Attachment E - ENERGY QAP C16.09-1 JA1 (CANADA) (JUL 2015).pdf

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Attached to
1. 6A Canada North Warning System Program Federal contract opportunity
Solicitation number
SPE605-21-R-0201
Issued by
Defense Logistics Agency Energy

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Amendment 0003.pdf PDF
Amendment 0002.pdf PDF
Amendment 00001.pdf PDF
Attachment D - AMPS Role Guide.pdf PDF
Attachment F - E Energy QAPS.pdf PDF
Attachment B - Requesting The OET Vendor Role in AMPS Guide.pdf PDF
Final SPE60521R0201.pdf PDF
Attachment G QCP.pdf PDF
Attachment C - PCS OET Vendor Guide.pdf PDF
Attachment A - Base Reference Price and Escalator.pdf PDF

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C16.09-1 TURBINE FUEL, AVIATION (JET A1) (CANADA ONLY) (DLA ENERGY JULY 2015)

Aviation turbine fuel shall conform to the requirements of CAN/CGSB-3.23-2012 dated April 1, 2012, with the following modifications:

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

9130-21-905-7412 Turbine Fuel, Aviation, Jet A-1 JA1

(a) ADDITIVES.

(i) Additives shall not be premixed with other additives before injection into the fuel.

(1) CONDUCTIVITY. If fuel contains electrical conductivity additive, the conductivity limits of 50 to 600 picosiemens per meter (pS/m) at ambient temperature or 85 degrees Fahrenheit (29.4ºC), whichever is lower shall apply at the custody transfer point, unless otherwise directed by the procuring activity.

(2) FUEL SYSTEM ICING INHIBITOR (FSII). When FSII is required by contract line item—

(i) The fuel shall contain 0.07 to 0.10 percent by volume FSII.

(ii) The FSII shall conform to the requirements outlined in either specification MIL-DTL-85470B dated June 15,1999, Inhibitor, Icing, Fuel System, High Flash, NATO Code Number S-1745; or the latest revision of ASTM D4171, Standard Specification for FSIIs, Type III.

(iii) When using the 20-ounce aerosol can to introduce FSII during over the wing refueling, determine the fuel quantity and calculate the amount of required additive. This additive shall be added gradually during filling to permit proper blending in the fuel.

One can of aerosol additive will inhibit 180 gallons of fuel to 0.087 percent by volume. The use of aerosol FSII is not permitted for U.S.

Navy aircraft refueling.

(3) CORROSION INHIBITOR/LUBRICITY IMPROVER (CI/LI). When CI/LI is required by contract line item the additive shall conform to the latest revision of MIL-PRF-25017H with amendment 1 dated August 4, 2011, and be listed in Qualified Products List (QPL)-25017. In order to obtain dosage data for QPL-25017 additives, log into ASSIST Online, access the Qualified Products Database (QPD), do a search for QPL number 25017, and click the MIL-PRF-25017 Category 1 link. The dosage information is located in the "source notes" for each qualified additive as minimum effective and maximum allowable concentrations in grams per cubic meter (g/m3).

(4) METAL DEACTIVATOR ADDITIVE (MDA). MDA shall not be used unless the supplier has obtained written consent from the procuring activity and user.

(b) Product shall be homogeneously mixed. Until all aviation turbine fuel tanks are coated, it is acceptable to perform stratification tests in lieu of circulating tanks to achieve homogeneity.

(5) Microseparometer (MSEP).

(ii) The following MSEP ratings apply in the presence of the additives listed below. Values apply at point of manufacture:

Jet A-1 Additive MSEP Rating, min.

Fuel System Icing Inhibitor (FSII) 85

Corrosion Inhibitor/Lubricity Improver (CI/LI) 80 Fuel System Icing Inhibitor (FSII) and

Corrosion Inhibitor/Lubricity Improver (CI/LI)

Signature

Prepared by:

Quality / Technical Support Office Approval:

Contracting Approval:

Legal Approval:

(Only required for E QAPs)

DMM0076

Typewritten Text DISTRIBUTION STATEMENT - A: APPROVED FOR PUBLIC RELEASE. DISTRIBUTION IS UNLIMITED

2015-07-15T12:48:05-0400
YOUNG.RHEANNAN.K.1503756524
2015-07-15T12:50:39-0400
BANISZEWSKI.DANIEL.J.1287388698

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