What it approves
Installation of a replacement main rotor blade, part number 500P2100-301 and 303.
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 Helicopter Technology Company 12902 South Broadway Los Angeles, California 90061 Part 6 of the Civil Air Regulations.
*Certification basis is set forth in Type Certificate Data Sheet H3WE.
H3WE MD Helicopter 396A, 396H, 369HE, 369HM and 369HS Description of Type Design Change: Installation of a replacement main rotor blade, in accordance with Helicopter Technology Company (HTC) Maintenance Manual HTCM-001, Rev E, dated 2/24/03 and Master Document List MDL-2100-01, Rev M, dated 2/24/03 or later FAA Approved Revisions.
Limitations and Conditions: HTC Maintenance Manual HTCM-001 Rev. E, dated 2/24/03 is required.
The HTC main rotor blades are a replacement for the MD Helicopter blade. The HTC blade is fully interchangeable in any combination and carries the same life-limit of 2440 hours. 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 aircraft model series 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 17, 1996
Date of issuance : December 08, 1997
Date reissued : December 24, 2003
Date amended : March 12, 2003, July 18, 2008
( Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office (Title)
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Number (STC No.)
ADs that name this STC · 2
An AD can apply because an STC is installed, or mention one in its text.