ATTACHMENT_8_C_QAPS.pdf

C1.02 ASSIST DATABASE OF SPECIFICATIONS (DLA ENERGY DEC 2014)

Unless otherwise specified, current versions of defense or federal specifications and standards, military handbooks, commercial item descriptions, qualified product lists, and other related technical documents cited in this solicitation/contract can be accessed from the Department of Defense (DoD) Acquisition Streamlining and Standardization Information System (ASSIST) database at https://assist.dla.mil under ASSIST-Quick Search or http://quicksearch.dla.mil. ASSIST is the official source for all Defense Standardization Program documents and contains the most current information on documents prepared by DoD, as well as information on how to acquire referenced non-Government standards that have been adopted for DoD use. Those who register for an ASSIST account may establish profiles to receive automatic E-mail alerts when changes are planned or made to documents of interest by selecting criteria on the [Alert Portal Profile Maintenance] screens accessed from the [User Profile] menu. Users may also view or download a bi-monthly summary of changes to the ASSIST database under the [ASSIST Update] menu.

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)

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

YOUNG.RHEANNAN.K.1503756524

Digitally signed by YOUNG.RHEANNAN.K.1503756524 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=YOUNG.RHEANNAN.K.1503756524 Date: 2014.12.19 13:46:43 -05'00' feb9073 Typewritten Text

ATTACHMENT 8

C16.01 TURBINE FUEL, AVIATION (JP5) (BULK) (DLA ENERGY APR 2016)

(a) Product shall meet MIL-DTL-5624W, Turbine Fuel, Aviation, Grade JP-5, dated March 28, 2016.

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

9130-00-273-2379 Turbine Fuel, Aviation, JP-5 JP5 9130-01-499-9521 Turbine Fuel, Aviation, JP-5 (Bunker fuel overseas locations only) JP5

(b) SPECIFICATION MODIFICATION: The requirements of Table I in the specification are modified as follows:

(1) FILTRATION TIME TESTING. Round upwards when reporting the filtration time, in minutes. For example, a filtration time of 4 minutes, 22 seconds, would be reported as 5 minutes.

(2) FLASH POINT TESTING. The referee procedure for performing flash point testing of JP-5 shall be the manual version of ASTM D93 as opposed to the automated version of ASTM D93.

(3) FLASH POINT.

(i) All batches of JP-5 that are presented for Government acceptance at origin and for subsequent shipment through a multiproduct pipeline, shall meet a minimum flash point requirement of 62.5°C.

(ii) In the U.S. all deliveries of JP-5 in the states of California, Oregon, and Washington shall have a minimum Flash Point of 62.5 oC at the custody transfer point.

(iii) In Australia all deliveries of JP-5 shall have a minimum Flash Point of 61.5°C at the custody transfer point.

(4) ACID NUMBER. For JP-5 fuels delivered to Kodiak Island, Alaska, the maximum total acid number shall be 0.020 mg KOH/g.

(5) MICRO-SEPAROMETER (MSEP) REQUIREMENTS.

(i) 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) and/or Corrosion Inhibitor/Lubricity Improver (CI/LI) after verification of product conformance with the MSEP requirement, the product is not required to meet a fixed limit on subsequent MSEP tests.

(ii) 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 jet fuel, FSII, CI/LI, and Antioxidant (only if required). The FSII shall be added to this hand blend at a concentration range between 0.10 volume percent minimum and 0.15 volume percent maximum. The amount of the CI/LI added to this hand blend shall be within the concentration range specified in QPL- 25017. The MSEP result on this hand blend is a REPORT ONLY requirement and shall be recorded corresponding to item 750X on the Standardized Test 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).”

(c) ADDITIVES.

(1) Additives are required for deliveries of JP-5, per MIL-DTL-5624W, unless addition is excluded by specific solicitation line item, applicable contract clause, or other contractual requirement. FSII included in jet fuel shall conform to MIL-DTL-85470B, Inhibitor, Icing, Fuel System, High Flash, Notice 1 dated March 24, 2004.

