ENERGY_QAP_C16.08-1_JAA_(AUG_2014).pdf

C16.08-1 TURBINE FUEL, AVIATION (JET A) (DLA ENERGY AUG 2014)

Jet A shall conform to the requirements of ASTM D 1655, Standard Specification for Aviation Turbine Fuels, except as modified below, at the custody transfer point

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

9130-00-359-2026 Turbine Fuel, Aviation, Jet A JAA

(a) ADDITIVES.

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

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

(i) FSII shall be added to the fuel and shall be Diethylene Glycol Monomethyl Ether (DIEGME) conforming to ASTM D4171, Standard Specification for FSIIs, Type III or MIL-DTL-85470B, dated June 15, 1999, Inhibitor, Icing, Fuel System, High Flash, NATO Code Number S-1745.

(ii) FSII shall be added to the fuel so that the resulting concentration in the final blend is between 0.07% and 0.10% by volume.

(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 required by contract line item-

(i) The additive must conform to MIL-PRF-25017H with Amendment 1, dated August 4, 2011 Inhibitor, Corrosion/Lubricity

Improver, Fuel Soluble (NATO S-1747), found in ASSIST and shall be listed in the electronic Qualified Products List (QPL)-25017, located in the Qualified Products Database (QPD) found at http://assistdocs.com.

(ii) The concentration of CI/LI added to the fuel must be between the minimum effective concentration and the maximum allowable concentration as listed for the CI/LI in QPL-25017.

(4) STATIC DISSIPATER ADDITIVE (SDA). When required by contract line item-

(i) SDA shall be added to the fuel and the conductivity limits of 50 to 600 picosiemens per meter (pS/m) at ambient temperature or 29.4oC (85oF), whichever is lower, unless otherwise directed by the procuring activity.

(5) METAL DEACTIVATOR (MDA). MDA shall not be used unless the supplier has obtained PRIOR written consent from the procuring activity.

(6) 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.

(b) SPECIFICATION MODIFICATIONS

(1) Microseparometer (MSEP).

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

Jet-AAdditive 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)

REPORTS. Refer to the MATERIAL INSPECTION AND RECEIVING REPORT contract provision for reporting requirements.

Signature

Prepared by:

Quality / Technical Support Office Approval: Prior approval as contract provision

Contracting Approval: Prior approval as contract provision Legal Approval:

(Only required for E QAPs) http://assistdocs.com/

DMM0076

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