STC SA02654SE

United States of America Department of Transportation p eaera[ JI viation ;zl_aministration Supplemental Type Certificate :J{um6er: SA02654SE CJ'liis certificate issuea to: AeroMech Incorporated 1604 Hewitt Avenue; Suite 505 Everett, WA 98201 certifies tliat tlie cliange in tlie type aesign for tlie foffowing proauct witli tlie fimitations ana conditions tlierefore as specifieali ereon meets tlie airwortliiness requirements of Part E.__of tlie Federal Aviation Regulations.

Original Product - Type Certificate Number: Make: Piper Aircraft Inc.

A25SO PA-46-500TP, P A-46-600TP Description of Type Design Change:

Group Reduced Vertical Separation Minimum (RVSM) airworthiness approval in accordance with Master Data List AM0325-DL02-00, Revision"-", dated 20 September 2019 (or later FAA-approved revision).

Description of Type Design Change: Continued on Page 3 of 4) Limitations aJ1d Conditions:

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

If the holder agrees to permit another person to use this certificate, the holder must give the other person written evidence of that permission.

CJ'liis certificate ana tlie supporting aata wliicli is tlie 6asis for appmva{ sha{{ remain in effect unti{ surrenaerea, suspencfea, ana revof?Ja or a termination aate is otherwise esta6Cishea 6y the Jiaministrator of the Pecfera{Jiviation )Iaministration.

Date of Application: 11 December 2018 Date Reissued:

Date of Issuance: 20 September 2019 Date Amended:

By Direction of the Administrator 'Iit[e Brian P. Smith ODA Administrator ODA-635882-NM AeroMech Incorporated Everett, WA

FAA Form 8110-2 (5/14) Page 1 of 4

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

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

FAA Form 8110-2 (5/14) Page 2 of 4

United States of America Department of Transportation ZOMINISTREI Supplemental Type Certificate Federal Aviation Administration (Continuation Sheet) Number: SA02654SE Description of Type Design Change: Continued:

Class 1 airframes must be maintained in accordance with the Instructions for Initial and Continued Airworthiness document AM0325-IC01-01, Rev. —, dated 20 September 2019 (or later FAA accepted revision) and is a required part of this STC. The Airplane Flight Manual Supplement (AFMS) for the Class 1 airframes, document AM0325-FM01-01, Rev. —, FAA approved 16 September 2019 (or later FAA approved revision) is required on board for operation of these aircraft.

Class 2 airframes must be maintained in accordance with the Instructions for Initial and Continued Airworthiness document AM0325-IC01-02, Rev. —, dated 20 September 2019 (or later FAA accepted revision) and is a required part of this STC. The Airplane Flight Manual Supplement (AFMS) for the Class 2 airframes, document AM0325-FM01-02, Rev. —, FAA approved 16 September 2019 (or later FAA approved revision) is required on board for operation of these aircraft.

Class 3 airframes must be maintained in accordance with the Instructions for Initial and Continued Airworthiness document АМ0325-IC01-03, Rev. —, dated 20 September 2019 (or later FAA accepted revision) and is a required part of this STC. The Airplane Flight Manual Supplement (AFMS) for the Class 3 airframes, document AM0325-FM01-03, Rev. —, FAA approved 16 September 2019 (or later FAA approved revision) is required on board for operation of these aircraft.

Class 4 airframes must be maintained in accordance with the Instructions for Initial and Continued Airworthiness document AM0325-IC01-04, Rev. —, dated 20 September 2019 (or later FAA accepted revision) and is a required part of this STC. The Airplane Flight Manual Supplement (AFMS) for the Class 4 airframes, document AM0325-FM01-04, Rev. —, FAA approved 16 September 2019 (or later FAA approved revision) is required on board for operation of these aircraft.

Class 5 airframes must be maintained in accordance with the Instructions for Initial and Continued Airworthiness document AM0325-IC01-05, Rev. —, dated 20 September 2019 (or later FAA accepted revision) and is a required part of this STC. The Airplane Flight Manual Supplement (AFMS) for the Class 5 airframes, document AM0325-FM01-05, Rev. —, FAA approved 16 September 2019 (or later FAA approved revision) is required on board for operation of these aircraft.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changed aeronautical products in FAA Order 8110.48, the type certification basis for the RVSM approval is as follows:

(Certification Basis Continued on Page 4 of 4)

FAA Form 8110-2 (5/14) Page 3 of 4

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02654SE Certification Basis Continued:

1. The type certification basis for Piper PA-46-500TP & PA-46-600TP airplanes is shown on TCDS A25SO for parts not changed or affected by this approval.

2. The certification basis for this change, since the reference date of application, December 11, 2018, is based on 14 CFR part 23 as amended by Amendment 23-64.

Regulations complied with through Amendment 23-64:

14 CFR §§23.1529, 23.2500(a), 23.2505, 23.2620 -END-

FAA Form 8110-2 (5/14) Page 4 of 4