STC SA01834WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the

Signature

Title Cutter Aviation, Inc 2802 E. Old Tower Road Phoenix, AZ 85034 3 SA01834WI Federal Aviation Regulations.23 Installation of a modified Climate Control System. Data required:

1. Aeronautix Master Data List, No. 15-007-SC4302, Rev 0, dated February 16, 2017, and

2. Aeronautix Airplane Flight Manual Supplement, No. 15-007-FT2901, Rev. 1, dated March 7, 2017, or

3. Aeronautix Airplane Flight Manual Supplement, No. 15-007-FT2902 or No. 15-007-FT2903, Rev. 0, dated October 1, 2018, or later FAA Approved revision to 1, 2 or 3.

Compatibility of this design change with previously approved modifications must be determined by the installer.

Piper PA-46-350P, PA-46R-350T, PA-46-500TP June 28, 2022 October 24, 2018 October 26, 2015 April 4, 2017 A25SO Grant Youngdahl Program Manager Wichita ACO Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

3 SA01834WI

This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

FAA Form 8110-2 (5/14) Page 3 of

3 Reissued: June 28, 2022

Certification Basis:

In accordance with 14 CFR 21.101(b) and the criteria specified in FAA AC 21.101-1B and FAA Order 8110-48, this design change does not constitute a substantial or significant change and is therefore “Non-Significant” and meets the criteria for earlier requirements equivalent to the existing certification basis. The certification basis for this modification is as follows:

1. Areas not changed or not affected by this modification: Regulations not affected by this modification remain as specified by TCDS A25SO.

2. Regulations at Amendment 23-0 through 23-62. The following rules are affected by this modification with a regulatory basis of 14 CFR Part 23, effective February 1, 1965, as amended by Amendment 23-62, effective January 31, 2012:

23.1; 23.29(a)(b); 23.301(a); 23.303; 23.305; 23.307(a); 23.337(a)(1)(b)(1); 23.341(a)(c); 23.561(a)(b)(3)(e); 23.601; 23.603(a)(1)(2)(3)

(b); 23.605(a); 23.607(a)(b)(c); 23.609(a)(b); 23.611; 23.613(a)(b)(c)(d); 23.619(a); 23.625(a)(b)(c); 23.771(a); 23.773(a)(1)(2)(b);

23.831(b); 23.841(a); 23.1181(b); 23.1183(b); 23.1191(c)(h); 23.1301(a)(b)(c); 23.1306; 23.1308; 23.1309(a)(1)(2)(b)(c)(d); 23.1310;

23.1311(a)(2)(3)(4)(c); 23.1322(a)(b)(c)(d)(e); 23.1351(a)(1)(2)(i)(b)(1)(i)(ii)(iii); 23.1357(a); 23.1359(a)(c); 23.1365(a)(b)(d)(e)(f);

23.1367(a)(b)(c)(d); 23.1381(a)(b); 23.1431(a)(b); 23.1438(b); 23.1461; 23.1529; 23.1581(a)(b)(1)(3)(c)(f); 23.1583(m); 23.1585(a)(b)

3. Regulations at Amendment 23-0 through 23-49. The following rules are affected by this modification with a regulatory basis of 14 CFR Part 23, effective February 1, 1965, as amended by Amendment 23-49, effective March 11, 1996: 23.1353(h) for PA-46-350P Serial Numbers 4636375 and Up, PA-46-350T, and PA-46-500TP aircraft models.

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