What it approves
Note A. Installation of ACT, Inc. FPTFW0000 High Strength Fuel Cells; Note B. Installation of ACT, Inc. FPTFW00001 High Strength Self Sealing Fuel Cells; Note C. Installation of ACT, Inc. FPTFW00003 High Strength Self Sealing Fuel Cells with interfaces for left side single point refueling and auxiliary tank 14-54 (at station 241.0)
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 SA1358SO This certificate issued to GKN Aerospace Transparency Systems Fort Worth 3220 South Grove Street Fort Worth, TX 76110
Part 3 of the Regulations.
Original Product -- Type Certificate Number: H1NE Sikorsky Make:
S-76A, B, C Model:
A. Installation of ACT, Inc. FPTFW0000 High Strength Fuel Cells in accordance with Westland Technologies, Inc./FPT Master Record Index WT/MRI/123, Issue 16, dated August 1986 and FPT, Inc. Manual FPR/MAN/870, Issue 8, dated July 1983.
B. Installation of ACT, Inc. FPTFW00001 High Strength Self Sealing Fuel Cells in accordance with Westland Technologies, Inc/FPT Mast Record Index WT/MRI/123, Issue 16 dated August 1986 and FPT, Inc. Manual FPT/MAN/870, Issue 8, dated July 1983.
C. Installation of ACT, Inc. FPTFW00003, Issue 3, dated May 5, 2004, High Strength Self Sealing Fuel Cells with interfaces for left side single point refueling and auxiliary tank 14-54 (at station 241.0) in accordance with FPT Industries Document Number T2092/MP/3092, Issue 2, dated 6 May 2003.
Date of application : March 12, 1981
Date of issuance : March 09, 1982 Date reissued : May 8, 2002;
December 24, 2003;
May 05, 2004
Date amended : September 29, 2003
Original signed by: Jennifer L. Kuehn
( Signature) Carl F. Mittag, Manager Rotorcraft Certification Office, Southwest Region
(Tl )
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA1358SO Date of Issuance: March 09, 1982 Re-issuance Date: May 5, 2004 (Page 3 of 3)
Limitations and Conditions: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. FAA Approved Rotorcraft Flight Manual Supplement is required with this installation as follows: Compatibility of this design change with previously approved modifications must be determined by the installer. 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. FPTFW00001 is limited to the Sikorsky S-76A and S-76B models and requires RFM FPT/MAN/899 dated August 9, 1983, for the Sikorsky S-76A Model and RFM FPT/Man1007 dated September 2, 1986, for the Sikorsky S-76B Model.
B. FPTFW00002 is limited to the S-76A and S-76B Model and requires RFM FPT/MAN/934 dated September 22, 1983, for the Sikorsky S-76A Model and FRM FPT/MAN/1007 dated September 2, 1986 for the Sikorsky S-76B Model.
C. FPTFW00003 requires RFM FPT/MAN/2049 dated October 2, 2003, for the Sikorsky S-76A, B, and C models. Aircraft must be equipped with:
• Single point refueling (L/H side) per Sikorsky Type Certificate Approve Option Installation Drawing 76088-300006.
• Auxiliary fuel tank 14-54 with auxiliary float valve at station 241.0 installed in accordance with Sikorsky Drawing 33776-61013 or 33776-61385.
-END-
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