# STC SH1262NW - Type: Supplemental type certificate - Status: Current, Amended - Holder: Onboard Systems International, United States - Description: Fabrication of either Onboard Systems Hydraulic Model H-69 (Part Number 200-018-00) or Electronic Models E-69 (Part Numbers 200-058-00 and 200-295-00) Cargo Hook Load Weigh Systems - Applied: May 1, 1981 - Status date: November 8, 2013 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 21, Part 27 - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) - Certificate PDF: https://openairdocs.org/files/sha256/79/b7/79b774d32adaf1a11f182f899a2fd0e200e629cc1e7b68654a40ae77d382010b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8F76D193738716C586257C22006E5BA9.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SH1262NW ## ADs that name it (0) None. ## Approved models (8) - Eurocopter France AS-350B ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350B1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350B2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350B3 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350BA ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350C ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350D ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350D1 ([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 SH1262NW This certificate, issued to Onboard Systems 13915 NW 3rd Court Vancouver, WA 98685 Part * of * Regulations. * FAR 21.29 and FAR 27 effective 2/1/65 plus Amendment 27-1 through 27-10, plus FAA Special Conditions No. 27-79-EU-23, dated 8/13/77. Original ProductType Certificate Number: H9EU Make: Eurocopter France Model: AS350C, AS350D, AS350D1, AS350B, AS350B1, AS350B2, AS350BA, and AS350B3 Description of the Type Design Change: Fabrication of either Onboard Systems Hydraulic Model H-69 (Part Number 200-018-00) or Electronic Models E-69 (Part Numbers 200-058-00 and 200-295-00) Cargo Hook Load Weigh Systems in accordance with Federal Aviation Administration (FAA) approved Onboard Systems Master Drawing List No. 155-010-00, Revision 20, dated October 25, 2004, or later FAA-approved revision, Limitations and Conditions: Approval of this change in type design applies only to the Eurocopter helicopter models identified above. This approval should not be extended to other aircraft of these models 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 helicopter. Date of application: May 1, 1981 Date reissued: August 2, 1990 Date of issuance June 23, 1981 Date amended: 3/22/88; 8/2/90; 9/20/90; 12/23/91; 3/17/92; 2/12/93; 8/13/04; 3/15/05; 11/8/13 (Signature) Manager, Seattle Aircraft Certification Office (Title) Number SH1262NW Onboard Systems Issued: June 23, 1981 Reissued: August 2, 1990 Amended: 3/22/88; 8/2/90; 9/20/90; 12/23/91; 3/17/92; 2/12/93; 8/13/04; 3/15/05; 11/8/13 Description of Type Design Change continued: Installation of either the H-69 system in accordance with FAA approved Onboard Systems Owner’s Manual No. 120-009-00, Revision B, dated January 10, 1990, or later FAA approved revision, or the E-69 systems in accordance with FAA-approved Onboard Systems Owner’s Manual No. 120-022-00, Revision 8, dated March 2, 2010, or later FAA-approved revision, for the P/N 200-058-00, or FAA approved Onboard System Owner’s Manual No. 120-114-00, Revision 4, dated January 20, 2011, or later FAA approved revision for the P/N 200-295-00. Inspect and maintain the H-69 system in accordance with Section 4.6 of Onboard Systems Owners Manual No. 120-009-00, Revision B, dated January 10, 1990, or later FAA-approved revision; and the E-69 systems in accordance with Section 4 of Onboard Systems Owners Manual No. 120-022-00, Revision 8, dated March 2, 2010, or later FAA-approved revision for the P/N 200-058-00, or in accordance with Section 4 of Onboard Systems Owners Manual No. 120-114-00, Revision 4, dated January 20, 2011, or later FAA-approved revision for the P/N 200-295-00. Rotorcraft modified in accordance with this STC must be operated in accordance with an FAA approved copy of Onboard Systems Rotorcraft Flight Manual Supplement (RFMS). For H-69 systems, in Section 8 of Owner’s Manual No. 120-009-00, the RFMS dated August 2, 1990; for E-69 system P/N 200-058-00, in Section 5 of Owner’s Manual No. 120-022-00, the RFMS dated February 12, 1993; and for E-69 system P/N 200-295-00, the RFMS No. 121-024-00, Revision 2 dated November 6, 2013, or later FAA approved revision. A copy of this Certificate, FAA approved RFMS, and Maintenance Manual must be maintained as part of the permanent records of the modified rotorcraft. -- END -- **FAA FORM 8110-2- 1 (10-69) PAGE 3 OF 3 PAGES** ## Every issue (3) - November 8, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/79/b7/79b774d32adaf1a11f182f899a2fd0e200e629cc1e7b68654a40ae77d382010b) - March 15, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/54/cb/54cba707469fb4761ba6af3d18d7a06622644d53fd5fd342135850f405c8e7e8) - August 13, 2004: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8f/78/8f78d338088085151e856141b2906770d4cff2b98abcd2f65243ba50c18b3b27) --- 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.