# STC SA2353WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Staggerwing Museum Foundation Inc., United States - Description: Installation of cargo pod. - Applied: April 27, 1971 - Status date: September 3, 2004 - 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/sha256/0e/a7/0ea7695295404af4c520b8a80468741c699c7f4da93051e6f2b8f9cd32e86836 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A157A971A6F513C6862570CB0071141F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2353WE ## ADs that name it (0) None. ## Approved models (15) - Raytheon Aircraft Company 3N ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company 3NM ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company 3TM ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - 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 E18S ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company E18S-9700 ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company G18S ([TCDS A-765](https://openairdocs.org/tcds/A-765)) - Raytheon Aircraft Company H18 ([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 TC-45J ([TCDS A-765](https://openairdocs.org/tcds/A-765)) ## 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. This Certificate issued to Staggerwing Museum Foundation, Inc. 560 Old Shelbyville Highway Tullahoma, TN 37388 Part 03 of the Civil Air Regulations, effective November 13, 1945, and Part 3 of CAR effective November 1, 1949, as amended by 3-14. 765 BEECH D18C, D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), JRB-6, 3N, 3NM, 3TM Description of Type Design Change: Installation of cargo pod in accordance with FAA Sealed Hamilton Aircraft Co. Inc. Drawing List No. 786. (See Page 2) Date of application : April 27, 1971 Date of issuance : June 16, 1971 Date reissued: August 10, 1971; April 28, 1977; September 3, 2004 ( Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title) Number SA2353WE D a t e : April 28, 1977; September 3, 2004 S T C : SA2353WE BEECH D18C, D18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), JRB-6, 3N, 3NM, 3TM **SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA2353WE** Aircraft must incorporate the provisions of STC SA1016WE, conventional landing gear (tail wheel type), and Pratt and Whitney PT6A-20 engines. Aircraft must also incorporate a wing lower spar reinforcement equivalent to the provisions of STC SA2000WE. The cargo pod is limited to a maximum load of 1,000 lbs. (See FAA approved AFM Supplement, Hamilton Aviation Co. Document No. D-127, to ATECO Basic Flight Manual No. 900-A). The approval of this change in type design applies basically to the models listed only. 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 interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. 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 - ## Every issue (1) - September 3, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0e/a7/0ea7695295404af4c520b8a80468741c699c7f4da93051e6f2b8f9cd32e86836) --- 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.