What it approves
Fabrication and installation of Erickson Model 10333-101 (S-64E) or 10333-103 (S-64F) Water/Foam Cannon 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.
United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR00502SE This certificate, issued to: Erickson Air-Crane, Inc.
dba Erickson Air-Crane 3100 Willow Springs Road Central Point, OR 97502 Part 29 of the Federal Aviation Regulations, effective February 1, 1965, including Amendments 29-1 and 29-2, except FAR 29.855(d).
Original ProductType Certificate Number H6EA Make: Erickson Model: S-64E and S-64F
Description of the Type Design Change: Fabrication and installation of Erickson Model 10333-101 (S-64E) or 10333-103 (S-64F) Water/Foam Cannon system in accordance with Erickson Master Drawing List No. 1188, Revision “D,” dated March 11, 1998, or later FAA approved revision. The 10333-101 water/foam cannon installation must be maintained in accordance with Erickson Owner Developed Inspection Checklist No. RS-001, dated November 10, 1997, or later FAA approved revision. The 10333-103 water/foam cannon is maintained in accordance with the basic S-64F maintenance manual.
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 these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship 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 rotorcraft. As a prerequisite to this installation, the rotorcraft must be equipped with an Erickson Fire Fighting System per STC No. SR00004SE and FAA approved installation of Erickson Main Transmission P/N 6435-20400-063 (S-64E) or 6435-20500-048 (S-64F) and Auxiliary Take-off Hydraulic Pump Pad No. 6435-20501-041. The modified rotorcraft must be operated in accordance with Erickson Air-Crane Rotorcraft Flight Manual Supplement (RFMS), dated March 17, 1998, or later FAA approved revision.
A copy of this Certificate and the FAA approved RFMS must be maintained as part of the permanent records for 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.
This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date of application: October 2, 1997 Date reissued: March 1, 2001 Date of issuance March 17, 1998 Date amended: March 1, 2001
(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)
ADs that name this STC · 0
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