STC SA00102MC

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00102MC This certificate issued to: Sierra Nevada Corporation 12500 E. Belford Ave.

Englewood, CO 80112 Part 23 of the Chapter 14 Code of Federal Regulations Original Product – Type Certificate Number: Make: Pilatus Aircraft Ltd.

A78EU PC-12/47E Description of Type Design Change:

Installation of multiple mission configuration options, including an equipment rack, non-required communications equipment, mission power distribution system, antennas, optional sensor, optional operator console, optional casualty evacuation configuration, replacement of cockpit mounted audio control panels, and addition of audio control panels in the cabin. Data required includes:

(Continued on page 3) Limitations and Conditions:

1) Compatibility of this design change with previously approved modifications must 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.

(Continued on page 3)

Date of Application: February 22, 2013 Date Reissued: February 27, 2017 Date of Issuance: December 12, 2013 Date Amended: August 15, 2014; August 17, 2015; November 30, 2022 By Direction of the Administrator Signature Title William Eckler ODA administrator, ODA-833355-CE 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 4

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

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 4

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00102MC Description of Type Design Change (continued from page 1):

1) Sierra Nevada Corporation (SNC), Master Data List (MDL) MDL-0232-00-9319, Revision D, Dated: 12/05/2013 or later FAA approved revisions

2) Sierra Nevada Corporation (SNC), Aircraft Flight Manual Supplement (AFMS) 0232-00-9308, Revision B, Dated: 12/12/2013 or later FAA approved revisions

3) Sierra Nevada Corporation (SNC), Configuration Conversion Manual (CCM) 0232-00-9513, Revision B, Dated: 11/01/2013 or later FAA approved revisions

4) Sierra Nevada Corporation (SNC), Instructions for Continued Airworthiness (ICA) 0232-00-9345, Revision C, Dated: 6/17/2014 or later FAA accepted revisions

5) Sierra Nevada Corporation (SNC), Illustrated Parts Catalog (IPC) 0232-00-9350, Revision B, Dated: 10/23/2013 or later FAA accepted revisions

6) Sierra Nevada Corporation (SNC), Wiring Diagram Manual Supplement 0232-00-9351, Revision B, Dated: 10/24/2013 or later FAA accepted revisions Limitations and Conditions (continued from page 1):

3) Approval of this change in type design applies to the above model of airplane only.

4) A copy of this certificate and the ICAs shall be maintained in the airplane permanent records.

5) Supplemental Type Certificate (STC) SA00634DE must be installed as a prerequisite for this STC installation.

6) This STC is intended for military, public, or government use aircraft only. Installation of this system on aircraft for civil use is prohibited.

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 4

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00102MC 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 Pilatus Model PC-12/47E Multi Mission Configurations is as follows:

a. The type certification basis for Pilatus PC-12/47E is shown on A78EU for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of the original STC application, 02/22/2013 and amendment applications, 04/29/2014 and 4/27/2015, is based upon 14 CFR Part 23 as amended by Amendment 23-42 and additional selected rules at later amendments as listed on the TCDS. Based on 14 CFR 21.115 and § 21.101, and the FAA policy for significant changes in the FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 23-0 through 23-62:

23.305(b) [Amdt. 23-45], 23.573(b) [Amdt. 23- 48], 23.575 [Amdt. 23-48], 23.607(a)(b) [Amdt. 23-48], 23.1306(a)(b) [Amdt. 23-61],

23.1308(b)(c) [Amdt. 23-57], 23.1322(a)(b)(c)(d) [Amdt. 23-43], 23.1351(a)(b)(1)(i) [Amdt. 23-49], 23.1357(b)(c) [Amdt. 23-43],

23.1365(a) [Amdt. 23-49] Regulations at the amendment level in TCDS A78EU:

23.21 [Amdt. 23-0], 23.23 [Amdt. 23-17], 23.25 [Amdt. 23-34], 23.29 [Amdt. 23-21], 23.45(a)(b)(c)(e) [Amdt. 23-34], 23.49 [Amdt.

