STC SA04188NY

This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title The STC’s supporting documentation (drawings, instructions , specifications, flight manual supplements, etc.) is the prop erty of the STC holder.

FAA Form 8110-2 (7/19) Page 1 of SA04188NY Lee Aerospace, Inc.

9323 E. 34th St. N.

Wichita, KS 67226 23 Federal Aviation Regulations.

A25SO Piper Aircraft, Inc.

PA-46-310P, PA-46-350P, PA-46-500TP, PA-46R-350T, PA-46-600TP, PA-46-701TP.

Installation of LAI CoolView Windshields and Windows in accordance with (1) Master Data List P46T-MDL-0067, Rev IR, dated 12/18/2019 or later FAA approved revision. (2) Instructions for Continued Airworthiness (ICA) P46T-ICA-0067, Rev IR, dated 12/17/2019, or later FAA accepted revision. The ICA and its contents must be incorporated into the operator's maintenance program.

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 the certificate to alter the product, the holder must give the other person written evidence of that permission.

11/20/2019 01/28/2020 05/05/202512/19/2019 ODA administrator, ODA-834634-NE 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate FAA Form 8110-2 (7/19) Page 2 of

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

Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an ai rcraft, aircraft engine, or propeller.

SA04188NY 3

FAA Form 8110-2 (7/19) Page of The STC’s supporting documentation (drawings, instructions, specifications, fl ight manual supplements, etc.) is the property of the STC hol der.

SA04188NY Date of Amendment: May 5, 2025 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 Aircraft Inc., Models PA-46-310P, PA-46-350P, PA-46-500TP, PA-46R-350T, PA-46-600TP and PA-46-701TP is as follows:

(1) The type certification basis for the Piper Aircraft Inc., Models PA-46-310P, PA-46-350P, PA-46-500TP, PA-46R-350T, PA-46-600TP and PA-46-701TP airplanes is shown on TCDS A25SO for parts not changed or not affected by the change.

(2) The certification basis for parts changed or affected by the change since the reference date of application November 20, 2019, is based upon Part 23 as amended by 23-1 through 23-25, with exception of those above 23-25 listed below.

Regulations at later amendments than the original certification:

14 CFR 23.301(a)(b) Amdt 23-48 14 CFR 23.305 Amdt 23-45 14 CFR 23.611 Amdt 23-48 14 CFR 23.773(a)(1)(2)(3)(b) Amdt 23-45 14 CFR 23.775(a)(b)(d)(e) Amdt 23-49 14 CFR 23.853(d)(3)(iv) Amdt 23-62 14 CFR 23.867 Amdt 23-49 14 CFR 23.1529 Amdt 23-26 ----------END---------- 3 3