(2) The CI/LI additive(s) used shall confirm to MIL-PRF-25017H Inhibitor, Corrosion/Lubricity Improver, Fuel Soluble, w/Amendment 1, dated August 4, 2011 and be of the type and concentration cited in the Qualified Products Database (QPD). To locate this information: (1) Go to the Acquisition Streamlining and Standardization Information System (ASSIST) QuickSearch website (URL http://quicksearch.dla.mil/), (2) type "QPL-25017" in the Document ID field, press the submit button, (3) click the QPL-25017 search result under Document ID, and (4) click the "Qualification" link located in the upper right side of the webpage to be directed to QPL-25017.

Only the following CI/LI additives are approved for shipment to North Atlantic Treaty Organization (NATO) countries:

CI/LI

CONCENTRATION,

GRAMS/CUBIC METER

Innospec Fuel Specialties, LLC DCI-4A 9 – 24

Innospec Fuel Specialties, LLC DCI-6A 9 – 15

Afton Chemical Corp., Hitec 580 15 – 22.5

Nalco Co, Nalco 5403 12 – 22.5

Nalco Co, Nalco 5405 11 – 11

Baker Petrolite Corp., Tolad 4410 9 – 22.5

Baker Petrolite Corp., Tolad 351 9 – 24

Dorf Ketal Chemicals, Unicor J 9 – 22.5

GE Betz Inc., Spec-Aid 8Q22 9 – 24

(3) Line injection of additives (FSII and CI/LI) from shipping tank to delivery conveyance or other free on board (FOB) point is permitted under the following conditions:

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

(ii) When FSII is required, additive concentration must be verified based on a representative sample from each shipping conveyance.

(iii) Conformance to specification requirements at the custody transfer point is required, however, prior to shipment, a laboratory hand blend of JP-5 fuel with all additives required by this contract shall be tested to verify compliance with the required specification (except for MSEP). MSEP analysis shall be performed per the Contractor’s election in MIL-DTL-5624W.

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

(e) ADDITIONAL REQUIREMENT APPLICABLE TO DEEP FREEZE PROGRAM ONLY. The Deep Freeze Program is for Antarctic operations of the Department of Defense and other federal agencies, whereby JP-5 sulfur content shall not exceed

0.0015 mass-percent (15 ppm).

(f) BATCH SAMPLING: The Contractor shall provide one 20 mL sample per each individual tank in a procurement batch. The sample from each tank/batch shall be either an all-level sample or a composite of upper, middle, and lower samples. A copy of the full-specification test report shall accompany each sample. The sample container will be any 20 mL amber borosilicate vial with a polytetrafluoroethylene (PTFE) lined screw cap. A tracking number for the samples shall be provided to: Robert Morris at Robert.morris@nrl.navy.mil or (202) 767-3845. Samples shall be shipped to:

US Naval Research Laboratory ATTN: Robert Morris, Code 6181 JP-5 Component Analysis Library Project 4555 Overlook Ave., S.W.

Washington D.C. 20375-5320

The paperwork provided with these samples shall include the following information:

Contract Number Contractor’s Name Product Refinery Location Quantity of Tank/Batch

For samples containing synthetic components, include the following additional information:

Manufacturer of synthetic component Batch Number

Date of Test Report Quantity of Tank/Batch Percent Composition Production Process of Synthetic Component Feedstock

Signature

Prepared by

Quality Technical Support Office Approval

Contracting Approval

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

CHANG.PHILIP.H.1241943107

Digitally signed by CHANG.PHILIP.H.1241943107 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=CHANG.PHILIP.H.1241943107 Date: 2016.04.19 10:11:08 -04'00'

MARTIN.DOUGLAS.A.1297748064

Digitally signed by MARTIN.DOUGLAS.A.1297748064 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=MARTIN.DOUGLAS.A.1297748064 Date: 2016.04.19 10:31:33 -04'00'

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.

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

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

C16.23 FUEL, NAVAL DISTILLATE (F-76) (DLA ENERGY MAY 2016)

a) ENVIRONMENTAL: In delivering supplies and services under this contract, the Contractor shall conform to all Federal, State, and local environmental requirements applicable to the geographic location of the receiving activity on the date of delivery. The Contractor shall also comply with all applicable International Agreements, Treaties, Conventions, and the like to which the United States is a signatory or with whose terms the receiving activity has otherwise agreed to comply, including but not limited to, the requirements of MARPOL 73/78, Annex VI Regulations 14 & 18. The Contractor shall be responsible for determining the existence of all such requirements prior to the time deliveries are made.

