# STC SA3499WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: DeVore Aviation Corporation of America, a New Mexico Corporation, United States - Description: Installation of tail flood lights on horizontal stabilizer. - Applied: September 6, 1977 - Status date: January 31, 2000 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A23CE](https://openairdocs.org/tcds/A23CE) - Certificate PDF: https://openairdocs.org/files/sha256/8c/ae/8cae978d95a190ffef6fdb55552472841e61321333e818a351f189d6f801c1f9 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3601364E68CF370786257DC4005EAB93.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA3499WE ## ADs that name it (0) None. ## Approved models (4) - Beechcraft Corporation 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Beechcraft Corporation 58PA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Beechcraft Corporation 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Beechcraft Corporation 58TCA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) ## 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: SA3499WE This certificate issued to: DeVore Aviation Corporation of America, a New Mexico Corporation 6104-B Jefferson, N.E. Albuquerque, NM 87109-3410 Part 23* of the Federal Aviation Negulation. *Certification basis is set forth in Type Certificate Data Sheet A23CE. Original Product Type Certificate Number : A23CE Make: Beech Model: 58P, 58PA, 58TC, 58TCA Description of Type Design Change: Installation of tail flood lights on horizontal stabilizer in accordance with DeVore Top Drawing 05500001, Revision E, dated September 1, 1977, or later FAA approved revisions. The approval of this change in type design applies to the Beech 58 aircraft 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 aircraft. This determination should include consideration of significant change in weight distribution such as an increase in the fixed disposable weight of the fuselage. Date of Application: September 06, 1977 Date Reissued: January 31, 2000 Date of Issuance: September 30, 1977 Date Amended: FEDERAL AVIATION By Direction of the Administrator Michel M Owler (Signature) Michele M. Owsley, Manager TOMINISTRATOS Airplane Certification Office, Southwest Region (Title) TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) - (Address of transferee) (Number and streel) (Cirj. Stake, and iIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and sireel ; (City, Stake, and ZIP code) Extent of Authority (if licensing agreement): Date of Transier:. Signature of grantor (In ink): + 11