# STC SH2692NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Hillsboro Aviation Inc, United States - Description: Installation of a Dual Electric Boost Pump System. - Applied: March 12, 1984 - Status date: June 7, 2016 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW) - Certificate PDF: https://openairdocs.org/files/sha256/c0/73/c073140c96b492947178ec367898b755239c3dc210d00d0fce786aa6bcf752dc - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4EE6EA0DDF64085386257FCB007679BA.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SH2692NM ## ADs that name it (0) None. ## Approved models (1) - Bell Helicopter Textron Inc. 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW)) ## 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 SH2692NM This certificate, issued to Hillsboro Aviation, Inc. 3845 NE 30th Avenue Hillsboro, OR 97124 Part 7 of the Civil Air Regulations. DATED August 1, 1956, including Amendments 7-1 through 7-4 Original ProductType Certificate Number: H1SW Make: Bell Model: 205A-1 Description of the Type Design Change: Installation of a Dual Electric Boost Pump System in accordance with Heli-Conversions, Inc. Installation Instructions Document Number HJ2000, dated March 15, 1984, or later Federal Aviation Administration (FAA) approved revision. Limitations and Conditions: Approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the inter-relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and FAA-approved airplane flight manual supplement shall be maintained as part of the permanent records for the modified aircraft. Date of application: March 12, 1984 Date reissued: 12/1/86; 4/12/13; 6/7/16 Date of issuance: April 16, 1985 Date amended: (Signature) Manager, Seattle Aircraft Certification Office (Title) Number SH2692NM Hillsboro Aviation, Inc. Issued: April 16, 1985 Reissued: 12/1/86; 4/12/13; 6/7/16 Amended: The limitations and conditions of Type Certificate Data Sheet H1SW apply except where superseded by the following: Bell 205A-1, 15 PCL4 (TRANSPORT AIRPLANE CATEGORY B) AS MODIFIED BY STC SH2692NM Placards: The following placards are to be placed as follows: 1. At L.H. Boost Pump Circuit Breaker 2. In full view of pilot instrument panel 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. - END - **FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES** **LEFT BOOST PUMP** **THIS AIRCRAFT EQUIPPED WITH** **DUAL ELECTRICAL BOOST PUMPS** ## Every issue (3) - June 7, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c0/73/c073140c96b492947178ec367898b755239c3dc210d00d0fce786aa6bcf752dc) - April 12, 2013: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/7b/f7/7bf79568a83d264ed0f19cba0a607223d48d29746bc08b96ad7c505b66ccccf3) - December 1, 1986: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/58/8b/588bb47c1624c36498d40fb41c486a25b3a24fecc74498f301b5b7bd13b34826) --- 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.