# STC SA00959DE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Concorde Battery Corporation, United States - Description: Installation of Concorde valve regulated Lead-Acid batteries in replacement of aircraft main batteries - Applied: February 7, 2019 - Status date: May 1, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A60CE](https://openairdocs.org/tcds/A60CE) - Certificate PDF: https://openairdocs.org/files/sha256/ac/9a/ac9a82af590af4844762f6253a6c80f6a7c51ac9dff7eaf2e6e820a3f6dc82f4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F6A13650174801CE862585CA004600CA.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00959DE ## ADs that name it (0) None. ## Approved models (1) - Embraer S.A. EMB-505 ([TCDS A60CE](https://openairdocs.org/tcds/A60CE)) ## 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. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00959DE This certificate and the supporting data which is the bases for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of Application: February 7, 2019 Date Reissued: Date of Issuance: May 1, 2019 Date Amended: Signature Title Kreg R. Voorhies ODA Administrator, Cert Works ODA(AIR)-833887-NM . The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. FAA Form 8110-2 (5/14) Page 1 of 3 This certificate, issued to: Concorde Battery Corporation 2009 W San Bernardino Road West Covina, CA 91790 Part 23 of the Federal Aviation Regulations. Original Product - Type Certificate Number: A60CE Make: Embraer S. A. Model: EMB-505 Description of the Type Design Change: Installation of Concorde valve regulated Lead-Acid batteries in replacement of aircraft main batteries in accordance with Document No. 5-0676, Master Drawing List, Embraer 505 Battery Upgrade, Revision NC dated 3/21/19, FAA approved 4/30/2019 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. 5-0678, Revision NC dated 3/21/2019, FAA Accepted 4/29/2019, or later FAA accepted revision are required to be made available at installation. An FAA Approved Airplane Flight Manual Supplement is not required for this modification. 1. The installer must determine whether this design change is compatible with previously approved modificat ions. 2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. (Certification Basis on page 3 of 3) . The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number: SA00959DE To (Name and address of transferee) From (Name and address of grantor) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00959DE Date of Issuance: May 1, 2019 FAA Form 8110-2 (5/14) Page 3 of 3 Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Embraer S. A. EMB-505 Concorde valve regulated Lead-Acid battery installation is as follows: a. The type certification basis for Embraer S. A. EMB-505 airplane is shown on TCDS A60CE for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, April 3, 2018, is based upon 14 CFR Part 23, effective February 1, 1965 plus Amendments 23-1 through 23-57, plus additional amendment levels as defined per the TCDS. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: Regulations at the TCDS Certification Basis (Part 23, Amendments 23-1 through 23-57): 14 CFR Sections: 23.301 Amdt. 23-48; 23.303 Amdt. - ; 23.305(a,b) Amdt. 23-45; 23.307(a) Amdt. - ; 23.337(a,b) Amdt. 23-48; 23.341 Amdt. 23-48; 23.601 Amdt. - ; 23.603 Amdt. 23-23; 23.605 Amdt. 23-23; 23.609 Amdt. - ; 23.611 Amdt. 23-48; 23.613(a-d) Amdt. 23-45; 23.619 Amdt. 23-7; 23.625(a- 23.1351(a)(1)(2)(ii),(b)(1)(ii-iii)(2-4),(g) Amdt. 23-49; 23.1351(b)(1)(i) Amdt. 23-49; 23.1353(a-e),(h) Amdt. 23-49; 23.1529 Amdt. 23-26 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ## Every issue (1) - May 1, 2019: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ac/9a/ac9a82af590af4844762f6253a6c80f6a7c51ac9dff7eaf2e6e820a3f6dc82f4) --- 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.