What it approves
Installation approval of an engine torque instrument with memory exceedance.
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.
This certificate issued to: DIAMOND J, INC.
2020 West Harry Wichita, KS 67213
Part 6 of the Civil Air Regulations.
Original Product - Type Certificate Number: H2SW Make: Bell Model: 206B, 206L, 206L-1, 206L-3, 206L-4
Installation of an Engine Torque Instrument with memory exceedance in accordance with Diamond J, Inc. Top Drawing No. 20101, Rev. B, dated May 6, 1996, or later FAA approved revision. See Continuation Page 3 of 3 for appropriate FAA Approved Rotocraft Flight Manual Supplements.
The approval of this change in the type design applies to the above aircraft model(s) only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that 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.
A copy of this certificate and FAA approved Diamond J, Inc. Top Drawing, Rev. B, dated May 6, 1996, or later FAA approved revision, must be maintained as part of the permanent records of each aircraft modified in accordance with this STC.
Date reissued: May 17, 1999, July 7, 2015
Date amended: May 29, 1996, February 14, 1997, February 11, 2010
Original signed by Yvette Emerson (Signature) Yvette Emerson Program Manager Wichita Aircraft Certification Office (Title)
Date of application: December 21, 1995 Date of issuance: May 7, 1996
United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate Continuation Page
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Number SR09065RC Date of Issuance: May 7, 1996 Date Amended: May 29, 1996, February 14, 1997, February 11, 2010 Date Reissued: May 17, 1999, July 7, 2015
Description of Type Design Change: (continuation page 3 of 3)
The following Rotocraft Flight Manual Supplements, or subsequent FAA Approved revisions, are required:
Model Engine Torque Gage Supplement No. Approval Date 206B 250-C20B/C20J 65100-003 65100-015 65100-022 65100-029 87021 February 14, 1997 206B 250-C20B/C20J 65100-007 87022 April 30, 1996 65100-010 65100-019 65100-033 87022, Rev. A February 14, 1997 206L 250-C28B/C20J 65100-009 87027 May 29, 1996 65100-021 65100-028 65100-035 87022, Rev. A February 14, 1997 206L-1 250-C28B 65100-004 97023 May 29, 1996 65100-016 65100-023 65100-030 97023, Rev. A February 14, 1997 206L-3 250-C30P With Increased Power Operation Kit No. 206-706-045 65100-008 87026 May 29, 1996 65100-020 65100-027 65100-034 87026, Rev. A February 14, 1997 206L-4 250-C30P 65100-006 87025 May 29, 1996 65100-018 65100-025 65100-032 87025, Rev. A February 14, 1997 206L-1 206L-3 250-C30P Modified Per Bell Service Instruction BHT-206-SI-2052 65100-006 65100-018 65100-025 65100-032 82025, Rev. C February 11, 2010 206L-3 206L-1* 250-C30P 65100-005 87024 May 29, 1996 65100-017 65100-024 65100-031 87024, Rev. A February 14, 1997 *L-1 modified by either STC SH296NM or SH5695SW
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.