STC SA01072DE

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:

SA01072DE Pilatus Business Aircraft, LTD.

12300 Pilatus Way Broomfield, CO 80021 Part 23 Title 14, Code of Federal Regulations A00072CE Pilatus PC-24 Airtext system installation in accordance with FAA approved Installation Master Document List, Airtext for the PC-24, 24-2001-01-0000, Revision A, dated February 7, 2022, or later FAA approved revision.

Instructions for Continued Airworthiness (ICA), Airtext Installation, 24-2001-64-0000, Revision A, dated September 21, 2021, or later FAA accepted revision is required for this installation.

Operation must be in accordance with Airplane Flight Manual Supplement, 24-2001-65-0000, Revision IR, dated October 29, 2021, or later FAA approved revision.

1. Approval of this change in type design applies to the model of aircraft listed above only.

2. This STC is applicable to all serial numbers for this Make/Model.

(see Continuation Sheet 3) July 24, 2020 April 6, 2022 for: Stacey Klein, Acting Manager Denver ACO Branch 3

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:

SA01072DE 3

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:

SA01072DE Limitations and Conditions Continued:

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

4. 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.

5. A copy of this certificate and the appropriate Flight Manual Supplement as listed above must be maintained as a part of the permanent record for the altered aircraft.

6. Certification Basis:

For components and areas not affected by the change, the original certification basis as shown on TCDS A00072CE, Revision 4.

For components and areas affected by the change, based on Title 14, Code of Federal Regulations Sections 21.115 and 21.101, and FAA Order 8110.48, the type certification basis due to this modification is the original certification basis for the Model Pilatus PC-24 shown on TCDS A00072CE, Revision 4, plus 14 CFR Part 23 effective December 18, 1964, including Amendments 23-1 through 23-62 as follows:

§§ 23.301(a) at 23-48, 23.303 at 23-0, 23.305 at 23-45, 23.307(a) at 23-0, 23.561(b)(3)

(e) at 23-62, 23.601 at 23-0, 23.603(a) at 23-23, 23.605(a) at 23-23, 23.607 at 23-48,

23.609 at 23-0, 23.611 at 23-48, 23.613(a)(b) at 23-45, 23.619 at 23-7, 23.625(a)(b)(c) at 23-7, 23.771(a) at 23-14, 23.773(a)(1)(2) at 23-45C, 23.853(a)(d)(3)(ii) at 23-62,

23.1301 at 23-62, 23.1309(a)(c) at 23-62, 23.1322(d)(e) at 23-43, 23.1351(a)(1)(2)(ii) at

23.49, 23.1357(a) at 23-43, 23.1359(c) at 23-49, 23.1361(a) at 23-49, 23.1365(a)(b)(d)

(e)(f) at 23-49, 23.1367(a)(b)(d) at 23-0, 23.1381(a)(b) at 23-0, 23.1431(a)(b)(e) at 23-62, 23.1529 at 23-26, 23.1581(a)(b)(f) at 23-50, 23.1583(h)(m) at 23-62, 23.1585(a)

(j) at 23-62, 23.1589(a) at 23-50.

Regulations at a later amendment than specified in TCDS A00072CE, Revision 4:

None.

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