What it approves
Installation of main rotor assembly P/N 20635000-501
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR02732LA This certificate issued to: Van Horn Aviation LLC 1510 W. Drake Drive Tempe, Arizona 85283 Part 27* of the Code of Federal Regulations. *See Certification Basis on Continuation Sheet Original Product Make : Bell Helicopter Textron Type Certificate Number: H2SW Canada Limited Model: 206B
Description of Type Design Change: Installation of main rotor assembly P/N 20635000-501 in accordance with FAA approved Van Horn Aviation LLC Master Document List 206B-MDL-0002, Revision C, dated May 13, 2020, or later FAA approved revision and maintained in accordancewith Airworthiness Limitations Section of report number VMM-MR-206B-503, dated August 11, 2020 or later FAA approved revision.
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. Instructions for Continued Airworthiness, report number VMM-MR-206B-503, Revision A, or later FAA accepted revision must be available to the operator at the time of installation.
Date of Application: February 05, 2019 Date Reissued:
Date of Issuance: August 12, 2020 Date Amended:
Title: Manager, Airframe Section, Los Angeles ACO Branch
MAUREEN A
MORELAND Digitally signed by MAUREEN A
MORELAND Date: 2020.08.12 15:45:23 -07'00'
FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR02732LA
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR02732LA Certification Basis: 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 49.
b. Certification Basis for components and areaschanged or affected by this modification.
Airworthiness requirements in compliance at the amendment levels of the date of application February 05, 2019:
Regulations at the latest amendment 27-0 through 27-47
27.25 27.143 27.321 27.605 27.907(b)
27.27 27.171 27.337 27.607 27.923
27.29 27.173 27.339 27.609 27.939(a)
27.33 27.175 27.341 27.610 27.1505
27.49 27.177 27.351 27.613 27.1529
27.51 27.251 27.547 27.623 27.1581
27.65 27.301 27.571 27.625 27.1583
27.71 27.303 27.573 27.629 27.1585
27.75 27.305 27.601 27.653 27.1587
27.79 27.307 27.602 27.659 A27.4
27.141 27.309 27.603 27.661 14 CFR part 36-1 through Amendment 36-31, Appendix J Airworthiness requirements in compliance at an earlier amendment level:
§27.79, Amendment 27-0 (in place of §27.87) §27.25, Amendment 27-0 §27.1587, Amendment 27-0 END
FAA Form 8110-2 (4/20) Page 3 of 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Bell Helicopter Textron Canada Limited | 206B | H2SW |