# STC SA02548SE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Hood Tech Corp. Vision, Inc., United States - Description: Installation of a Tac Rack external sensor rack - Applied: October 7, 2016 - Status date: July 24, 2017 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A00006SE](https://openairdocs.org/tcds/A00006SE) - Certificate PDF: https://openairdocs.org/files/sha256/d0/bc/d0bc5bed514e91b007f5f8e0a660711e7ff7be9952520abc4abfdaf3b21e17b7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/98D0CD33803F4BAD8625816A00670571.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02548SE ## ADs that name it (0) None. ## Approved models (2) - Topcub Aircraft Inc CC18-180 ([TCDS A00006SE](https://openairdocs.org/tcds/A00006SE)) - Topcub Aircraft Inc CC18-180A ([TCDS A00006SE](https://openairdocs.org/tcds/A00006SE)) ## 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. Un i te d St ate s of Am e ri ca Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA02548SE This certificate, issued to Hood Tech Corp. Vision, Inc. 1750 Country Club Road Hood River, OR 97031 Part 23 of the Federal Aviation Regulations. Original ProductType Certificate Number: A00006SE Make: Topcub Aircraft, Inc. Model: CC18-180, CC18-180A Description of the Type Design Change: Installation of a Tac Rack external sensor rack in accordance with Instructions for Installation and Continued Airworthiness, Report No. HTCV-006, Revision A-04, dated June 16, 2017, or later Federal Aviation Administration (FAA) approved revision. Maintained in accordance with Instructions for Installation and Continued Airworthiness, Report No. HTCV-006, Revision A-04, dated June 16, 2017, or later FAA-accepted revision. Operated in accordance with Pilot Operating Handbook and Airplane Flight Manual Supplement, Report No. HTCV-007, Revision IR, dated July 17, 2017, or later FAA-approved revision. Limitations and Conditions: 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 series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. Date of application: October 7, 2016 Date reissued: Date of issuance: July 24, 2017 Date amended: (Signature) Manager, Seattle Aircraft Certification Office (Title) Un i te d St ate s of Am e ri ca Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02548SE Hood Tech Corp. Vision, Inc. Issued: July 24, 2017 Reissued: Amended: A copy of this certificate, Report No. HTCV-006, Revision A-04, dated June 16, 2017, or later FAA-accepted revision, and Report No. HTCV-007, Revision IR, dated July 17, 2017, or later FAA-approved revision must be maintained as part of the permanent records for the modified aircraft. 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. Certification Basis: Part 23 of the Federal Aviation Regulations (FAR) effective December 18, 1964, as amended by 23-1 through 23-55 and FAR 36 as amended on the date of certification. Application for type certificate, dated August 28, 2002. - END - **FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES** ## Every issue (1) - July 24, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d0/bc/d0bc5bed514e91b007f5f8e0a660711e7ff7be9952520abc4abfdaf3b21e17b7) --- 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.