23-21], 23.49(a)(b)(1)(c)(d)(f)(2) [Amdt. 23-44], 23.51(a)(c) [Amdt. 23-34], 23.53(b)(2) [Amdt. 23-34], 23.65 (a)(c) [Amdt. 23-34], 23.75

(a)(b)(c)(d)(e)(f)(g) [Amdt. 23-42], 23.77(a)(b) [Amdt. 23-34], 23.233(a) [Amdt. 23-0], 23.251 [Amdt. 23-0], 23.301 [Amdt. 23-48],

23.303 [Amdt. 23-0], 23.305(a) [Amdt. 23-45], 23.307 (a)(b) [Amdt. 23-0], 23.321 [Amdt. 23-0], 23.331 [Amdt. 23-42], 23.333 [Amdt.

23-34], 23.335(a)(b)(c) [Amdt. 23-48], 23.337 [Amdt. 23-34], 23.341(b) [Amdt. 23-42], 23.347 [Amdt. 23-0], 23.365 [Amdt. 23-0],

23.421 [Amdt. 23-42], 23.423 [Amdt. 23-42], 23.425 [Amdt. 23-42], 23.441 [Amdt. 23-42], 23.443 [Amdt. 23-42], 23.471 [Amdt.

23-0], 23.473 [Amdt. 23-28], 23.477 [Amdt. 23-0], 23.479(a) [Amdt. 23-17], 23.479(b)(c) [Amdt. 23-45], 23.481 [Amdt. 23-0], 23.483 [Amdt. 23-0], 23.561(a)(b)(1)(c)(1)(2)(e) [Amdt. 23-36], 23.561(b)(2)(3)(c)(3) [Amdt. 23-48], 23.562(c)(5) [Amdt. 23-36], 23.562 (d)(1) [Amdt. 23-50], 23.571(a) [Amdt. 23-45], 23.572 [Amdt. 23-45], 23.601 [Amdt. 23-0], 23.603 [Amdt. 23-23], 23.605(a) [Amdt. 23-23],

23.607(c) [Amdt. 23-48], 23.609 [Amdt. 23-0], 23.611 [Amdt. 23-7], 23.613 [Amdt. 23-45], 23.615(a) [Amdt. 23-7], 23.619 [Amdt.

23-7], 23.623(a) [Amdt. 23-7], 23.625 [Amdt. 23-7], 23.627 [Amdt. 23-0], 23.771(a) [Amdt. 23-14], 23.773(a)(1)(2) [Amdt. 23-45],

23.777 (a)(b) [Amdt. 23-33], 23.785(a)(1)(b)(i)(m)(n)(3) [Amdt. 23-36], 23.807(b)(1) [Amdt. 23-36], 23.853(a) [Amdt. 23-34], 23.867(a)

(b)(1)(2) [Amdt. 23-7], 23.1301 [Amdt. 23-20], 23.1323(b) [Amdt. 23-42], 23.1325(e) [Amdt. 23-42], 23.1351(a)(b)(1)(i) [Amdt. 23-34],

23.1351(g) [Amdt. 23-49], 23.1353(h) [Amdt. 23-49], 23.1357(a) [Amdt. 23-43], 23.1359(a)(c) [Amdt. 23-49], 23.1365(b)(c)(d)(e)(f) [Amdt. 23-49], 23.1367 [Amdt. 23-0], 23.1381 [Amdt. 23-0], 23.1419(b) [Amdt. 23-14], 23.1431(a)(b) [Amdt. 23-49], 23.1441 [Amdt.

23-9], 23.1443(a)(3) [Amdt. 23-43], 23.1447(a)(c)(d) [Amdt. 23-30], 23.1457(a)(1)(3)(4)(5)(c) [Amdt. 23-35], 23.1501 [Amdt. 23-21],

23.1524 [Amdt. 23-10], 23.1529 [Amdt. 23-26], 23.1541(a)(b) [Amdt. 23-21], 23.1557(a) [Amdt. 23-23], 23.1581(a)(b)(d) [Amdt.

23-34], 23.1583(d)(h)(l) [Amdt. 23-34], 23.1585(a) [Amdt. 23-34], 23.1587(a)(1)(2)(3)(4)(5)(6)(7)(8) [Amdt. 23-34], 23.1589 [Amdt.

23-13] Regulations at an intermediate amendment:

23.571(b)(c) [Amdt. 23-45], 23.1309(a)(b)(c)(1)(e) [Amdt. 23-49], 23.1555(a) [Amdt. 23-50] 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 4 of 4