STC SA02233LA

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA02233LA This certificate issued to:

Innovative Solutions & Support, Inc.

1500 District Avenue Burlington, MA 01803 Part 23 of the Federal; Aviation Regulations.

Original Product - Type Certificate Number: A78EU Make: Pilatus Model: PC-12, PC-12/45, PC-12/47 Description of Type Design Change:

Reduced Vertical Separation Minimum (RVSM) Compliant Aircraft (design satisfies RVSM performance requirements, Group Aircraft) in accordance with the inspection criteria of Innovative Solutions & Support Instructions for Continued Airworthiness (ICA), Document number F TA-IS- 001008, Rev 2, dated April 05, 2017, or later FAA approved revision.

1. Operation must be in accordance with Innovative Solutions & Support Aircraft Flight Manual 20PP, crater FAA apDoved ret simber FTA-IS-001009, Rev 1, FAA approved on June 01, The AFMS must be carried in the aircraft during all flights.

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Date of Application: March 23, 2009 Date Reissued: June 10, 2009 Date of Issuance: March 27, 2009 Date Amended: June 01, 2017 By Direction of the Administrator Signature Thomas Boudreau Acting Manager, Boston Aircraft Certification Office Title This

FAA Form 8110-2 (5/14) Page 1 of 3

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number._ To (Name and address of transferee) Make:

Address (Number and Street, City, State, and ZIP Code):

From (Name and address of grantor) Make:

Address (Number and Street, City, State, and ZIP Code):

Date of Transfer.

This The ST's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02233LA Limitations and Conditions: (continued from Page 1 of 3)

2. Either FAA STC SA02255NY or FAA STC SA00381BO is a prerequisite or concurrent requirement for this STC.

3. Any revisions to Innovative Solutions & Support part number 9B-81070-5 Air Data Module (ADM) Static Source Error Correction (SSEC) curve, as installed by either FAA STC SA02255NY or by FAA STC SA00381BO, results in this STC being invalid.

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

Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Pilatus PC-12, PC-12/45, PC- 12/47 aircraft is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A78EU.

b. The modification certification basis for parts changed or affected by the change since the reference application date, March 23, 2009, is based upon part 23 as amended by Amendment 23-57 as follows:

Regulations at the latest amendment 23-0 through 23-57 Not Captured.

Regulations at an intermediate amendment Not Captured.

Regulations at the amendment level in TCDS A78EU Not Captured.

-END- This The ST's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder.

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