# STC SR04007AT - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Concorde Battery Corporation, United States - Description: Replace original equipment Nickel-Cadmium (NiCd) or Concorde Lead-Acid main battery with higher capacity Concorde Lead-Acid, main battery on Agusta A119 and AW119 MKII rotorcraft and associated hardware - Applied: August 10, 2012 - Status date: July 28, 2021 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H7EU](https://openairdocs.org/tcds/H7EU) - Certificate PDF: https://openairdocs.org/files/sha256/fc/27/fc27594d8a6fdbfbb0c3b7960ca40b667ab6aa880afc7501a5ebd3337d96faf8 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DDDBCF87F63F90B286258727004C52D8.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR04007AT ## ADs that name it (0) None. ## Approved models (2) - Leonardo S.p.a. A119 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Leonardo S.p.a. AW119 MKII ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) ## 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. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR04007AT Concorde Battery Corporation 7905 Troon Cir SW Austell, GA 30168 Part 27 the Federal Aviation Regulations H7EU Agusta A119, AW119 MK II Replace Nickel-Cadmium (NiCd) battery with Lead-Acid, main battery on Agusta A119 and AW119 MK II rotorcraft and associated hardware in accordance with Master Drawing List 5-0465 Revision C, dated March 14, 2013 or later FAA approved drawing revisions. (See Continuation Sheet 3 of 4) August 10, 2012 July 28, 2021 May 22, 2013 (for)Christina Underwood, Manager Atlanta Aircraft Certification Office 4 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR04007AT FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR04007AT Limitations and Conditions - cont.: This approval should not be extended to other aircraft of this model on which other previously approved modification are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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. FAA Approved Rotorcraft Flight Manual Supplement for the Replace Nickel-Cadmium (NiCd) battery with Lead-Acid, main battery, 5-0466, revision NC, dated May 22, 2013 or later FAA approved revision is a required part of this STC. Instructions for Continued Airworthiness (ICA), Concorde Battery Corporation No. 5-0470, Rev. NC, dated October 23, 2012, or later FAA approved revision must be made available to the operator at the time of installation. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR04007AT 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 Agusta A119 and AW119 MK II series rotorcrafts is as follows: a. The type certification basis for the Agusta A119 and AW119 MK II rotorcraft is shown on TCDS H7EU 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, August 10, 2012, is based upon part 27 as amended by Amendment 27-47. 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 latest amendment 27-0 through 27-47 27.29, 27.33, 27.65, 27.71, 27.151, 27.161, 27.173, 27.307, 27.321, 27.337, 27.339, 27.351, 27.361, 27.391, 27.395, 27.397, 27.427, 27.501, 27.571, 27.602, 27.603, 27.613, 27.663, 27.672, 27.727, 27.779, 27.783, 27.807, 27.863, 27.917, 27.923, 27.955, 27.967, 27.975, 27.977, 27.997, 27.1027, 27.1041, 27.1043, 27.1045, 27.1141, 27.1143, 27.1145, 27.1193, 27.1327, 27.1337, 27.1411, 27.1501, 27.1525, 27.1545, 27.1547, 27.1559 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS H7EU None --------------------------END--------------------------- 4 4 ## Every issue (2) - July 28, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fc/27/fc27594d8a6fdbfbb0c3b7960ca40b667ab6aa880afc7501a5ebd3337d96faf8) - May 22, 2013: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/f6/9c/f69c0a84f094d0262184a3ab13ddec96a6a1ff46e1177eba1ddb5bdbd9f5a278) --- 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.