STC SA00416BO

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SA00416BO Outerlink Corporation 150 Baker Avenue Ext., Suite 302 Concord, MA 01742-2199 Part 23 Title 14 Code of Federal Regulations A24CE Textron Aviation (Beechcraft) 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, B200GT, B200CGT, B300, B300C Installation of an Outerlink Satellite Communications System (Satcom) and Flight Data Monitoring System Kit B300/200-SAT-100 in accordance with Outerlink Master Drawing List (MDL) MDL300/200-SAT-100 Revision C, dated April 22, 2022, or later FAA approved revision.

1. Operation must be in accordance with Outerlink Aircraft Flight Manual Supplement (AFMS) Document FMSB300/200SAT001, Revision B, FAA approved on May 24, 2023, or later FAA approved revision.

(Limitations and Conditions continued on page 3) July 26, 2021 November 08, 2023, December 4, 2024 August 11, 2023 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4

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Too (Name and address of transferee):

Date oI transfer:

SA00416BO 4

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The AFMS must be carried in the aircraft during all flights.

2. Maintenance must be in accordance with Outerlink Instructions for Continued Airworthiness (ICA) Document No. ICA300/200SAT001, Rev. E, dated February 16, 2023, or later FAA accepted revision.

The ICA must be made available to the operator at the time of installation.

3. The Wireless Fidelity (WiFi) system does not include Portable Electronic Devices (PED) tolerance approval. Refer to FAA AC 91.21-1D to secure FAA operational approval of PEDs aboard aircraft.

Rockwell Collins Pro Line Fusion™ Avionics equipped aircraft Models B200GT, B200CGT and B300 have demonstrated tolerance for both transmitting and non-transmitting PEDs per Textron Engineering Test Report No. 300E701150, Rev. 4, dated August 10, 2015.

4. Compatibility of this design with previously approved modifications must be determined by the installer. Refer to FAA Advisory Circular (AC) 20-188.

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 Textron Aviation (Previous holder:

Beechcraft) Models 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, B200GT, B200CGT, B300, B300C aircraft is as follows:

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

b. The modification certification basis for parts changed or affected by the change since the reference application date, July 26, 2021, is based upon Part 23 as amended by Amendment 23-64 as follows:

(Certification Basis continued on page 4) 34

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Regulations at the latest amendment 23-64: None.

Regulations at an intermediate amendment level:

23.301 (23-48), 23.305(a) (23-45), 23.337 (23-48), 23.561(b)(3) (23-48), 23.571(a) (23-34 for 200 series only), 23.603 (23-23 for 200 series only), 23.605 (23-23 for 200 series only), 23.607 (23-48),

23.613(a)(b) (23-45), 23.771(a) (23-14 for 200 series only), 23.773(a)(1)(2) (23-45), 23.777(a)(b) (23-51),

23.867(a)(b)(1) (23-49), 23.1301 (23-20 for 200 series only), 23.1309(a)(b)(c)(d)(e) (23-49), 23.1321(e) (23-49), 23.1322(d)(e) (23-43), 23.1351(a) (23-49), 23.1357(a)(b)(c) (23-43), 23.1529 (23-26 for 200 series only), 23.1541 (for 200 series only), 23.1555(a) (23-50), 23.1581 (23-50), 23.1583 (23-50),

23.1585 (23-50), 23.1589 (23-13) (for 200 series only).

Regulations at the amendment level in TCDS A24CE:

23.303, 23.307(a), 23.365(a)(b)(d), 23.571(a), 23.601, 23.603 (for 300 series only), 23.605 (for 300 series only), 23.609, 23.611, 23.615, 23.619, 23.623, 23.625(a), 23.627, 23.771(a) (for 300 series only),

23.853(a), 23.1301 (for 300 series only), 23.1367(a)(b)(c), 23.1381(a)(b), 23.1529 (for 300 series only),

23.1541 (for 300 series only), 23.1589 (for 300 series only).

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