STC SA01905WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

EPPSAviation 1 Aviation Way Number: SA01905WI Atlanta, GA 30341 Part 23of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Pilatus Aircraft LTD.

A00072CE PC-24

Transmitting Portable Electronic Devices (T-PED) Aircraft Tolerance Testing:

1) 3SCertification, Master Data List (MDL) 3S18-029-1001, Revision IR, Dated: 04/01/2019 or later FAA approved revision.

2) 3SCertification, Instructions for Continued Airworthiness(ICA) 3S18-029-6101, Revision IR, Dated: 03/29/2019 or later FAA accepted revision.

1) Compatibility of this design change with previously approved modificationsmust be determined by the installer.

2) 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.

3) Approval of this change in type design appliesto the above model aircraft only.

4) A copy of this certificate and the ICA shall be maintained aspart of the permanent records for the modified airplane.

Date of Application: 11/09/2018

Date Reissued: 02/05/2020

Date of Issuance: 04/01/2019 Date Amended:

Signature

Title Ben Tyson Program Manager Wichita ACOBranch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA01905WI

To (Name and address of transferee)

From (Name and address of grantor)

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

(Continuation Sheet) Number: SA01905WI

Limitationsand Conditions (continuation) Certification Basis:

Based on 14 CFR§21.115 and §21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the applicable 14 CFRPart 23 aircraft affected isasfollows:

a. The type certification basisfor Pilatus Aircraft LTD. Model PC-24 isshown on A00072CEfor parts not changed or not affected by the change.

b. The certification basisfor partschanged or affected by the change since the reference data of application, 11/09/2018, is based upon 14 CFRPart 23 asamended by Amendment 23-62. Based on 14 CFR21.115, and the FAA policy for significant changes in the FAA order 8100.48A, the certification basisfor this modification wasdetermined to be:

Regulationsat the latest amendment 23-0 through 23-62:

23.1301(a)(b)(c) [Amdt. 23-62], 23.1309(a)(c) [Amdt. 23-62], 23.1431(b) [Amdt. 23-62], 23.1529 [Amdt. 23-26].

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