Attachment 7 ENERGY QAP C Portfolio.pdf

For the best experience, open this PDF portfolio in

Acrobat X or Adobe Reader X, or later.

Get Adobe Reader Now!

http://www.adobe.com/go/reader

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

DEFENSE LOGISTICS AGENCY ENERGY Page 1 of 2

8725 JOHN J. KINGMAN ROAD

FORT BELVOIR, VIRGINIA 22060-6222

C16.09 TURBINE FUEL, AVIATION (JET A1) (DLA ENERGY JUL 2022)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE PRODUCT CODE

9130-00-753-5026 Turbine Fuel, Aviation, Jet A-1 JA1

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. The list of such requirements contained in this contract is not intended to be a complete list, and the Contractor shall be responsible for determining the existence of all such requirements. Selected regional environmental requirements are highlighted in the SPECIFICATIONS (CONT’D) clause. In the event that a Federal, State, or local environmental requirement is more stringent than a fuel specification contained in this contract, the Contractor shall deliver product that complies with the more stringent fuel specification. Product that fails to meet the more stringent fuel specification will be considered to be a nonconforming supply. Product(s) to be supplied shall fully meet the requirements of the applicable specification(s) as cited above. In the event that compliance with the more stringent fuel specification causes the contractor to incur additional costs, the contractor may request an equitable adjustment.

(a) PRODUCT REQUIREMENTS. Product shall conform to the latest version of ASTM D1655: Standard Specification for Aviation Turbine Fuels with the following modifications. For European, Middle Eastern, and Asian Locations Only: product shall conform to the latest revision of Defence Standard 91-091.

(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 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) 70

a. MSEP shall be performed on unadditized Jet A that has a custody transfer point on the distribution system using, D7224 or D8073. If either method is not available testing may be conducted with D3948. Passing results (min 85) for D3948 will be considered acceptable. Test failures using D3948 shall be retested using D7224 or D8073. If fuel passes D7224 with a minimum limit of 85 or D8073 with a limit of 88, the fuel is acceptable with no further action.

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

(1) 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) FSII shall be added to the fuel and shall be Diethylene Glycol Monomethyl Ether (DIEGME) conforming to the latest version of ASTM D4171, Standard Specification for FSIIs, Type III or MIL-DTL-85470B, dated June 15, 1999 revalidated August 28, 2019, Inhibitor, Icing, Fuel System, High Flash, NATO Code Number S-1745.

(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.

(2) 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, revalidated May 25, 2021 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).

(3) 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.

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

(i) 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.

Signature

Prepared by:

Date:

Quality/Technical Support Office Approval

Contracting Approval: Digitally signed by

MACLANE.SKYLLAR.B.1252141827

Digitally Signed By:

Digitally Signed By: MACLANE.SKYLLAR.B.1252141827

2022.08.03 09:13

C16.09 TURBINE FUEL, AVIATION (JET A1) (DLA ENERGY OCT 2017AUG 2021JULN 2022)

PRODUCT CODE

PRODUCT NOMENCLATURE

NATIONAL STOCK NUMBER

JA1

Turbine Fuel, Aviation, Jet A-1

9130-00-753-5026

(b) SPECIFICATION MODIFICATIONS.

2022-08-15T12:12:18-0400

RALPH.ERIN.S.1229663042

2022-09-08T13:05:30-0400

BANISZEWSKI.DANIEL.J.1287388698

C16.15 GASOLINE, AVIATION (GRADE 100LL) (DLA ENERGY FEB 2021)

Aviation Gasoline shall conform to the latest revision of ASTM D910 or Defense Standard 91-090.

Quality Technical Directorate Approval: Prior approval as contract provision

Contracting Approval: Prior approval as contract provision

2021-02-05T13:11:17-0500

STEPHENS.MAKEENA.1276390119

DEFENSE LOGISTICS AGENCY ENERGY

C16.64-1 TURBINE FUEL, AVIATION (JP8) (INLAND EAST GULF/OFFSHORE) (ROCKY

MOUNTAIN/WEST) (WESTPAC) (ATL/EUR/MED) (PC&S) (DLA OCT ENERGY 2022)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

9130-01-031-5816 Turbine Fuel, Aviation JP8

Aviation Turbine Fuel (JP8) shall conform to MIL-DTL-83133K, dated July 18, 2018 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. The list of such requirements contained in this contract is not intended to be a complete list, and the Contractor shall be responsible for determining the existence of all such requirements. Selected regional environmental requirements are highlighted in the SPECIFICATIONS (CONT’D) clause. In the event that a Federal, State, or local environmental requirement is more stringent than a fuel specification contained in this contract, the Contractor shall deliver product that complies with the more stringent fuel specification. Product that fails to meet the more stringent fuel specification will be considered to be a nonconforming supply.

