STC SA00340BO

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA00340BO This certificate issued to:

BAE Systems Information and Electronic Systems, Inc.

65 Spit Brook Road Nashua, NH 03061 Part 23 of the Federal; Aviation Regulations.

Original Product - Type Certificate Number: A24CE Make: Beechcraft Corporation Model: B300, B300C Description of Type Design Change:

Installation of an infrared signature suppression system (Ship Set 8495791-1 and 8495791-2) in accordance with BAE Systems, Inc. Master Document List (MDL), 94117-8495803, Rev A, dated February 19, 2014, or later FAA approved revisions.

1. Operation must be in accordance with BAE Systems, Inc. Aircraft Flight Manual Supplement (AFMS) 94117-A83692, Rev IR, dated January 28, 2014, or later FAA approved revisions.

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

(continued on Page 3 of 3)

Date of Application: September 24, 2009 Date reissued:

Date of Issuance: March 28, 2014 Date amended: July 14, 2021 By direction of the Administrator Signature Nicholas Faust Manager, Boston ACO Branch Title

FAA Form 8110-2 (8/13) Page 1 of 4

ign data

SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)

TRANSFER

ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number:

To (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP Code) From (Name of grantor) (Address of grantor) (Number and street) (City, State, and ZIP Code) Extent of Authority (if licensing agreement):

FAA Form 8110-2 (8/13) Page 2 of 4

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA00340BO July 14, 2021 Limitations and Conditions: (continued from Page 1 of 3)

2. Maintenance must be in accordance with BAE Systems, Inc. Instructions for Continued Airworthiness (ICA), 94117-A83693, Rev IR, dated January 28, 2014, or later FAA accepted revisions.

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

3. Compatibility of this design with previously approved modifications must be determined by the installer.

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 the Make Model 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, September 24, 2009, is based upon part 23 as amended by Amendment 23-62 as follows:

Regulations at the latest amendment 23-0 through 23-62 and 36-0 through 36-29

23.1(a)(b), 23.29(a), 23.53(c), 23.55(a)(b), 23.57(a)(1)(2), 23.59, 23.67(d)(1)(2), 23.77(c),

23.251, 23.301(a)(b), 23.305, 23.307, 23.321(a), 23.333(a)(b)(c)(1), 23.337(a)(1)(b),

23.561(a)(b)(2)(i)(ii)(iii), 23.573(b), 23.574, 23.575, 23.601, 23.603, 23.605, 23.607, 23.609,

23.611, 23.613, 23.619, 23.623(a), 23.625(a)(b)(c), 23.627, 23.863(a)(b)(1)(2)(3)(4), 23.865,

23.867(b)(1)(c), 23.901(a)(1)(b)(2)(c)(e), 23.903(e)(4), 23.929, 23.939(a), 23.1041,

23.1043(a)(1)(2)(3), 23.1045(a), 23.1093(b)(1)(i)(2), 23.1121(a)(b)(c)(d)(f)(g)(i), 23.1123,

23.1181(b)(2)(3), 23.1191(b)(c)(f)(g)(h), 23.1193(b), 23.1301(a), 23.1419(a), 23.1529,

23.1581, SFAR23.28, SFAR23.35(h)(j), SFAR23.50, SFAR23.57, 36.9.

FAA Form 8110-2 (8/13) Page 3 of 4

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA00340BO July 14, 2021 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS XYZ None ------------------------------------------------------------END-------------------------------------------------------

FAA Form 8110-2 (8/13) Page 4 of 4