STC SA01082DE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SA01082DENumber:

This certificate issued to: Pilatus Business Aircraft, LTD 12300 Pilatus Way Broomfield, CO 80021 BB__.

Make: Pilatus Aircraft Ltd.Original Product A00072CE7\SH&HUWLILFDWH1XPEHU Model: PC-24 Description of Type Design Change:

Installation of Cabin Power Outlets in accordance with Doc No. 24-2011-01-0000, Master Drawing List, PC-24 Cabin Utility Power, Issue C dated 6/22/2021, FAA approved 7/1/2021 or later FAA approved revisions. Doc No. 24-2011-64-0000, Instructions for Continued Airworthiness (ICA), Issue "-" dated 5/21/21, FAA accepted 7/1/2021 or later FAA accepted revision are required to be made available at installation. Doc No. 24-2011-65-0000, FAA Approved Flight Manual Supplement, Revision IR dated 4/15/2021, FAA approved 7/1/2021 or later FAA approved revision, is required for this installation.

1. This STC is applicable to all serial numbers for the Pilatus Aircraft Ltd. PC-24.

Continued Page 3 of 3

March 26, 2021Date of Application: Date Reissued:

Date of Issuance: July 2, 2021 Date Amended:

Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC ODA Title: ODA No. ODA(AIR)-833887-NM $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5   )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB 3

I United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SA01082DENumber:

Date oI transfer:

$Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&’s supporting documentation (drawings, instructions, SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5   )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01082DE Limitations and Conditions Continued:

2. The installer must determine whether this design change is compatible with previously approved modifications

3. 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:

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 Pilatus Aircraft Ltd PC-24 Cabin Power Outlets installation is as follows:

a. The type certification basis for Pilatus Aircraft Ltd PC-24 is shown on TCDS A00072CE 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, 3/26/2021 is based upon 14 CFR Part 23, effective February 1, 1965 plus Amendments 23-1 through 23-62. 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 latest amendment; None Regulations at an intermediate amendment; None Regulations at the amendment level in TCDS A00072CE;

14 CFR Sections: 23.23 Amdt. 23-45; 23.25 Amdt. 23-50; 23.301(a-c) Amdt. 23-48; 23.303 Amdt. - ;

23.305(a) Amdt. 23-45; 23.307(a) Amdt. - ; 23.337(a,b) Amdt. 23-48; 23.561(b)(3) Amdt. 23-62; 23.601 Amdt. - ; 23.603 Amdt. 23-23; 23.605 Amdt. 23-23; 23.609 Amdt. - ; 23.611 Amdt. 23-48; 23.613(a-c) Amdt. 23-45; 23.619 Amdt. 23-7; 23.625(a-c) Amdt. 23-7; 23.853(a)(d)(3)(i,ii,iv,v) Amdt. 23-62; 23.1301 Amdt. 23-62; 23.1309(a),(b),(c) Amdt. 23-62; Amdt. 23-62; 23.1351(a)(1)(2i), (b)(1) Amdt. 23-49;

23.1357(a,c) Amdt. 23-43; 23.1359(c) Amdt. 23-49; 23.1365(a),(b),(d),(e) Amdt. 23-49; 23.1529 Amdt.

23-26; 23.1557(e) Amdt. 23-45; 23.1581 Amdt. 23-34; 23.1585(j) Amdt. 23-62 End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