STC SA02892NY

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA02892NY This certificate, issued to: Delta Engineering Corporation 13 DRBA Way New Castle, Delaware 19720 Part 23 of the Federal Aviation Regulations.

Original Product — Type Certificate Number: Make: Textron Aviation Inc.

A24CE Model: B300 Description of Type Design Change:

Configuration 1: Installation of Nose Extension, Radomes and Cabin Systems in accordance with Delta Engineering Master Data List 0141-07069-2233 Revision S dated Mar. 12, 2020 or later FAA approved revisions to Delta Engineering Master Data List previously listed.

The Instructions for Continued Airworthiness and Airplane Flight Manual Supplement as listed on Master Data List is required for this installation.

Configuration 2: Installation of Nose Extension, Antennas and Radomes in accordance with Delta Engineering Master Data List 0141- 08882-2233 Revision C dated Aug. 27, 2019 or later FAA approved revisions to Delta Engineering Master Data List previously listed. The Instructions for Continued Airworthiness and Airplane Flight Manual Supplement as listed on Master Data List is required for this installation.

Configuration 3: Installation of mission racks in accordance with Delta Engineering Master Data List 0141-10270-2233 Revision B dated Sep. 25, 2017 or later FAA approved revisions to Delta Engineering Master Data List previously listed. The Instructions for Continued Airworthiness as listed on Master Data List is required for this installation.

Configuration 4: Installation of Strake and/or Tail Cone in accordance with Delta Engineering Master Data List 0141-11137-2233 Revision - dated Dec. 11, 2020 or later FAA approved revisions to Delta Engineering Master Data List previously listed. The Instructions for Continued Airworthiness as listed on Master Data List is required for this installation Limitations and Conditions:

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

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

(See Continuation Sheets 3, 4 and 5)

Date of Application: December 4, 2010 Date reissued:

Date of issuance: January 18, 2012 Date amended: March 1, 2013, July 18, 2014 August 2, 2014, January 11, 2017, March 21, 2017, September 26, 2017, September 25, 2019, March 13, 2020 December 14, 2020 By direction of the Administrator Signature:

Title: Jonathan E. Moritz ODA Administrator ODA-800728-NE Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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

Transfer Endorsement Transfer the ownership of Supplement Type Certificate Number:

Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02892NY Date December 14, 2020 Limitations and Conditions:

3. Operational approval of the ASE (Aircraft Survivability Equipment) and MX-15 Class IV Laser is not approved by this FAA STC. These system s must be electrically disconnected.

4. Configuration 1 (of the STC) FAA STC SA03698AT is required for installation of Mission Alternator.

5. Hawker Beechcraft ER version landing gear and rudder required for Configurations 1 and 2 (of the STC).

6. This STC does not include ditching equipment required by CFR 23.1415.

7. This modification may have affected RVSM qualification, therefore testing and qualification needs to be re-established.

8. The FAA has not certified the mission system provisions for which these provisions are intended. You must get additional FAA approval to activate the systems. The FAA must evaluate to ensure it complies with the applicable airworthiness standards.

9. Configuration 1 or 2 (of the STC) optionally can be installed with FAA STC’s SA00263WI and/or SA04080NY.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, this STC is a significant change. The certi fication basis for un-changed or not affected areas by this STC remains un-changed by this STC and the certification basis for this STC is as follows:

a. Part 36 Amendment 36-28 is applicable.

b. The following regulations for CFR Part 23 at later amendment than the TCDS all other regulations at certification basis defined in the TCDS:

Section Title At Amendment 23-

23.23 Load distribution limits 45

23.25 Weight limits 50

23.45 General 50

23.49 Stalling speed 50

23.63 Climb: general 50

23.67 Climb: one engine inoperative 50

23.69 Enroute climb/descent 50

23.77 Balked landing 50

23.143 General 50

23.145 Longitudinal control 50

23.147 Directional and lateral control 50

23.149 Minimum control speed 50

23.153 Control during landings 50

23.157 Rate of roll 50

23.175 Demonstr ation of static longitudinal stability 50

23.177 Static directional and lateral stability 50

23.181 Dynamic stability 45

23.201 Wings level stall 50 Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02892NY Date December 14, 2020 Section Title At Amendment

23.203 Turning flight and accelerated stalls 50

23.207 Stall warning 50

23.251 Vibration and buffeting 45

23.253 High speed characteristics 50

23.301 Loads 48

23.305 Strength and deformation 45

23.321 General 45

23.331 Symmetrical flight conditions 42

23.335 Design airspeeds 48

23.337 Limit maneuvering load factors 48

23.341 Gust load factors 48

23.347 Unsymmetrical flight conditions 48

23.349 Rolling conditions 48

23.351 Yawing conditions 42

23.421 Balancing loads 42

23.423 Maneuvering loads 42

23.425 Gust loads 42

23.427 Unsymmetrical loads 42

23.441 Maneuvering loads 48

23.443 Gust loads 48

23.479 Level landing conditions 45

23.561 General 48, 34*

23.573 Damage tolerance and fatigue evaluation of structure 48

23.574 Metallic damage tolerance and fatigue evaluation of commuter category 48

23.575 Inspections and other procedures 48

23.607 Self-locking nuts 48

23.611 Accessibility 48

23.613 Material strength properties and design values 45

23.629 Flutte r 48

23.785 Seats, berths, safety belts, and harnesses 49

23.787 Cargo compartments 49

23.773 Pilot compartment view 45

23.791 Passenger information signs 49

23.803 Emergency evacuation 46

23.811 Emergency exit marking 46

23.813 Emergency exit access 46

23.815 Width of aisle 46

23.831 Ventilation 42

23.853 Compartment interiors 49

23.867 Lightning protection of structure 49

23.1307 Miscellaneous equipment 49

23.1309 Equipment, systems, and installations 49

23.1322 Warning, caution, and advisory lights 43

23.1323 Airspeed indicating system 49

23.1325 Static pressure system 50

23.1351 General 49

23.1353 Storage battery design and installation 49

23.1357 Circuit protective devices 43

23.1359 Electrical system fire protection 49 Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02892NY Date December 14, 2020 Section Title At Amendment

23.1401 Anti-collision light system 49

23.1431 Electronic equipment 49

23.1441 Oxygen equipment and supply 43

23.1443 Minimum mass flow of supplemental oxygen 43

23.1445 Oxygen distribution system 43

23.1447 Equipment standards for oxygen dispensing units 49

23.1451 Fire protection for oxygen equipment 49

23.1581 General 50

23.1583 Operating limitations 50

23.1585 Operating procedures 50

23.1587 Performance information 50 * 23.561 is amendment 23-34 for cabin modifications.

-------------------------------------------------END------------------------------------------------- Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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