STC SA00081MC

Number SA00081MC

This certificate issued to: L-3 Communications Integrated Systems, L.P.

10001 Jack Finney Blvd.

Greenville, TX 75402

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A24CE Make: Textron Aviation, Inc.

Model: B300

Installation of communication and surveillance equipment in accordance with (1) L -3 Communications Integrated Systems, L.P. Sealed Drawing List SDL 18231-1 Revision F dated 20 Dec 2017, (2) L-3 Flight Manual Supplement dated Nov 2017,

(3) Instructions for Continued Airworthiness, L-3 Document G18231.28.08 Revision B, dated 6 December 2013 or later FAA/ODA approved revisions of (1) (2) and/or (3).

(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: 11 Feb 2011 Date reissued: 06 Nov 2012 Date of issuance: 07 Aug 2012 Date amended: 20 Dec 2017

Signature

Title ODA-750173-SW Administrator Page 1 2 3 Amdt 1 1 1

FAA Form 8110-2 (5/14) Page 1 of 4

To (Name and address of transferee)

From (Name and address of grantor)

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

Number: SA00081MC Amendment 1 Date of Issuance: 20 December 2017 Limitations and Conditions: (Continued)

2. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. This airplane is restricted from flight in known icing conditions.

4. Flight Environments STC SA00085MC is a prerequisite for this STC.

5. In accordance with FAA Order 8110.101, the ALE 47 self protect flare dispensers are installed under a limited approval. The LIDAR system is installed non-operational, as safe carriage equipment.

6. This STC includes provisions for installation in the mission system equipment racks of the ARC -231 radio, Blue Force Tracker, Data Management, Primary Mission Equipment, TCDL, Ku SATCOM, TCAS II, C -band transceiver, amplifier, and diplexer. The equipment for which these provisions are intended has not been certified. Additional FAA approval is required for the installation of this equipment and must be evaluated to assure satisfactory compliance with the applicable airworthiness standards.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA O rder 8110.48, the certification basis for the Textron Aviation, Inc. aircraft is as follows:

a. The type certification basis for Textron Aviation 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, 11 February 2011, was determined to be as follows:

(Certification Basis continued on Page 4 of 4)

FAA Form 8110-2 (5/14) Page 3 of 4

Number: SA00081MC Amendment 1 Date of Issuance: 20 December 2017 Para. Amdt. Para. Amdt. Para. Amdt. Para. Amdt

23.23(a)(b) 23-45 23.303 23-0 23.605(a)(b) 23-23 23.1359(a)(c) 23-49

23.25(b) 23-50 23.305(a)(b) 23-45 23.607(a)(b)(c) 23-48 23.1361(a)(b)(c) 23-49

23.29(a)(b) 23-21 23.307(a) 23-0 23.609(a)(b) 23-0 23.1365(a)(b)(c)(d)(e) 23-49

23.45(a)(b)(d)(e)(f)(g)(h) 23-62 23.321(a)(b)(c) 23-45 23.611 23-48 23.1367(a)(b)(c)(d) 23-0

23.45(h)(4) 23-50 23.331(a)(b) 23-42 23.613(a)(b)(c)(d)(e) 23-45 23.1381(a)(b)(c) 23-0

23.51(c) 23-50 23.333(a)(b)(c)(d) 23-34 23.619 23-7 23.1401(a)(b) 23-49

23.53(c) 23-62 23.335(a)(b)(c)(d) 23-48 23.625(a)(b)(c)(d) 23-7 23.1411(a)(b) 23-36

23.55(a)(b) 23-62 23.337(a)(b) 23-48 23.627 23-0 23.1413(a)(c) 23-22

23.57(a)(b)(c)(d)(e) 23-62 23.341(a)(c) 23-48 23.629(a)(b) 23-31 23.1415(a)(b)(d) 23-0

23.59(a) 23-62 23.347(a) 23-48 23.771(a) 23-14 23.1431(a)(b)(c)(e) 23-49

23.61(a)(b)(c) 23-62 23.351 23-42 23.783(a)(c)(3)(4)(e)(2) 23-49 23.1441(a)(b)(c)(d)(1)(e) 23-43

23.63(a) 23-62 23.365(a)(b)(d) 23-0 23.785(a)(b)(f)(g)(2)(i)(j)(l) 23-34 23.1447(a)(d)(e)(f) 23-49

23.63(d) 23-50 23.367(a)(b) 23-7 23.787(a)(b) 23-49 23.1449 23-9

23.67(c) 23-50 23.441(a)(c) 23-48 23.803(a)(b) 23-46 23.1501(a)(b) 23-21

23.69(a)(b) 23-50 23.443(a)(b)(c) 23-48 23.807(a)(1)(b)(c)(d)(2)(4)(i) 23-49 23.1524 23-10

23.77(c) 23-62 23.471 23-0 23.811(a)(c) 23-46 23.1525 23-0

23.141 23-17 23.473(a)(b)(c)(d)(e)(f)(g) 23-28 23.813(a)(b) 23-46 23.1529 23-26

23.143(a)(b)(c) 23-17 23.479(a)(b)(c) 23-17 23.815(b) 23-46 23.1541(a)(b) 23-21

23.147(a)(b) 23-0 23.481(a)(b) 23-0 23.853(a)(c)(d) 23-49 23.1555(a) 23-50

23.171 23-0 23.483 23-0 23.863(a)(b)(d) 23-34 23.1557(a)(c)(i)(ii)(d)(e) 23-45

23.177(a) 23-21 23.485(a)(b)(c) 23-0 23.867(a)(b)(c) 23-49 23.1559(a)(c) 23-21

23.181(a)(b) 23-21 23.493(a)(b)(c) 23-0 23.1301(a)(b)(c)(d) 23-20 23.1561(a)(b) 23-0

23.201(a)(b)(c)(d)(e) 23-50 23.561(a)(b)(c)(e) 23-34 23.1307 23-49 23.1581(a)(b)(c)(d)(f) 23-50

23.207(c ) 23-50 23.573(a)(b) 23-48 23.1309(a)(b)(c)(d)(e)(f) 23-49 23.1583(c)(4)(5) 23-50

23.233(b)(c) 23-0 23.574(a) 23-48 23.1321(a)(c)(e) 23-49 23.1583(m) 23-62

23.251 23-45 23.575 23-48 23.1322(a)(b)(c)(d)(e) 23-43 23.1585(a)(1)(c)(1)(j) 23-50

23.253(b)(c) 23-50 23.601 23-0 23.1351(a)(b) 23-49 23.1587(a)(2)(d)(2)(7)(8) 23-62

23.301(a)(b)(c) 23-48 23.603(a)(b) 23-23 23.1357(a)(b)(c)(d) 23-43

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