Attachment 2 - C QAPS_Updated.pdf
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- Solicitation number
- SPE602-23-R-0711
- Issued by
-
Defense Logistics Agency Energy
About this file
This document contains specifications for various aviation and ground fuel products required by the Defense Logistics Agency Energy. Key details include:
The specifications cover aviation turbine fuel grades JP-5 and AN-8 to be used in Antarctica, as well as unleaded midgrade gasoline. The fuels must meet military standards modified as specified, including sulfur content limits of 15 ppm for JP-5 and AN-8, freezing point of minus 58°C for AN-8, and flash point minimums varying by location. Additives such as fuel system icing inhibitors and corrosion inhibitors are required and must meet additional military standards. Samples from each procurement batch of JP-5 must be provided for testing.
The solicitation seeks bulk petroleum products to meet the specifications for delivery to Antarctica under solicitation SPE602-23-R-0711 issued by the Defense Logistics Agency Energy. Compliance with environmental regulations and fuel quality at the custody transfer point are emphasized.
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DEFENSE LOGISTICS AGENCY ENERGY
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 DEC 2022)
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, 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 0.10 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, 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 approved test methods. The latest versions of 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 the latest revisions of either D4176 or D6986.”
(i) ASTM D6986, latest version, shall be the referee test method, see requirements, as drafted, in MIL-DTL-83133K, dated July 18, 2018, section 3.5.
FORT BELVOIR, VIRGINIA 22060-6222
DISTRIBUTION STATEMENT – A: APPROVED FOR PUBLIC RELEASE. DISTRIBUTION IS UNLIMITED
(ii) For ASTM D 4176, latest version, 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, dated July 18, 2018, Table IV, the workmanship criteria is met.
(3) TABLE IV MODIFICATIONS.
(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, 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) 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.
Signature
Prepared by: Digitally signed by
Quality/Technical Support Office Approval
Digitally signed by
Contracting Approval:
Digitally signed by
RALPH.ERIN.S.1229663042 Digitally signed by RALPH.ERIN.S.1229663042 Date: 2022.12.20 10:08:08 -05'00'
BANISZEWSKI.DANIEL.J.1287388698 Digitally signed by BANISZEWSKI.DANIEL.J.1287388698 Date: 2022.12.22 13:26:05 -05'00'
FORT BELVOIR, VIRGINIA 22060-6222
FORT BELVOIR, VIRGINIA 22060-6222
C16.01 TURBINE FUEL, AVIATION (JP5) (DLA ENERGY DEC 2022)
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, revalidated December 31, 2020.
(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 the latest revision 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. This requirement is meant to address multiproduct commercial pipelines and does not apply to multiproduct systems within a facility.
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, dated March 28, 2016, revalidated December 31, 2020, unless addition is excluded by specific solicitation line item, applicable contract clause, or another 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 August 28, 2019.
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, and revalidated May 25, 2021,
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, dated March 28, 2016, and revalidated December 31, 2020.
(d) BATCH SAMPLING: The Contractor shall provide one 20 mL sample per each individual tank in a procurement batch.
For each 20 mL sample provided by the Contractor, the Contractor shall also submit a Refinery Certificate of Quality (RCQ), or Certificate of Analysis (CoA), as applicable, with the JP-5 sample when submitting to the US Naval Research Laboratory. The RCQ or CoA for each individual tank shall be representative of Level A testing for the JP-5 product.
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-3004-1A, 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.
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
• Full-Specification Test Report
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
• Full-Specification Test Report
Signature Prepared by
Quality Technical Support Office Approval
Contracting Approval mailto:Robert.morris@nrl.navy.mil
C16.01 TURBINE FUEL, AVIATION (JP5) (DLA ENERGY DECJUL 2022APRIL 2018)
c. FLASH POINT.
e. MICRO-SEPAROMETER (MSEP) REQUIREMENTS.
(b) ADDITIVES.
NOTE: This sample is in addition to those required in accordance with Quality Assurance Provision (QAP) E1
2022-12-20T10:32:42-0500
RALPH.ERIN.S.1229663042
2022-12-22T13:27:12-0500
BANISZEWSKI.DANIEL.J.1287388698
2022-12-27T09:36:58-0500
MACLANE.SKYLLAR.BRYANNA.1252141827
DEFENSE LOGISTICS AGENCY ENERGY Page 1 of 1
Signature
Prepared by:
Quality/Technical Support Office Approval
Contracting Approval:
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
2017-06-07T13:33:52-0400
MEREDITH.MICHAEL.E.1290973453
2017-06-07T14:15:28-0400
BANISZEWSKI.DANIEL.J.1287388698
2017-08-24T07:16:28-0400
PETERSON.DAVID.W.1074069483
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