STC SR02577LA

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR02577LA This certificate issued to: Van Horn Aviation, L.L.C.

1510 W. Drake Drive Tempe, Arizona 85283 Part 27* of the Federal Aviation Regulations. *See Certification Basis on Continuation Sheet 1 Original Product Type Certificate Number : H2SW Make: Bell Helicopter Textron Model: 206B Description of Type Design Change: Installation and maintenance of main rotor blade assembly P/N 20631000-101 in accordance with Instructions for Continued Airworthiness, ICA Manual No. VMM-MR- 206B-501 Revision B, dated February 10, 2016 or later FAA approved revisions.

Fabrication in accordance with Van Horn Aviation, L.L.C. Master Document List, 206B-MDL-0001, Revision B, dated February 10, 2016 or later FAA approved revisions.

Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted helicopter models only. A copy of this STC must be included in the permanent records of the modified aircraft. 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.

Date of Application: December 11, 2012 Date Reissued: January 24, 2018;

January 30, 2018 Date of Issuance: February 17, 2016 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) Manager, Technical & Administrative TOMNISTRATIO Los Angeles ACO Branch Support Staff

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

- SR02577LA

Date of Issuance: February 17, 2016 Date Reissued: January 24, 2018;

January 30, 2018 Date Amended:

For the Model 206B. Based on the application date and under the provisions of 14 CFR §21.101 and the FAA policy for significant changes in FAA Order 8110.48, the Certification Basis is as follows:

a. Certification Basis for components and areas not changed or affected by this modification is the original certification basis for the Model 206B as shown on TCDS H2SW, Revision 48.

b. Certification Basis for components and areas changed or affected by this modification.

Airworthiness requirements in compliance at the amendment levels of the date of application December 11, 2012:

14 CFR part 27 through Amendment 27-47

27.27 27.171 27.321 27.603 27.661

27.29 27.173 27.337 27.605 27.1529

27.33 27.175 27.339 27.609 A27.4

27.49 27.177 27.341 27.610

27.51 27.251 27.351 27.613

27.65 27.301 27.547 27.623

27.71 27.303 27.571 27.625

27.75 27.305 27.573 27.629

27.141 27.307 27.601 27.653

27.143 27.309 27.602 27.659

14 CFR part 36 through Amendment 36-30, Appendix J, Stage 2

Airworthiness requirements in compliance at the original basis for the Model 206B as shown on TCDS H2SW, Revision 48:

CAR 6.101, Amendment 6-4 (in place of §27.25) CAR 6.116, Amendment 6-4 (in place of §27.87)

END