Product(s) to be supplied shall fully meet the requirements of the applicable specification(s) as cited above. In the event that compliance with the more stringent fuel specification causes the contractor to incur additional costs, the contractor may request an equitable adjustment

(a) INCIDENTAL CONTAMINANTS. Particulate Matter and Fatty Acid Methyl Ester (FAME) content shall not exceed the limits outlined in Table IV of MIL-DTL-83133K dated July 18, 2018.

(b) SPECIFICATION MODIFICATIONS. Aviation Turbine Fuel (JP8) shall conform to MIL-DTL-83133K, dated July 18, 2018, modified as follows:

(1) TESTING

(i) FILTRATION TIME TESTING. For filtration time testing round upwards when reporting the filtration time, in minutes. For example, a filtration time of 10 minutes, 18 seconds, would be reported as 11 minutes.

(ii) MICROSEPAROMETER (MSEP) RATING LIMITS. See MIL-DTL-83133K, dated July 18, 2018, Table 1, Note 15 for MSEP test method selection criteria.

(A) Prior to initial production under this contract, the Contractor shall elect, on a one-time basis, which MSEP limit will be met for the balance of the contract. If the Contractor introduces fuel system icing inhibitor (FSII), corrosion inhibitor/lubricity improver (CI/LI), and/or static dissipater additive (SDA) after verification of product conformance with the MSEP requirement, the product is not required to meet a fixed limit on subsequent MSEP tests.

(B) If the Contractor elects to verify conformance with the MSEP requirement on a sample of product that does not contain FSII and CI/LI, an additional MSEP test shall be performed on a hand blend containing aviation turbine fuel, FSII, CI/LI, and antioxidant (AO) (AO only if required). The FSII shall be included in this hand blend at a concentration of 0.07 to 0.10 volume percent and the amount of the CI/LI included shall be within the concentration range specified in QPL-25017. The additional MSEP result of this hand blend is a REPORT ONLY requirement and shall be recorded corresponding to item 750X on the Standardized Report Form (see Attachment ). This result shall be recorded with an asterisk next to it, and with a footnote below, stating, “*MSEP result is a ‘Report Only’ requirement.

Original result of (fill in actual result) on product containing the following additives:

(fill in combination of additives).”

(iii) WORKMANSHIP. The workmanship criteria in MIL-DTL-83133K, dated July 18, 2018, paragraph 3.5, is revised to read, “At the custody transfer point, the finished fuel shall be clear and bright and visually free from undissolved water and particulate matter in accordance with the latest revisions of the approved test methods. ASTM D4176 or ASTM D6986, latest versions, may be used. In case of dispute as determined by sample results taken from the custody transfer point, the fuel shall be clear and bright at 21 degrees Celsius (°C) (70 degrees Fahrenheit [°F]) and shall contain no more than 1.0 mg/L of particulate matter. The sample in dispute shall be taken into an area where the sample is permitted to slowly equilibrate to 21°C (70°F); this shall apply to either D4176 or D6986.”

(A) ASTM D6986, latest revision, shall be the referee test method, see requirements, as drafted, in MIL-DTL- 83133K, dated July 18, 2018, section 3.5.

(B) For the latest revision of ASTM D 4176, Procedure 2, with a result of Rating 1, maximum. If the sample fails ASTM D4176 only because it contains visible particulate matter but meets the particulate matter requirements of 1.0 mg/L maximum as stated in MIL-DTL-83133K, Table IV, the workmanship criteria is met.

(2) SPECIAL LOCATION REQUIREMENTS

(i) Rocky Mountain/West. Aviation fuel movement via the Chevron Pipeline (Utah, Idaho, or Washington state entry points) shall be limited to total sulfur content of 0.15 mass percent, maximum.

