# STC SA360WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Aerotech Industries, Canada - Description: PAC Tradewind Modification -(Gross weight modification, empennage modification, installation of tricycle gear, windshield, outer wing fuel tanks, M-4 autopilot, Bendix RS10B fuel injection system, and optional R-985 APS4 engines). - Applied: January 3, 1994 - Status date: March 15, 1996 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A-765](https://openairdocs.org/tcds/A-765) - Certificate PDF: https://openairdocs.org/files/sha256/80/90/8090380fa73bfe34f5d1c75ceda4e71dfc2816dc70687c2be9e7f84a8c51a83f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EEE3CA3B1B8360C18625826E004A5F0C.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA360WE ## ADs that name it (1) - [AD 78-10-01](https://openairdocs.org/ad/78-10-01): Lower Rudder Torque Tube ยท United Aircraft of Canada Ltd. PT6 series engines (Staggerwing Museum Foundation STC SA1016WE or 2 others). Effective May 17, 1978. Named in the applicability ## Approved models (8) - Raytheon Aircraft Company C-45G ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company C-45H ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company D18C ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company D18S ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company JRB-6 ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company TC-45G ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company TC-45H ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company UC-45J (SNB-5) ([TCDS A-765](https://openairdocs.org/tcds/A-765)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 52360WE This certificate issued to: Aerotech Industries Ltd. Box 727 Campbell River B.C. V9W 6J3 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airvorthiness requirement's of Part 3 of the Civil Air Regulations Original Product - Type Certificate Number: A-765 Make: Beech Model: C45G, C45H, D18C, D18S, SNB5, TC45G, IC45 H, and JRB6 Description of Type Design Change: see Bage 3 Limitations and Conditions: See Page 3 Date of Application: January 3, 1994 Date of Issuance: August 23, 1994 TOMNISTRATO Date Reissued: Sept. 2, 1970 Jan. 9, 1975, March 15, 1996 Date Amended: Nov. 1, 1963, Sept. 24, 1964 By Direction of the Administrator (Signature) Manager, Technical and Administrative Support Staff, ANM-1031 (Title) FAA Form 8110-2-1(10-68) Page 1 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA360WE Date of Application: February 28, 1963 Date of Issuance: March 25, 1963 Date Amended: Nov. 1, 1963, Sept. 24, 1904 Date Reissued: Sept. 2, 1970, Jan. 9, 1975 March 15, 1996 Description of Type Design Change: PAC Tradewind Modification which consists of the following installations: Gross weight modification in accordance with STC SA4-1462. Modification of empennage as per Top Dwg. 450002. Tricycle gear installation in accordance with STC SAlllWE. Windshield installation as per STC SA4-1341. Outer wing fuel tanks as per STC SA4-569 as an optional installation. Installation of M-4 Autopilot as per Dwg. 452101 as an optional item. Installation of Bendix RS10B Fuel Injection System in accordance with STC SA4-1427 as an optional item. 8. Installation of optional R-985 APS4 Engines (P & W R985 AN14B modified per STC SE4-864). The approval of this change in type design applied basically to Beech Models C45G, C45H, D18C, D18S, SNB5, TC45G, and JRB6 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 by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that Provisions of STC's SA4-1462, SA111WE and SA4-1341 must be incorporated. Incorporation of previsions of STC SA4-569 and SA4-1427 are optional. Operational Limitations: PAC FAA Approved Airplane Flight Manual dated March 25, 1963, or subsequent revisions is required. END FAA Form 8110-1(10-69) Page 3 of 3 ## Every issue (1) - March 15, 1996: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/80/90/8090380fa73bfe34f5d1c75ceda4e71dfc2816dc70687c2be9e7f84a8c51a83f) --- 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.