Attachment A - C_QAPs.pdf

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DLA FORM 1889, JUL 2023

D L A FORM 0 0 1 3, AUGUST 20 22

Prescribed by: eSOP 4155.05-001 Sponsor: J3

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

DLA NOT FOR PRODUCTION

PREVIOUS EDITION IS OBSOLETE

REV

DESCRIPTION

DATE

APPROVED

REVISIONS

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

DISTRIBUTION STATEMENT - A

APPROVED FOR PUBLIC RELEASE

DISTRIBUTION IS "UNLIMITED"

REV

DESCRIPTION

DATE

APPROVED

REVISIONS

DISTRIBUTION STATEMENT - A

APPROVED FOR PUBLIC RELEASE

DISTRIBUTION IS "UNLIMITED"

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

9.0.0.2.20100902.2.720808

Form ID - Form Title

Form ID - Form Title

Randy Davis

DLA DT

DLA DT

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description: ENERGY QAP C1.02 revdate: 2025-03-11 revapproved:

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apprdate: 2025-03-13 apprBy:

reviewdate: 2025-03-11 revBy:

prepdateA: 2025-03-11 prepbyA:

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scale: 1:1 codeIDNo: 52838 size: A nsn:

itemdesc: ENERGY QAP C1.02 btnDSCC:

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line1: DEFENSE LOGISTICS AGENCY, ENERGY line2: 8725 JOHN J. KINGMAN RD line3: FORT BELVOIR, VIRGINIA 22060-6222 revcomments2:

totInstances: 2.00000000

MACLANE.SKYLLAR.

BRYANNA.1252141827

Digitally signed by

MACLANE.SKYLLAR.BRYANNA.1252141827

Date: 2025.01.16 14:17:55 -05'00'

BANISZEWSKI.DANIE

L.J.1287388698

BANISZEWSKI.DANIEL.J.1287388698

Date: 2025.01.22 11:40:41 -07'00'

ROSE.JAMAAL.R.10502

93366

ROSE.JAMAAL.R.1050293366

Date: 2025.01.21 13:21:00 -05'00'

DISTRIBUTION STATEMENT-A: APPROVED FOR PUBLIC RELEASE:DISTRIBUTION IS UNLIMITED

C16.09-1 TURBINE FUEL, AVIATION (JET A1) (CANADA ONLY) (DLA ENERGY JAN 2025)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

9130-21-905-7412 Turbine Fuel, Aviation, Jet A1 CA1

Supplies delivered under this contract shall conform to all in-country environmental requirements applicable to the geographic location of the receiving activity on the date of delivery. In the event the in-country environmental requirement is more stringent than the specification contained in this contract, the Contractor shall deliver product that complies with the more stringent requirement.

Product that fails to meet the more stringent requirement will be considered to be a nonconforming supply.

(a) PERFORMANCE REQUIREMENTS. Aviation turbine fuel shall conform to the requirements of the latest revision of CAN/CGSB-3.23, with the following modifications below when required by contract line item.

(b) NORTH WARNING SYSTEM LOCATIONS. All North Warning System locations shall adhere to the requirements detailed in the most recent revisions of CAN/CGSB-3.23.

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

(i) CONDUCTIVITY. The conductivity limits of 150 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.

(ii) FUEL SYSTEM ICING INHIBITOR (FSII).

(A) The fuel shall contain 0.10 to 0.15 percent by volume FSII.

(B) The FSII shall conform to the requirements outlined in either specification MIL-DTL-85470C dated March 5, 2024, 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) 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, access the Qualified Products Database (QPD) at https://qpldocs.dla.mil, 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).

(c) SYNTHETIC BLEND COMPONENT (SBC) and CO-HYDROPROCESSED SYNTHESIZED KEROSENE

(1) If a fuel containing an SBC or a co-hydroprocessed synthesized kerosene is being offered, notification shall be made to the contracting point of contact with submission of relevant details regarding the blend percentage and which Annex of ASTM D7566 for the synthetic blend component used, and which feedstocks and co-processing percentage for co-hydroprocessed synthesized kerosene. Only synthetic blend components approved in ASTM D7566, MIL-DTL-83133, and MIL-DTL-5624 and co-hydroprocessed synthesized kerosene produced from approved feedstock and percentage in ASTM D1655, MIL-DTL-83133, and MIL-DTL-5624 shall be acceptable to the government

(d) ADDITIVES.

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

(i) 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.

https://qpldocs.dla.mil/

DISTRIBUTION STATEMENT-A: APPROVED FOR PUBLIC RELEASE:DISTRIBUTION IS UNLIMITED

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

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

(B) 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.

(C) 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.

(iii) 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, access the Qualified Products Database (QPD) at https://qpldocs.dla.mil,, 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).

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

(e) 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.

(f) Microseparometer (MSEP).

(1) The following MSEP ratings apply in the presence of the additives listed below. Values apply using ASTM D3948 at the point of manufacture:

Jet A1 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) https://qpldocs.dla.mil/

ENERGY QAP C16.09-1 Turbine Fuel Aviation (Jet A1) (Canada Only) (JAN 2025) .pdf

C16.09-1 TURBINE FUEL, AVIATION (JET A1) (CANADA ONLY) (DLA ENERGY JANAUG 20254)

(ii) FUEL SYSTEM ICING INHIBITOR (FSII).

(d) ADDITIVES.

(5f) Microseparometer (MSEP).