Attachment 2 - C QAPS.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

C16.64-3 TURBINE FUEL, AVIATION (AN8) (DEEP FREEZE) (PC&S) (DLA ENERGY OCT 2018)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

9130-01-373-0208 Turbine Fuel, Aviation AN8

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) Aviation Turbine Fuel (AN8) is used for Antarctic fuels operations. See nomenclature above. While a special low freezing point is required, minimum flash point of 38 degrees Celsius (°C) (100 degrees Fahrenheit [°F]) shall be maintained.

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

(1) TABLE I MODIFICATIONS:

(i) TOTAL SULFUR CONTENT shall not exceed 0.0015 mass percent (15 ppm).

(ii) FREEZING POINT shall be minus 58 °C (minus 72 °F) or lower.

(iii) FUEL SYSTEM ICING INHIBITOR (FSII) content shall be between 0.10 and 0.15 volume percent.

(iv) MICROSEPAROMETER (MSEP) RATING LIMITS. See MIL-DTL-83133K, 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 0.10 to 0.15 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).”

(2) WORKMANSHIP. The workmanship criteria in MIL-DTL-83133K, 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 approved test methods. ASTM D4176 or ASTM D6986 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 °C (70 °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.”

(i) ASTM D6986 shall be the referee test method, see requirements, as drafted, in MIL-DTL-83133K, section 3.5.

(ii) For 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.

(3) TABLE IV MODIFICATIONS.

DEFENSE LOGISTICS AGENCY ENERGY Page 2 of 2

FORT BELVOIR, VIRGINIA 22060-6222

Signature

Prepared by:

Quality/Technical Support Office Approval

Contracting Approval:

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

(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.

(c) ADDITIVES. Additives are required for deliveries of AN8 per MIL-DTL-83133K, 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 " 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 AN8 unless the Contractor has obtained written consent from the Contracting Officer.

(3) 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 proportionally 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.

MEREDITH.MICHAEL.E.1290973453 Digitally signed by MEREDITH.MICHAEL.E.1290973453 Date: 2018.10.10 15:25:04 -04'00'

BANISZEWSKI.DANIEL.J.128738869

Digitally signed by

BANISZEWSKI.DANIEL.J.1287388698

Date: 2018.10.17 11:34:44 -04'00'

CATLIN.JOSHUA.D.1276289540 Digitally signed by CATLIN.JOSHUA.D.1276289540 Date: 2018.10.17 11:01:34 -04'00'

DEFENSE LOGISTICS AGENCY ENERGY Page 1 of 1

FORT BELVOIR, VIRGINIA 22060-6222

Signature

Prepared by:

Quality/Technical Support Office Approval

Contracting Approval:

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

C16.69-2 GASOLINE AUTOMOTIVE, UNLEADED, MIDGRADE (MUM) (PC&S) (DLA ENERGY JUN 2017)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

9130-01-272-0983 Gasoline, Midgrade Unleaded MUM

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, MIDGRADE. Gasoline shall conform to each countries specification as listed below:

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 midgrade 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.

COUNTRY SPECIFICATION NATIONAL STOCK NUMBER

AUSTRALIA FUEL STANDARD (PETROL) 2001

CANADA CAN/CGSB-3.5-2001

COSTA RICA RTCA 75.01.20:04

EL SALVADOR RTCA 75.01.20:04

GUATEMALA RTCA 75.01.20:04

HONDURAS RTCA 75.01.20:04 9130-01-272-0983

NICARAGUA RTCA 75.01.20:04

PHILLIPINES PNS/DOE QS 008:2012

MIDDLE EAST EN 228

ALL OTHER REGIONS ASTM D4814

MEREDITH.MICHAEL.E.1290973453 Digitally signed by MEREDITH.MICHAEL.E.1290973453 Date: 2017.06.07 13:33:52 -04'00'

BANISZEWSKI.DANIEL.J.1287388698 Digitally signed by BANISZEWSKI.DANIEL.J.1287388698 Date: 2017.06.07 14:15:28 -04'00'

PETERSON.DAVID.W.1074069483 Digitally signed by PETERSON.DAVID.W.1074069483 Date: 2017.08.24 07:16:28 -04'00'

DEFENSE LOGISTICS AGENCY ENERGY Page 1 of 2

C16.01 TURBINE FUEL, AVIATION (JP5) (DLA ENERGY APRIL 2018)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT

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

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

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

a. 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.

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

c. 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 JP-5 deliveries in California, Oregon, and Washington shall have a minimum Flash Point of 62.5 oC at the custody transfer point.

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

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

e. MICRO-SEPAROMETER (MSEP) REQUIREMENTS.

i. Prior to initial production under this contract, the Contractor shall elect, on a one-time basis, which MSEP limit to meet 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 0.08 volume percent minimum and 0.11 volume percent maximum. The amount of the CI/LI added to this hand blend shall be within the concentration range specified in QPL-25017.

f. 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).

(b) ADDITIVES.

a. 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 June 15, 1999 and revalidated March 24, 2004.

b. The CI/LI additive(s) used shall conform to MIL-PRF-25017H Inhibitor, Corrosion/Lubricity Improver, Fuel Soluble, w/Amendment 1, dated August 4, 2011

c. 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.

(c) 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) BATCH SAMPLING: The Contractor shall provide one 20 mL sample per each individual tank in a procurement batch.

NOTE: This sample is in addition to those required in accordance with Quality Assurance Provision (QAP) E1

QUANTITY OF SAMPLE WHEN SAMPLED SUBMISSION PERIOD

20 mL Upon completion of each individual procurement batch Shipped within 30 days of procurement batch delivery

“Batch” Definition in accordance with MIL-STD-3004, 3.1.9: A specific quantity of product that is processed or utilized as a single unit and tested to meet test criteria and specifications.

DEFENSE LOGISTICS AGENCY ENERGY Page 2 of 2

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 batch’s full-specification test report shall accompany each sample. The sample container shall be any 20 mL amber borosilicate vial with a polytetrafluoroethylene (PTFE) lined screw cap. A tracking number for the samples shall be provided to: Thomas Loegel at thomas.loegel@nrl.navy.mil or (202) 767-1716. Samples shall be shipped to:

US Naval Research Laboratory ATTN: Thomas Loegel, 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 mailto:Robert.morris@nrl.navy.mil

C16.01 TURBINE FUEL, AVIATION (JP5) (DLA ENERGY APRIL 2018)

c. FLASH POINT.

e. MICRO-SEPAROMETER (MSEP) REQUIREMENTS.

(b) ADDITIVES.

c. 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:

2018-04-25T09:13:12-0400

YEN.CHENG.H.1539446041

2018-04-25T09:18:48-0400

BANISZEWSKI.DANIEL.J.1287388698

2018-04-26T16:45:01-0400

SHEPHERD.SANDRA.S.1012568459