STC SA01050DE

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___

Part of .

SA01050DE Concorde Battery Corporation 2009 W San Bernardino Road West Covina, CA 91790 23 Federal Aviation Regulations A25SO Piper Aircraft Inc.

PA-46-500TP, PA-46-600TP Installation of aircraft main battery replacement with Concorde valve regulated Lead-Acid battery in accordance with Document No.

5-0691, Master Drawing List, Piper M500 & M600 Battery Upgrade, Revision NC dated 6/11/20, FAA approved 7/3/2020 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. 5-0693, Revision NC dated 6/11/20, FAA Accepted 7/3/2020, 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 modifications.

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.

01/06/2020 07/03/2020 Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC ODA ODA No. ODA(AIR)-833887-NM 3

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___

SA01050DE SA01050DE 3

SA01050DE 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 Piper PA-46-500TP and PA-46-600TP Concorde valve regulated Lead-Acid battery installation is as follows:

a. The type certification basis for Piper PA-46-500TP and PA-46-600TP airplane is shown on TCDS A25SO 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, January 6, 2020, is based upon 14 CFR Part 23 as amended by amendment 23-25 effective March 6, 1980 & amendment 23-62 effective January 31, 2012, 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 23-62):

14 CFR Sections: 23.301 Amdt. 23-48; 23.303 Amdt. - ; 23.305 Amdt. 23-45; 23.307 (a,b) Amdt. - ; 23.337(a,b) Amdt. 23-48; 23.341(a,c) Amdt. 23-48; 23.601 Amdt. - ;

23.603 Amdt. 23-23; 23.605(a) Amdt. 23-23; 23.609 Amdt. - ; 23.611 Amdt. 23-48;

23.613 Amdt. 23-45; 23.619 Amdt. 23-7; 23.625(a-c) Amdt. 23-7; 23.1301 Amdt. 23-62;

23.1309(a) Amdt. 23-62; 23.1309(c) Amdt. 23-62; 23.1351(a)(1,2)(g) Amdt. 23-49;

23.1351(b)(1)(i) Amdt. 23-49; 23.1351(b)(1)(ii-iii)(2,3) Amdt. 23-49; 23.1353(a-e,h) Amdt. 23-62; 23.1529 Amdt. 23-26

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