STC SA00088MC

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00088MC This certificate issued to: L3Harris Technologies Integrated Systems L.P.

10001 Jack Finney Blvd.

Greenville, TX 75402 Part 23 of the Code of Federal Regulations.

Original Product Make: Textron Aviation, Inc.

Type Certificate Number: . A24CE Model: B300 Description of Type Design Change:

Removal of CAT radome and installation of a L3Harris radome in accordance with (1) L3Harris Technologies Integrated Systems L.P. Sealed Drawing List 10207-2 Revision Q dated 10 June 2024, (2) L3Harris Technologies Integrated Systems L.P. Instructions for Continued Airworthiness (ICA), Document No. G10207.28.09 Revision E, dated 15 March 2024, (3) L3Harris Flight Manual Supplement ETM-JM(GEN-3)-1 Revision 6 dated March 2024, or Limitations and Conditions:

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

Limitations and Conditions: continued on page 3 of 4)

Date of Application: 02 April 2012 Date Reissued:

Date of Issuance: 06 Nov 2012 Date Amended: (1) 18 Sept 2017; (2) 11 June 2024 By Direction of the Administrator Page 2 sime JessicS Rogus Amdt 2 2 Title_ODA-750173-SW Administrator

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00088MC

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

EDERAY PINATION United States of America Department of Transportation PANSTRANG Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00088MC Date of Issuance: 11 June 2024 Limitations and Conditions: (Continued)

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.

4. The ran as not cert fed eared or evil perat com Tens i elect pay sions are intended.

You must get additional FAA approval to install this equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards.

5. Refer to L3Harris Technologies Integrated Systems L.P. STC Configuration Management Document for Special Mission B300 Aircraft, G10748.28.52 Revision A, dated 18 October 2023, or later FAA- approved revision, for applicable prerequisite STC configurations and FAA-approved configurations certified by this STC.

6. The lithium battery is not installed in the KG-250X.

7. This design approval is limited to government/military use only.

8. Equivalent Level of Safety Findings have been made for the following regulation: 14 CFR 23.815(b) Amdt 23-46 Width of Aisle (documented in FAA ELOS Memorandum SA00814MC-A-C-1) 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 Textron Aviation, Inc. B300 aircraft is as follows:

a. The type certification basis for Textron Aviation, Inc. B300 series airplanes 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 reference date of application, 02 April 2012, is as shown below:

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FEDE AEL AVIATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00088MC Amendment 1 Date of Issuance: 11 June 2024 Para. Amdt Para. Amdt Para Amdt

23.21(a) 23-0 23.23(a)(b) 23-45 23.25(b) 23-50

23.29(a)(b) 23-21 23.45(a) (b)(d-h) 23-62 23.45(h4) 23-50

23.49(a)(b) 23-62 23.51 (c) 23-50 23.51 (c) 23-62

23.53(c) 23-62 23.55 (a)(b) 23-62 23.57(a)(b)(c)(d)(e) 23-62

23.59(a) 23-62 23.61 (a)(d)(c) 23-62 23.63(d) 23-50

23.63(a) 23-62 23.65(b) 23-62 23.66(a) (b)(c)(d)(e) 23-50

23.67(c) 23-50 23.67(d) 23-62 23.69(a)(b) 23-50

23.73(c) 23-50 23.77(c) 23-62 23.141 23-45

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23.207(a) (b)(c)(d)(e) 23-50 23.233(a)(b)(c) 23-50 23.251(a)(b)(c) 23-62

23.253(a) (b)(c)(d) 23-62 23.301 (a)(b)(c) 23-48 23.303 23-0

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23.331 (a)(b)(c) 23-42 23.333(a) (b)(c)(d) 23-34 23.335(a) (b)(c)(d) 23-48

23.337(a)(b) 23-48 23.341 (a)(c) 23-48 23.347(a) 23-48

23.351 23-42 23.365(a)(b)(d) 23-0 23.367(a)(b) 23-7

23.441 (a)(c) 23-48 23.443(a)(b)(c) 23-48 23.471 23-0

23.473(a) (b)(c)(d) (e) (g) 23-28 23.479(a)(b)(c) 23-17 23.481 (a)(b) 23-0

23.483 23-0 23.485(a)(b)(c) 23-0 23.493(a)(b)(c) 23-0

23.561 (a)(b)(c)(e) 23-34 23.573(a)(b) 23-48 23.574(a) 23-48

23.575 23-48 23.601 23-0 23.603(a)(b) 23-23

23.605(a)(b) 23-23 23.607(a)(b)(c) 23-48 23.609(a)(b) 23-0

23.611 23-48 23.613(a)(b)(c)(d) 23-45 23.619 23-7

23.625(a) (b)(c)(d) 23-7 23.627 23-0 23.629(a)(b) 23-31

23.771 23-14 23.783 (a)(b3)(c3)(c4)(€2) 23-49 23.785(a) (b)(f)(g2)(i)(i) (1) 23-34

23.791 (a)(b) 23-49 23,803(a)(b) 23-46 23.807(b1) (3)(c)(d2) 23-62

23.811 (a) b)(c) 23-46 23.813(a) 23-46 23.815(a)(b) 23-46

23.851(b)(c1) 23-45 23.853(a)(d3) (i)(ii) (iv)(c) 23-62 23.856 23-62

23.863 (a) (b)(c)(d) 23-34 23.867(a)(b)(c) 23-49 23.1301(a)(b)(c) 23-62

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23.1321 23-49 23.1322(a) (b)(c)(d)(e) 23-43 23.1351 (a)(b) 23-49

23.1357(a)(b)(c)(d) 23-43 23.1359(a)(c) 23-49 23.1361 23-49

23.1365(a)(b)(c)(d)(e) 23-49 23.1367(a) (b)(c)(d) 23-0 23.1401 (a) (b)(c)(d)(e)(t) 23-49

23.1411(a)(b) 23-36 23.1413(a)(c) 23-22 23.1415(a) (b)(d) 23-0

23.1419(b)(c) 23-14 23.1431(a) (b)(c)(d) (e) 23-62 23.1447(d1) 23-62

23.1501 (a)(b) 23-21 23.1524 23-10 23.1529 23-26

23.1541(a)(b) 23-21 23.1555 23-62 23.1557(a)(d) 23-45

23.1561(a)(b) 23-0 23.1581(a) (b)(c)(d)(e)(f) 23-50 23.1583(c1)(c2)(c6)(d) (i)(1)(m) 23-62

23.1583(c4)(c5) 23-50 23.1585(a)(c1)(c2) (f(j) 23-62 23.1587(a2) (c)(d) 23-62

23.1589(a)(b) 23-50

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