STC ST04442CH

ST04442CH Apcela IFC JV, LLC dba Apcela ATG 1900 Reston Metro Plaza, Suite 615 Reston, VA 20190 Part 23 the Title 14, Code of Federal Regulations A24CE Textron Aviation Inc.

200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, 300, 300LW, B300, B300C

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

(See Continuation Sheet 3 of 4) 02/24/2020 11/05/2025 03/26/2020 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4 Installation of SmartSky LiTE System in accordance with Liberty Partners Inc. Master Data List, Doc. No. LP3931-1002, Revision A, dated March 25, 2020, or later FAA approved revision.

FAA 8110-2 ( 10/24) Page 2 of __

ST04442CH 11/05/2025 4

ST04442CH 11/05/2025 Limitations and Conditions (Continued):

2) FAA Approved Airplane Flight Manual Supplement, Liberty Partners Inc. Doc. No.

LP3931-2002, Revision IR, approved March 26, 2020, or later FAA approved revision is required on board the modified aircraft.

3) FAA Approved Instructions for Continued Airworthiness - Airworthiness Limitations, Section 14, of Liberty Partners Inc. Doc. No. LP3931-2001, Revision IR, approved March 26, 2020, or later FAA approved revision is a required part of this STC.

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

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 Textron Aviation Inc. 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, 300, 300LW, B300 and B300C aircraft is as follows:

a. The type certification basis for the Textron Aviation Inc. 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, 300, 300LW, B300 and B300C aircraft is shown on TCDS A24CE for parts not changed or affected by the change.

b. This certification basis for parts changed or affected by the change since the reference date of application is based upon TCDS A24CE. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in Order 8110.48, the certification basis for this modification was determined to be:

ST04442CH 11/05/2025 Certification Basis (Continued):

Applicable regulations at the latest amendment 23-0 through 23-34 §23.29(a)(b) §23.603(a)(b) §23.627 §23.1431 §23.301(a)(b) §23.605(a) §23.867(a)(b)(c) §23.1501(a)(b) §23.303 §23.607 §23.1301(a)(b)(c)(d) §23.1529 §23.305(a)(b) §23.609(a)(b) §23.1307(b)(3) §23.1581(a)(b) §23.307(a) §23.611 §23.1309(a)(b)(c)(d) §23.1585(a) §23.341 §23.613(a)(b)(c) §23.1351(a)(2) §23.365(a)(b)(c)(d) §23.615(a)(c) §23.1357(a)(c) §23.561(a)(b)(c)(d)(e) §23.619 §23.1365(a)(b) §23.601 §23.625(a)(b)(c) §23.1367(a)(b)(c)(d)

Applicable 14 CFR Part 23 regulations at other amendment levels

§23.571(c) [Amdt 23-62]*; §23.573(b)[Amdt 23-48]; §23.574(a)[Amdt 23-48]**; §23.575 [Amdt 23-48]; §23.1359(c)[Amdt 23-49]

* §23.571(c) applies only to Normal Category models (all models except B300 and B300C)

** §23.574(a) applies only to Commuter Category models (B300 and B300C)

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