16fa40df453625885c7836fabaefb - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/64FDA16D58B26FDB86257D3A005DD528.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR01373SE ## ADs that name it (0) None. ## Approved models (1) - Airbus Helicopters EC 130 B4 ([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. Number SR01373SE This certificate, issued to Aerometals, Inc. 3920 Sandstone Drive El Dorado Hills, CA 95762 Part 21.29 of the Federal Aviation Regulations. Original ProductType Certificate Number: H9EU Make: Airbus Helicopters Model: EC130B4 Description of the Type Design Change: Installation of an engine air filter, in accordance with INTEC Master Drawing List No. 1350-1001, Revision G, dated January 05, 2004, and INTEC Installation Instructions 1130-INST-1, Revision A, dated December 23, 2003, or later Federal Aviation Administration (FAA) approved revisions to these documents. Limitations and Conditions: This air filter installation must be maintained in accordance with INTEC Document 1130-SERIES-ICA-1, Revision-IR, dated December 23, 2003, or later FAA-approved revision. Approval of this change in type design applies to the above model rotorcraft only. This approval should not be extended to rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer 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. A copy of this certificate, and the FAA-Approved Rotorcraft Flight Manual Supplement, dated January 23, 2003, or later FAA-approved revision, must be maintained as part of the permanent record 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: June 2, 2003 Date reissued: 11/9/06; 3/20/07; 6/11/07; 7/30/10; 8/15/14 Date of issuance: February 3, 2004 Date amended: November 9, 2006 (Signature) Manager, Seattle Aircraft Certification Office (Title) ## Every issue (3) - August 15, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/49/5c/495c6d65159d6017901712b80d7169682bd16fa40df453625885c7836fabaefb) - July 30, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/3a/6e/3a6eb4ce3ca858ab2f52019589804e6236744902ed973eb91939c9d1e4499275) - June 11, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/53/06/530699f0ef080f366f63b74e5682b94e9454a3715c6cb2b0fdc71326014c7fb4) --- 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.