(ii) Alaska. For fuels refined in Alaska and delivered to Alaska locations, the total acid number shall be relaxed to

0.020 mg KOH/g maximum.

(c) ADDITIVES. Additives are required for deliveries of JP8 per MIL-DTL-83133K, dated July 18, 2018, unless addition is excluded by specific solicitation line item, applicable contract clause, or another contractual requirement.

(1) The CI/LI additive(s) used shall be of the type and concentration cited in QPL-25017. To locate this information: (1) Go to the Acquisition Streamlining and Standardization Information System (ASSIST) Quick Search website (URL http://quicksearch.dla.mil/), (2) type "QPL-25017" in the Document ID field, press the Search button, (3) click the QPL- 25017 search result under Document ID, (4) click the "Qualification" link under Overview [or the "View QPD data" link under Revision History], and (5) click the “MIL-PRF- 25017 CATEGORY 1” link under Govt Designation. The concentration range for each additive is listed under the “Source Notes” link under the far-right column of the table.

(2) Metal deactivator additive (MDA) shall not be used in JP8 unless the Contractor has obtained written consent from the Contracting Officer.

(3) The requirement for SDA (see MIL-DTL-83133K, dated July 18, 2018, paragraph 3.3.3 and fuel electrical conductivity requirement in Table I) shall not apply unless stated otherwise in the Schedule. Line injection of additives (FSII, CI/LI, and SDA) from shipping tank to delivery conveyance is permitted under the following conditions:

(i) A laboratory hand blend containing the required additives and aviation turbine fuel shall be tested to verify compliance with the specification.

(ii) Additives shall be proportionately injected throughout the entire loading process to ensure the additive is homogeneously blended into the product. The Contractor shall maintain records evidencing the homogeneous blending of all line-injected additives. Such records shall include meter or tank gauge readings or test results taken at intervals to provide confidence in the injection process.

(iii) When FSII is line injected, additive concentration shall be verified based on a representative sample from each shipping conveyance.

(iv) When SDA is line-injected, and insufficient time is available for the fuel to reach equilibrium before departure of the shipping conveyance, the Contractor shall verify conductivity level on a representative sample from each shipping conveyance. The receiving activity will measure the conductivity and advise DLA Energy if it does not meet the specification requirements.

(4) SPECIAL LOCATION REQUIREMENTS (ATL/EUR/MED ONLY)

(i) For deliveries to La Spezia, Italy, the CI/LI shall be 3.5 g/m3 above the minimum effective concentration as identified in QPL-25017. See paragraph (c)(1) above.

(ii) When AO is added to the hydrotreated portion of the finished product, the percentage of the blend that has been hydrotreated shall be reported.

(iii) The requirement for SDA (see MIL-DTL-83133K, dated July 18, 2018, paragraph 3.3.3 and fuel electrical conductivity requirement in Table I) shall not apply unless stated otherwise in the Schedule.

Contracting Approval:

Signed by:

Date: October, 27, 2022 12:10 http://quicksearch.dla.mil/)

(1) TESTING

(2) SPECIAL LOCATION REQUIREMENTS

(4) SPECIAL LOCATION REQUIREMENTS (ATL/EUR/MED ONLY)

2022-11-02T09:58:07-0400

RALPH.ERIN.S.1229663042

2022-11-03T13:33:31-0400

BANISZEWSKI.DANIEL.J.1287388698

DEFENSE LOGISTICS AGENCY ENERGY Page 1 of 1

C16.69-1 GASOLINE AUTOMOTIVE, UNLEADED, REGULAR (PC&S) (DLA ENERGY JUN 2017)

9130-00-148-7103 Gasoline, Regular Unleaded MUR

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 existing or future Title V (Clean Air Act) Permits. In the event that a Federal, State, or local environmental requirement is more stringent than a similar requirement in a fuel 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 environmental requirement will be considered to be a nonconforming supply. All supplies furnished under this contract shall fully meet the requirements of the applicable specification(s) as cited below. In the event that compliance with the more stringent requirement causes the contractor to incur additional costs, the contractor may request an equitable adjustment.

NOTE: Gasoline Reid Vapor Pressure (RVP) specification requirements are seasonal and vary geographically. Therefore, Contractors are expected to know the In-country, State, or Federal RVP requirements of areas being supplied and comply with those requirements.