1) In the event that an International, Federal, State, and / or local environmental requirement, as identified above, is more stringent than a requirement contained in this contract, the Contractor shall deliver product(s) that complies with the more stringent requirement. Product(s) that fails to meet the more stringent requirement will be considered nonconforming supply. Product(s) to be supplied shall fully meet the requirements of the applicable specification(s). In the event that compliance with the more stringent requirement causes the contractor to incur additional costs, the contractor may request an equitable adjustment.

2) Unless otherwise indicated by the Contractor in writing, prior to award, the product offered shall be required to fully meet all applicable specifications. The supplier shall provide to the receiving vessel a “Statutory Sample” of at least 400-mL in volume, taken from the receiving vessel’s inlet bunker manifold, together with a Bunker Delivery Note (BDN). This sample will be sealed and carry a sample tag that provides the documentation required per MARPOL 73/78, Annex VI Regulation 18.

b) SPECIFICATION: Military specification MIL-DTL-16884N dated 22 Apr 2014 applies.

c) SPECIFICATION MODIFICATIONS:

1) Flash Point: All batches of F-76 that are presented for Government acceptance at origin and for shipment through a multiproduct pipeline shall meet a minimum flash point requirement of 62.5 degrees Celsius.

2) Storage Stability: Total insolubles shall be less than 2.0 mg/100ml when ASTM D5304 is used and 1.0 mg/100ml when ASTM D2274 is used.

3) F-76 offered from a location other than where refined (excludes synthesized material as defined in section 3.2.1 of MIL-DTL- 16884N) requires testing for FAME content by test method ASTM D7963, BS EN 14078, or IP 579.

4) In Australia all deliveries of F-76 shall have a minimum Flash Point of 61.5°C at the custody transfer point.

d) MATERIALS: The F-76 supplied under this contract shall not contain un-hydrotreated light cycle oils or contain any stabilizer additives, or any other additive or material not explicitly allowed per section 3.2 of MIL-DTL-16884N.

1) For F-76 containing a synthetic component, the synthetic component shall be certified to Tables A-I and A-II of MIL-DTL-

16884N. It is not necessary to analyze each batch of the synthetic component for compliance with Table A-II once it is demonstrated that the process scheme is adequately controlled and if no significant changes to existing production operations have been made, such as a turnaround event on a refinery unit used to produce the synthetic component or a change in feedstock material. The signed F-76 synthetic component certification page shall be supplied for each shipment which includes synthetic paraffinic materials attesting that no changes to the production process have been made and certifying that the last certificate of analysis, dated and including Table A-II results, is still valid.

e) TRACEABILITY:

1) F-76 fuel supplied under this contract shall maintain traceability with respect to additives and materials, which is defined as the ability to trace the individual batch of fuel back to the original point of manufacture through documentation.

2) All traceability documentation shall be sufficient to guarantee that at no point have any unauthorized materials or additives been blended into the final product or any of is associated blend components per section 3.2 Material of MIL-DTL-16884N.

3) For all F-76 supplied, the traceability documentation shall consist of statement(s) attesting to the materials composition, which includes materials derived from non-petroleum sources, additives and their concentration levels.

4) If F-76 is produced by means of blending, the traceability requirement and documentation for additives and materials shall apply to each blending component used from the point of manufacture through the blend operation. Materials composition, additives and their concentration levels shall be included. The requirement and intent of traceability for blend components is not to obtain full certificates of analysis of each individual blend component, but for certification that no unapproved additives or materials are present in blend components used.

5) The form titled: “F-76 Traceability Signature Page” shall be used to document conformance with the provisions of this traceability paragraph. The offeror/supplier shall comply with this requirement utilizing one of the three options below and notification shall be provided to both the contracting office and PQIS@dla.mil during the pre-award phase which option was chosen for compliance. Documents provided in conjunction with individual shipments shall be uploaded into Wide Area Work Flow as attachments under the quality tab.

OPTION 1 – As part of the offeror submission package the offeror shall provide the traceability signature page from each entity in the supply chain providing and/or handling F-76 product and/or blending components all the way back to the point of manufacture. For each individual shipment, the supplier will submit a traceability page signed only by the awardee.

OPTION 2 – As part of the offer submission package the offeror shall provide the traceability signature page, signed only by the offeror. Upon award and prior to the first shipment the awardee shall provide the signed traceability signature page from each mailto:PQIS@dla.mil entity in the supply chain providing and/or handling F-76 product and/or blending components all the way back to the point of manufacture. For each individual shipment, the supplier will submit a traceability page signed only by the awardee.

