# STC SA2493WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Staggerwing Museum Foundation Inc., United States - Description: Installation of cockpit exterior door. - Applied: February 17, 1972 - Status date: September 3, 2004 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS A-765](https://openairdocs.org/tcds/A-765) - Certificate PDF: https://openairdocs.org/files/sha256/6c/47/6c477d1861c8cfd3643a7a630d2b06c3fe203d964c60523d170faefc24b0ad7c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/90294AA8C6BF2B2D862570C9006B7744.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2493WE ## ADs that name it (0) None. ## Approved models (4) - 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)) ## 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 13 November 1945 and Part 3 effective 1 November 1949 as amended by 3-14 (paragraph 3.242) (Normal Category). **SA2493WE BEECH E18S, E18S-9700, G18S, H18** Description of Type Design Change: Installation of Cockpit Exterior Door in accordance with FAA Sealed Hamilton Aircraft Company, Inc. Drawing No. 677-033. Limitations and Conditions: The approval of this change in type design applied basically to the Beech Models E18S, E18S-9700, G18S, and H18 aircraft 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. 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 Date of application : 10 February 1972 Date of issuance : 24 March 1972 Date reissued: April 28, 1977; September 3, 2004 ( Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title) ## Every issue (1) - September 3, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6c/47/6c477d1861c8cfd3643a7a630d2b06c3fe203d964c60523d170faefc24b0ad7c) --- 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.