GASOLINE AUTOMOTIVE, UNLEADED, REGULAR. Gasoline shall conform to each country specification as listed below:

COUNTRY SPECIFICATION NATIONAL STOCK NUMBER

AUSTRALIA FUEL STANDARD (PETROL) 2001

CANADA CAN/CGSB-3.5-2001

JAPAN JIS K 2202

PHILIPINES PNS/DOE QS 008:2012 9130-00-148-7103

MIDDLE EAST EN 228

ALL OTHER REGIONS ASTM D4814

LOCAL SPECIFICATIONS: In-country specifications not meeting the specification requirements in the chart above, but meet local requirements may also be submitted for review and approval.

(a) OCTANE REQUIREMENTS

(1) Unleaded regular automotive gasoline shall meet the Motor Octane Number (MON), Research Octane Number (RON) and/or

Anti-Knock Index (AKI) limits described in the specification listed for each country or the in-country requirements when applicable.

(2) Reductions for altitude and seasonal variations are allowed for all AKI values in accordance with specification listed for each country requirements when applicable.

(b) OXYGENATE REQUIREMENTS.

(1) In order to achieve minimum/maximum oxygen content limits specified per Federal, State, and local environmental requirements, supplies shall only include oxygenates that are permitted by environmental regulations applicable to the time and place of delivery.

(2) Blending of oxygenates into gasoline to meet oxygenated fuel requirements shall be accomplished by mechanical mixing or agitation in a tank, or by in-line blending, prior to loading the product into transport equipment, and the resultant product must meet contract requirements.

2017-06-07T13:33:14-0400

MEREDITH.MICHAEL.E.1290973453

2017-06-07T14:14:28-0400

BANISZEWSKI.DANIEL.J.1287388698

2017-08-24T07:15:59-0400

PETERSON.DAVID.W.1074069483

C16.69-11 DIESEL FUEL SPECIFICATION (PC&S) (DLA ENERGY DEC 2016)

9140-01-524-0139 Grade Number 2-D S15 (ULSD) DS2

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. The list of such requirements contained in this contract is not intended to be a complete list, and the Contractor shall be responsible for determining the existence of all such requirements. Selected regional environmental requirements are highlighted in the SPECIFICATIONS (CONT’D) clause. In the event that a Federal, State, or local environmental requirement is more stringent than a fuel specification contained in this contract, the Contractor shall deliver product that complies with the more stringent fuel specification. Product that fails to meet the more stringent fuel specification will be considered to be a nonconforming supply. Product(s) to be supplied shall fully meet the requirements of the applicable specification(s) as cited above. In the event that compliance with the more stringent fuel specification causes the contractor to incur additional costs, the contractor may

Product shall conform to commercial specification ASTM D 975. In accordance with this specification, product shall be visually free of undissolved water, sediment, and suspended matter. Product classification is shown above. Maximum sulfur content shall be 0.0015 wt%.

(a) ADDITIVES.

(1) A fuel stabilizer additive conforming to MIL-S-53021, latest revision, may be blended into the fuel to improve the suitability of fuel for long term storage. Permissible additive concentrations are specified in the latest revision of QPL-53021.

(2) A corrosion inhibitor/lubricity improver additive may be blended into the fuel to inhibit corrosion and improve fuel lubricity.

Permissible additive concentration limits are specified in the latest revision of QPL 25017.

(3) A fuel system icing inhibitor may be blended into the fuel to purge small quantities of water from the fuel and prevent the formulation of ice crystals. The additive concentration shall not exceed 0.15 volume percent when tested in accordance with ASTM D 5006.

(b) BLENDING. Blending one grade of diesel fuel with another grade, or other compatible components, to produce a different grade or a variation within a grade is permitted. However, such blending shall be accomplished by mechanical mixing or agitation in a tank, or in-line blending, prior to loading the product into transport equipment, and the resultant product must meet all the requirements of the desired fuel.

(c) LOW TEMPERATURE OPERABILITY. The low temperature performance of diesel fuel shall be defined by the following property:

CLOUD POINT. Unless a more restrictive cloud point limit is specified in the contract schedule, the cloud point shall be equal to or lower than the tenth percentile minimum ambient temperature specified in Appendix X5 of ASTM D 975. Within Alaska for activities where fuel support is limited to April-September, for example "JUN/JUL", "MAY 15 - JUN 15", "DURING SUMMER MONTHS", etc, and fuel will be used year-round in support of continuing operations, the cloud point shall be equal to or lower than the tenth percentile minimum temperature specified in Appendix X5 of ASTM D 975 for the month of January.

