What it approves
Fabrication of AMC AM369A6200-45, -46, -57, -58 Landing Gear Fillet Fairings and AM369H6200-73, and -74 Landing Gear Fairing Guides per AMC Master Drawing List No. MDL-AMC-003, Rev A, dated August 29, 2002 or later FAA approved revision; and installation of this assembly in accordance with the Maintenance Manual for the rotorcraft, document number CSP-HMI-2, Rev 21, or later FAA approved revision.
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.
United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR01136SE
This certificate, issued to Aerometals 3920 Sandstone Drive El Dorado Hills, CA 95762 Part 6 of the Civil Aviation Regulations.
Original ProductType Certificate Number: H3WE Make: MDHI Model: 369A, HS, HM, HE, D, E, FF and 500N
Description of the Type Design Change: Fabrication of AMC AM369A6200-45, -46, -57, -58 Landing Gear Fillet Fairings and AM369H6200-73, and -74 Landing Gear Fairing Guides in accordance with in accordance with AMC Master Drawing List No. MDL-AMC-003, Revision A, dated August 29, 2002 or later Federal Aviation Administration (FAA) approved revision; and installation of this assembly in accordance with the Maintenance Manual for the rotorcraft, document number CSP-HMI-2, Revision 21, or later FAA approved revision. This modification must be maintained in accordance with the MDHI Service and Maintenance instructions, Document number CSP-HMI-2, Section 32-10-00 (Models 369D, E, FF and 500N) or CSP-H-2, Section 6 (Models 369A, HM, HS, HE).
Limitations and Conditions: Approval of this change in type design applies to the MDHI model rotorcraft listed above. This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that helicopter. A copy of this Certificate and the Service and Maintenance Instructions must be maintained as part of the permanent records of the modified helicopter.
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: June 18, 2002 Date reissued: March 1, 2005 Date of issuance: October 21, 2002 Date amended:
(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.