STC SA01820WI

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 Aeronautix, LLC 3450 N. Rock Road, Suite 300 Wichita, KS 67226 3 SA01820WI Civil Air Regulations.3* Installation of a Lycoming IO-540-K1G5 Engine. Data required:

1. Aeronautix Master Data List (MDL), Document No. 16-001-SC4302, Rev. 1, dated September 21, 2016; and

2. Aeronautix Airplane Flight Manual Supplement (AFMS), Document No. 16-001-FT2901, Rev. 1, dated October 3, 2016, or later FAA Approved revision to (1) or (2).

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

2. Compatible with FAA STC SA433CH, Installation of a McCauley Propeller Model B3D36C427/82NGA-2.

3. Compatible with FAA STC SA00953AT, Installation of a composite mod comp engine cowling with cowl flaps.

Piper PA-32R-300, PA-32RT-300, PA-32R-301(SP) June 28, 2022March 22, 2016 October 12, 2016 A3SO 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 SA01820WI

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: (continued from page 1) Based on 14 CFR §§ 21.101 and 21.115, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for FAA STC, SA01820WI, is as follows:

1. The type certification basis for areas not changed or not affected by the this modification is shown on TCDS A3SO.

2. The type certification basis for areas changed or affected by this modification since the date of application was determined to be:

a. Regulations at the latest amendment: N/A.

b. Regulations at the intermediate amendment: N/A.

c. Regulations at the amendment level in the applicable TCDS:

i) Civil Air Regulations (CAR), Part 3, effective May 15, 1956, through Amendment 3-8, effective December 18, 1962, sections:

3.0, 3.171, 3.195, 3.196, 3.385, 3.393, 3.411, 3.415, 3.416 - 3.418, 3.422, 3.429, 3.433, 3.435 - 3.437, 3.449, 3.550, 3.554,

3.561 - 3.567, 3.570, 3.576, 3.581, 3.651, 3.652, 3.655(d)(2), 3.735, 3.737, 3.744 - 3.748, 3.756, 3.759 - 3.761, 3.767(a)(b), 3.777,

3.778(b)(c)(d).

ii) 14 CFR 23.959 as amended by Amendment 23-7, effective September 14, 1969.

iii) 14 CFR 23.1529 as amended by Amendment 23-26, effective October 14, 1980.

iv) 14 CFR 23.1581(b)(2) as amended by Amendment 23-21, effective March 1, 1978.

v) 14 CFR 23.1589 as amended by Amendment 23-13, effective October 23, 1972.

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