STC SA04648CH

FEDERAL AVIATIO United States of America Department of Transportation Federal Aviation Administration PREAMISTRATE Supplemental Type Certificate Number: SA04648CH This certificate issued to: StandardAero Business Aviation Services, LLC.

1200 North Airport Drive Springfield, Illinois 62707 USA Part 23 of the Federal Aviation Regulations.

Type Certificate Number: A37CE Original Product Model: 208B Make: Textron Aviation Inc.

Installation of a Universal Adapter Plate (UAP) and Radome for Electronically Steered Antenna (ESA) in accordance with FAA approved Master Data List 1042163 Revision (B), dated October 30, 2024, or later FAA Approved Revision.

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

Date of Application: November 3, 2023 Date Reissued:

Date of Issuance: November 6, 2024 Date Amended:

Dan Trigg, ODA Administrator StandardAero, Springfield, IL Title: ODA-100079-CE

000. or imprisonment not exceeding 3 years, or both. The ST's supporting documentation (drawings, instructions.

specifications, flight manual supplements, etc.) is the property of the STC holder.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of _4

EDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration TAN STRATO Supplemental Type Certificate Number: SA04648CH

specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to use the STO to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120).

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of _4

EDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration TOUNISTRATO Supplemental Type Certificate (Continuation Sheet) Number: SA04648CH Description of Type Design Change: - cont.

FAA Approved Airplane Flight Manual Supplement document number 2022009-AFMS-001, Revision (IR), dated 25 OCT 2024, or later FAA Approved Revision is a required part of this modification.

The aircraft must be maintained in accordance with FAA accepted Instructions for Continued Airworthiness, document number 2022009-ICA-1100, Revision (A), dated 01 JUL 2024, or later FAA accepted revision in addition to the basic airplane maintenance manuals.

Limitations and Conditions: - cont.

2. 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.

3. Any equipment installed on the UAP must meet ICD requirements and requires additional FAA approval.

4. This STC is applicable to serial number 208B2197, 208B5000 and higher for this Make-Model with the following prerequisite installations.

5. This STC is limited to aircraft equipped with the Pratt and Whitney Canada (P&WC) PT6A140 engine.

6. This STC is limited to aircraft equipped with model number 4HFR34C778/102BHA-0 Propeller (installed under McCauley Propeller Systems STC SA09850AC).

7. This STC is limited to aircraft with increased Maximum Takeoff Weight or 9,062 Ibs.

(installed under AeroAcoustics Aircraft Systems, Inc. STC SA01805SE) Certification Basis - cont.

Based on 14 CFR §§ 21.101, 21.115 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the Textron Aviation Inc. 208B Aircraft installation of a UAP for ESA is as follows:

This

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United States of America Department of Transportation Federal Aviation Administration TAIN STRATO Supplemental Type Certificate (Continuation Sheet) Number: SA04648CH Certification Basis - cont.

a. The type certification basis for Textron Aviation Inc. 208B is shown on TCDS A37CE 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 application, November 3, 2023, is based upon TCDS A37CE. Based on 14 CFR § 21.101, 21.115 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for this modification was determined to be:

Regulations at the amendment level in TCDS A37CE.

23.93(b) [21-27], 23.1(a, b) [23-10], 23.51 (a(1)) [23-21], 23.251 [Original],

23.301(a, b) [23-28], 23.303 [Original], 23.305(a, b) [Original], 23.307(a) [Original],

23.331(a, b) [Original], 23.333(a-d) [23-7], 23.335(a-c) [23-16], 23.337(a-c) [23-7],

23.341 [23-7], 23.349(a, b) [23-7], 23.351 [Original], 23.561(a-e) [23-7],

23.572(a(1)) [23-14], 23.601 [Original], 23.603(a) [23-23], 23.605(a) [23-23],

23.607 [23-17], 23.613 (a-c) [23-23], 23.615(a) [23-7], 23.619 [23-7],

23.625(a-c) [23-7], 23.627 [Original], 23.629(a, b, f(2)) [23-23], 23.867 (a, c(2)) [23-7],

23.1419(a-d) [23-14], 23.1519 [Original], 23.1529 [23-26], 23.1581(a, b, d) [23-21],

23.1583(c) [23-23], 23.1585(a) [23-23], 23.1587(a) [23-28].

Regulations at later amendment level:

23.49(a-d) [23-62], 23.65(b(1-4)) [23-62], 23.77 (b(1-4)) [23-50], 23.143(a) [23-50],

23.145(e(1)) [23-50], 23.147(c) [23-50], 23.201 [23-62], 23.203 [23-62],

23.251 (a,b) [23-62], 23.573(b(2), c) [23-45], 23.575 [23-48].

•-END.

This (14 CFR 21.47). , FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 4 of 4