ENERGY QAP C16.08-1 (JAA) (APR 2020) Redact.pdf

DEFENSE LOGISTICS AGENCY ENERGY Page 1 of 2

8725 JOHN J. KINGMAN ROAD

FORT BELVOIR, VIRGINIA 22060-6222

DISTRIBUTION STATEMENT – A: APPROVED FOR PUBLIC RELEASE. DISTRIBUTION IS UNLIMITED

C16.08-1 TURBINE FUEL, AVIATION (JET A) (DLA ENERGY APRIL 2020)

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

Supplies delivered under this contract shall conform to all Federal, State, and local environmental requirements applicable to the geographic location of the receiving activity on the date of delivery. This includes delivery of fuel and documentation in a manner consistent with any existing or after-imposed Title V (Clean Air Act) Permits.

(a) 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-A 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)

(2) Fatty Acid Methyl Ester (FAME)

(i) For offerors that will be offering Jet A FOB Destination and/or Origin TT, which involves staging jet fuel at a terminal via a multi-product pipeline, a Certificate of Quality of the issue tank must include testing for FAME for Acceptance of the fuel. The Test method to be used is either IP 585, IP 583, IP 590, IP 599, or ASTM D 7797. The Referee Method is IP

585. Current ASTM D1655 Jet A specification allows no more than 50 parts per million of FAME in jet fuel.

(b) 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 https://assist.dla.mil (or http://quicksearch.dla.mil)

(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-

DEFENSE LOGISTICS AGENCY ENERGY Page 2 of 2

8725 JOHN J. KINGMAN ROAD

FORT BELVOIR, VIRGINIA 22060-6222

DISTRIBUTION STATEMENT – A: APPROVED FOR PUBLIC RELEASE. DISTRIBUTION IS UNLIMITED

(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.

(c) REPORTS. Refer to the MATERIAL INSPECTION AND RECEIVING REPORT (QAP E40.01) contract provision for reporting requirements.

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