MEREDITH.MICHAEL.E.1290973453 Digitally signed by MEREDITH.MICHAEL.E.1290973453 Date: 2016.12.22 15:09:43 -05'00'

BANISZEWSKI.DANIEL.J.1287388698 Digitally signed by BANISZEWSKI.DANIEL.J.1287388698 Date: 2016.12.28 09:07:05 -05'00'

PETERSON.DAVID.W.1074069483 Digitally signed by PETERSON.DAVID.W.1074069483 Date: 2017.01.06 16:51:05 -05'00'

C40 PROPANE-BUTANE MIXTURES (PC&S) (BULK)(DLA ENERGY MAR 2018)

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 existing or future Title V (Clean Air Act) Permits. In the event that a Federal, State, or local environmental requirement is more stringent than a similar requirement in a fuel 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 environmental requirement will be considered to be a nonconforming supply. All supplies furnished under this contract shall fully meet the requirements of the applicable specification(s) as cited below. In the event that compliance with the more stringent requirement causes the contractor to incur additional costs, the contractor may

6830-01-628-8003 Propane-Butane Mixtures CNG

(a) PROPANE, PROPANE-BUTANE MIXUTRES

(1) Product shall conform to commercial specification GPA 2140 Liquid Petroleum Gas Specifications and Test Methods or ASTM D1835, Standard Specification for Liquid Petroleum Gases, Product Type, Commercial Propane-Butane Mixtures, latest revision.

(2) In cases where methanol is present, ASTM D2713 is not applicable for determining dryness of propane products.

(b) VAPOR PRESSURE REQUIREMENTS

(1) The permissible vapor pressures of products classified as propane-butane mixtures shall not exceed 1430 kPa (208 psig) and additionally shall not exceed that calculated from the relationship as specified in note B of ASTM D1835.

2018-06-05T11:03:00-0400

ATKINS.RENRICK.L.1024389320

2018-06-06T09:31:28-0400

BANISZEWSKI.DANIEL.J.1287388698

2018-06-28T13:38:00-0400

PETERSON.DAVID.W.1074069483

C16.08-1 TURBINE FUEL, AVIATION (JET A) (DLA ENERGY JUL 2022)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE 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) PRODUCT REQUIREMENTS. Jet A shall conform to the requirements of the latest version of ASTM D 1655, Standard Specification for Aviation Turbine Fuels, except as modified below, at the custody transfer point.

(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-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)

(ii) MSEP shall be performed on unadditized Jet A that has a custody transfer point on the distribution system using, D7224 or D8073. If either method is not available testing may be conducted with D3948. Passing results (min 85) for D3948 will be considered acceptable. Test failures using D3948 shall be retested using D7224 or D8073. If fuel passes D7224 with a minimum limit of 85 or D8073 with a limit of 88, the fuel is acceptable with no further action.

(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.

(c) 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 the latest version of ASTM D4171, Standard Specification for FSIIs, Type III or MIL-DTL-85470B, dated June 15, 1999, revalidated August 28, 2019, 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, revalidated May 25, 2021, 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) https://assistdocs.com/ 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-

(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.

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

Quality / Technical Support Office Approval:

MACLANE.SKYLLAR.B.1252141827 Digitally Signed By:

MACLANE.SKYLLAR.B.1252141827

2022.08.02 07:51

C16.08-1 TURBINE FUEL, AVIATION (JET A) (DLA ENERGY APRIL 2020JUNJUL 2022AUG 2021)

(a) PRODUCT REQUIREMENTS. Jet A shall conform to the requirements of the latest version of ASTM D 1655, Standard Specification for Aviation Turbine Fuels, except as modified below, at theat the custody transfer point.

(b) SPECIFICATION MODIFICATIONS

(c) ADDITIVES.

2022-08-15T12:13:46-0400

RALPH.ERIN.S.1229663042

2022-09-08T13:04:22-0400

BANISZEWSKI.DANIEL.J.1287388698