OPTION 3 – As part of the offeror submission package, the offeror shall provide the traceability signature page, signed only by the offeror. For each individual shipment, the awardee shall provide the signed traceability signature page from each entity in the supply chain providing and/or handling F-76 product and/or blending components all the way back to the point of manufacture.

Regardless of the option chosen, the traceability sheet signed by offeror shall be submitted to both the contracting office and to PQIS@dla.mil during pre-award phase.

For OPTION 1 or OPTION 2, the purpose of the awardee submitting a signed traceability page with each shipment is to confirm that the initial traceability certification is still valid at the time of F-76 product shipment.

6) If at any point during the contract period the traceability information provided under OPTION 1 or OPTION 2 becomes invalid

(i.e. the supply chain is altered or the source of F-76 product or a blending component changes), the supplier shall notify both the contracting office and PQIS@dla.mil and updated documentation shall be provided.

f) ADDITIVES:

1) Lubricity Improver Additive (LIA) – Lubricity additives are allowed in F-76. The LIA additive(s) used shall conform to MIL-

PRF-32490, Additive, Lubricity Improver, Diesel, dated 3 Feb 2014 and be of the type and concentration cited in the Qualified Products Database (QPD). To locate this information: (1) Go to the Acquisition Streamlining and Standardization Information System (ASSIST) QuickSearch website (URL: http://quicksearch.dla.mil/), (2) type “QPL-32490” in the Document ID field, press the search button, (3) click the QPL-32490 search result under Document ID and (4) click the “View QPD Data” link to be directed to webpage showing all grades of additive qualified to MIL-PRF-32490. Either Grade A or Grade B material is suitable for treatment of de-sulfurized F-76. Additive concentration shall not exceed the maximum allowable concentration applicable to the specific additive selected for inclusion in finished F-76.

2) Information pertaining to qualification of additives not currently listed on QPL-32490 may be obtained from Commander, Naval Sea Systems Command, ATTN: SEA 05S, 1333 Isaac Hull Avenue, SE, Stop 5160, Washington Navy Yard, DC 20376-5160, USA, or by e-mailing CommandStandards@navy.mil.

3) Dyes And Markers - Red dye required in off-highway diesel fuel in accordance with 40 CFR Part 80 as modified by the Environmental Protection Agency's interim final rule published in the Federal Register dated July 14, 1994 shall not be added to F-76. The finished product shall show no visual evidence of red dye. This F-76 product is for military, off-highway use only and must be segregated at all times from any diesel fuel used on-highway. NOTE: Red dye does not apply to Atlantic/Europe/Mediterranean or Western Pacific Overseas Bulk purchase programs unless offering refinery is located in the United States or one of its possessions.

g) BATCH SAMPLING: The Contractor shall provide one 20 mL sample per each individual tank in a procurement batch. The sample from each tank/batch shall be either an all-level sample or a composite of upper, middle, and lower samples. A copy of the full-specification test report shall accompany each sample. The sample container will be any 20 mL amber borosilicate vial with a polytetrafluoroethylene (PTFE) lined screw cap. A tracking number for the samples shall be provided to: Robert Morris at Robert.morris@nrl.navy.mil or (202) 767-3845. Samples shall be shipped to:

US Naval Research Laboratory ATTN: Robert Morris, Code 6181 F76 Component Analysis Forensic Project 4555 Overlook Ave., S.W.

Washington D.C. 20375-5320

The paperwork provided with these samples shall include the following information:

Contract Number Contractor’s Name Product Refinery Location Quantity of Tank/Batch

For samples containing synthetic components, include the following additional information:

Manufacturer of synthetic component Batch Number Date of Test Report Quantity of Tank/Batch Percent Composition Production Process of Synthetic Component Feedstock mailto:PQIS@dla.mil http://quicksearch.dla.mil/ mailto:CommandStandards@navy.mil mailto:Robert.morris@nrl.navy.mil

F-76 Traceability Signature Page

Contract or Solicitation Number:

CLIN:

Order Number:

Shipment Number:

Traceability OPTION selected per paragraph e.5 (circle or otherwise indicate which one of the three options is chosen):

