What it approves
Fabrication and Installation of Erickson external load dynamic shock absorber system.
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.
Number SR00026SE This certificate issued to
Part 29 of the Federal Aviation Regulations.
Description of Type Design Change: Fabrication and Installation of Erickson external load dynamic shock absorber system in accordance with Erickson Air-Crane Master Drawing List 1051, Revision L, dated November 9, 2001, or later FAA approved revision.
Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer 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 rotorcraft.
Rotorcraft modified in accordance with this STC must be operated in accordance with an FAA approved copy of the Rotorcraft Flight Manual Supplement (RFMS), dated March 9, 2000, or later FAA approved revision. A copy of this Certificate and FAA approved RFMS must be maintained as part of the permanent records of the modified rotorcraft.
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.
Erickson Air-Crane, Inc.
dba Erickson Air-Crane 3100 Willow Springs Road Central Point, OR 97502 H6EA Make : Erickson Model : S-64E and S-64F
Date of application : October 29, 1992
Date of issuance : October 29, 1993
Date reissued : 08/22/97; 03/01/01
Date amended : 05/17/95; 03/09/00;
03/01/01; 08/21/03; 09/17/03;11/21/08
( Signature) Lance T. Gant, Manager Rotorcraft Certification Office Southwest Region
( Title) P/N SA1706RC-R PM EE ASW-170
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