STC SA00748DE

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

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

By Direction of the Administrator Signature Title 4 SA00748DE Textron Aviation, Inc One Cessna Boulevard Wichita, KS Federal Aviation Regulations.

23* Installation of the Rockwell Collins IDS-3000 System with new Primary Flight Displays, Multi-Function Display, Display Control Panels, Audio Panels and Engine Instrumentation. Also included: Integrated File Server System capability, XM Satellite Graphical Weather, Turbulence Weather Radar, WAAS/LPV capable GPS Receivers and standby instrument package. Data required: 1) FAA Approved Master Data List (MDL) Document No. 014-3110-L01-00, Revision 4, dated 9/17/2012, or later approved revisions; (continued on page 3).

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

2. Installation of the Rockwell Collins APS-65 Autopilot System must be previously accomplished.

3. A copy of this certificate and the ICA shall be maintained in the airplane permanent records.

4. Approval of this change in type design applies to the above mentioned airplane only.

Program Manager, Wichita ACO Branch Textron Aviation (Hawker Beechcraft) 1900D February 8, 2021 April 14, 2010 October 5, 2012 A24CE *it was determined that there is no acoustical change IAC with 21.93(b)(3)(iii) as a result of this modification.

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

To (Name and address of transferee)

From (Name and address of grantor)

4 SA00748DE

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

4 SA00748DE Description of Type Design Change (continued from page 1) data required:

2) FAA Approved Aircraft Flight Manual Supplement (AFMS) Document No's: 014-3110-A01-00 Revision 3, 14-3110-A02-00 Revision 2, 14-3110-A03-00 Revision 1 and 14-3110-A04-00 Revision 1, all dated 9/17/2012, or later approved revisions; and

3) Instructions for Continued Airworthiness (ICA) Document No's: 014-3110-C01-00 Revision 10, 014-3110-C02-00 Revision 7, 014-3110-C03-00 Revision 6, 014-3110-C04-00 Revision 6, all dated 5/10/2012, or later FAA Accepted revisions.

Certification Basis:

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 the Model 1900D IDS-3000 Cockpit Upgrade is as follows:

a. The type certification basis is shown on TCDS A24CE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the referenced date of the application is based upon Part 23 as amended by Amendment 23-57, the certification basis for this modification was determined to be:

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

Amendment 23-57 23-49 23-43 23-50 23-20 23-49 23-20 23-49 23-43 23-49 23-49 Orig Orig 23-43 23-21 Orig 23-26 23-21 23-50 23-45 23-50

Amendment 23-21 23-48 Orig 23-45 Orig 23-48 23-48 23-48 Orig 23-23 23-23 23-48 Orig 23-48 23-45 23-7 Orig 23-14 23-45 23-34 23-49 23-52 23-49

14 CFR Part

23.29

23.301(a)(b)

23.303

23.305(a)(b)

23.307

23.573(b)

23.574(a)

23.575

23.601

23.603

23.605(a)

23.607

23.609

23.611

23.613

23.625

23.627

23.771(a)

23.773(a)(2)

23.863

23.867

23.1305(a)(2-4)(c)(2)(5)(e)

23.1307

14 CFR Part

23.1308

23.1321(a-d)(5)(e)

23.1322

23.1325(b)(1)(2)(ii)

23.1327

23.1329(f-h)

23.1335

23.1351(a)(2)(ii)(b)

23.1357(a-d)

23.1359(a)(c)

23.1365(a)(b)(d)(e)

23.1367

23.1381

23.1441(a-c)

23.1501

23.1519

23.1529

23.1541(a)(b)

23.1543(c)

23.1549(a-c)

23.1581(a)

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

4 SA00748DE Regulations at the intermediate amendment:

Regulations at the amendment level in TCDS A24CE:

------ END -------

Amendment 23-51 23-49 23-49

23-49 23-43 23-49 23-49 23-50 23-50 23-50 23-50

Amendment 23-20

14 CFR Part

23.777(a)(b)

23.1303(a-c)(e-g)

23.1309(a)(1)(3)(4)(b)(c)

23.1311

23.1331

23.1353(a-e)(h)

23.1431(a)(b)

23.1545(a-c)

23.1555(a)

23.1583(h)

23.1585(j)

14 CFR Part

23.1301