OPTION 1 OPTION 2 OPTION 3

F-76 fuel supplied under the above contract, CLIN, order number and shipment number maintains traceability with respect the materials composition, additives and their concentration levels. This signed statement certifies that at no point have any unauthorized un-hydrotreated light cycle oils, other unauthorized materials, or additives been blended into the final product or any of its associated blend components per the most recent revision of MIL-DTL-16884 at date of contract award. All materials and additives are listed below. The percentage of each material as defined in section 3.2 and 3.2.1 (i.e. refined hydrocarbon distillate fuel, Fischer-Tropsch, Hydroprocessed Renewable Diesel, etc.) and the concentration level for each additive are also shown. For the purposes of the offeror submission this signed statement attests that no unapproved additives or materials will be added to batches or components of batches of F-76 for delivery under government contracts.

Signature:

Printed Name:

Title:

Company Name:

Date:

Material Percent

Additive Concentration Responsible Party for Injection

F-76 Synthetic Component Certification

Contract or Solicitation Number:

CLIN:

Order Number:

Shipment Number:

Synthetic paraffinic materials supplied as indicated with the above contract, CLIN, order number, and shipment number is derived from either Fischer-Tropsch (FT) or Hydroprocessed Renewable Diesel (HRD) methods. This signed statement certifies that since the last certificate of analysis (COA), including table A-II results of MIL-DTL-16884N, Appendix A, no changes, including feedstock material, production location, or production processes have been made. In addition, no turnaround events have been executed on any units utilized to produce the synthetic paraffinic materials since the last COA, including table A-II, properties were tested. Please supply the date of the most recent COA and an identifying number for that report in the space provided below.

DATE OF COA: ____________________________________

LAB REPORT ID NUMBER__________________________

Signature:

Printed Name:

Title:

Company Name:

Date:

Quality / Technical Support Office Approval:

Contracting Approval:

Legal Approval:

(Only required for E QAPs)

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

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

(WESTPAC) (ATL/EUR/MED) (PC&S) (DLA ENERGY JAN 2016)

(a) Nomenclature for Aviation Turbine Fuel (JP8) is shown below:

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

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

(b) INCIDENTAL CONTAMINANTS. Particulate Matter and Fatty Acid Methyl Ester (FAME) content shall not exceed the limits outlined in Table III of MIL-DTL-83133J dated December 16, 2015.

(c) SPECIFICATION MODIFICATIONS. Aviation Turbine Fuel (JP8) shall conform to MIL-DTL-83133J modified as follows:

(1) TESTING

(i) FILTRATION TIME (FT) 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.

(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-83133J, paragraph 3.4, 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 Standard Test Method for Free Water and Particulate Contamination in Distillate Fuels, ASTM D4176, 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- 83133J, Table III, the workmanship criteria is met. 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 (70 degrees Fahrenheit) 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 degrees Celsius (70 degrees Fahrenheit).

(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.

(d) ADDITIVES. Additives are required for deliveries of JP8 per MIL-DTL-83133J, unless addition is excluded by specific solicitation line item, applicable contract clause, or other 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) QuickSearch 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 "View QPD Data" link under Overview , 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 shall not be used in JP8 unless the Contractor has obtained written consent from the Contracting Officer.

(3) The requirement for static dissipater additive (SDA) (see MIL-DTL-83133J, paragraph 3.3.3 and fuel electrical conductivity requirement in Table I) shall not apply unless stated otherwise in the Schedule.

(4) 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 must be tested to verify compliance with the specification.

(ii) Additives must 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 must 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 is not required to report or verify the conductivity level on a representative sample from the conveyance. This does not relieve the Contractor of the requirement to inject SDA homogeneously and in sufficient quantity to obtain a conductivity level which the Contractor would anticipate to be within the specification limits once the fuel is at equilibrium. The receiving activity will measure the conductivity and advise the Contractor if it does not meet the specification requirements and the Contractor shall adjust the SDA injection quantity accordingly.

(5) SPECIAL LOCATION REQUIREMENTS (AEM 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 antioxidants (AO) are 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 static dissipater additive (SDA) (see MIL-DTL-83133J, paragraph

3.3.3 and fuel electrical conductivity requirement in Table I) shall not apply unless stated otherwise in the Schedule.

Quality / Technical Support Office Approval:

Contracting Approval:

Legal Approval:

(Only required for E QAPs)

DMM0076

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