# STC SA00007SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Spoilers Inc, United States - Description: Installation of hydraulically actuated spoiler kit SP11,000. - Applied: October 1, 1992 - Status date: July 9, 2013 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A12CE](https://openairdocs.org/tcds/A12CE) - Certificate PDF: https://openairdocs.org/files/sha256/5c/b8/5cb8568ec5abd9f991bc05d486fc0beaa2cc55514d300552f26a950b1eef346b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/ACA355287AADA96C86257BA500515FC6.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00007SE ## ADs that name it (0) None. ## Approved models (3) - Hawker Beechcraft Corporation 60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE)) - Hawker Beechcraft Corporation A60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE)) - Hawker Beechcraft Corporation B60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE)) ## 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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA00007SE This certificate, issued to Spoilers, Inc. 1202 26th Avenue NW Gig Harbor, WA 98335 Part 23 of the Federal Aviation Regulations. February 1, 1965 Original Product Type Certificate Number: A12CE Make: Beechcraft Model: 60, A60, B60 Description of the Type Design Change: Installation of hydraulically actuated Spoiler Kit SP 11,000 in accordance with Spoilers, Inc. Master Drawing List SP 11,000 dated April 8, 1993, and Installation Instructions SP 11,000 dated April 9, 1993, or later FAA approved revisions. NOTE: This STC has been demonstrated to be compatible with STC SA5761NM. Approval of this change in type design applies 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 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 aircraft. A copy of this Certificate and Airplane Flight Manual Supplement dated July 26, 1993, must be maintained as part of the permanent records for the modified aircraft. Date of application: October 1, 1992 Date reissued: July 9, 2013 Date of issuance: July 26, 1993 Date amended: (Signature) Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - July 9, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5c/b8/5cb8568ec5abd9f991bc05d486fc0beaa2cc55514d300552f26a950b1eef346b) - July 26, 1993: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/29/45/29450a5150a827a7518c2c2ae976567b053124415ceb1704b7a6ea420cc74105) --- 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.