Amedment0001.pdf
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- Solicitation number
- SP0600-14-R-0161
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- Defense Logistics Agency Energy
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Amendment 0001
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|---|---|---|
| J A_PetroStar.pdf | ||
| Summary_of_Award.pdf | ||
| Min_Laid-Down_Cost_Solution_Contractor_Summary.pdf | ||
| Min_Cost_Solution_Bid_Evaluation_Sheet.pdf | ||
| Min_Cost_Solution_Bid_Award_Sheet.pdf | ||
| Amend_0009.pdf | ||
| Amendment0008.pdf | ||
| Amend_07.pdf | ||
| amend0006.pdf | ||
| Amend0005.pdf | ||
| Amend0004.pdf | ||
| Amend0003.pdf | ||
| Amendment0002_FBO.pdf | ||
| OSP_Attach2.pdf | ||
| OSP_Attach1.pdf | ||
| 14R0161_OSP_FINAL.doc | DOC document | |
| 14R0161_ADD_PKG_FINAL.pdf | ||
| 14R0161_OSP_FINAL.pdf | ||
| 14R0161_Solicitation_FINAL.pdf | ||
| 14R0161_OSP_DRAFT.docx | DOCX document | |
| 14R0161_ADD_PKG_DRAFT2.docx | DOCX document | |
| 14R0161_Solicitation_DRAFT.doc | DOC document | |
| Solicitation_14R0161-DRAFT.doc | DOC document |
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SP0600-14-R-0161
Amendment 0001
Block 14 (CONT’D)
A. Page 2, item number 1 of the solicitation has been updated to read the following:
The following quantities are estimated maximum quantities. The actual purchases will be made pursuant to orders placed in accordance with FAR 52.216-22 INDEFINITE QUANTITY (OCT 1995) and FAR 52.216-18 ORDERING (OCT 1995).
LOCATION: ROCKY MOUNTAIN/WEST COAST/OFFSHORE
TURBINE FUEL, AVIATION JP8: 3,406,000 USG
TURBINE FUEL, AVIATION JP5: 107,929,000 USG
FUEL NAVAL, DISTILLATE F76: 120,217,000 USG
TURBINE FUEL, AVIATION. JAA*: 392,801,000 USG
TURBINE FUEL, AVIATION JP4: 843,000 USG
TURBINE FUEL, AVIATION JA1: 103,929,000 USG
*JAA is the product code for Jet A
B. General Note 17 has been added to the solicitation package to read the following:
“For deliveries in California, Oregon and Washington, all JP-5 will have a minimum Flash Point of 62.5 degrees C.”
C. Line items 0601 and 0602 are hereby modified to include the additive requirements for FSII.
The line items now read as follows:
0601 DFSP PEARL HARBOR, PEARL HARBOR, HI
N00604 890510000 PEARLHRBR
QUANTITY 1,925,000 8A QUANTITY 0 SA QUANTITY 0
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
TANKER REQUIRED NONE REQUIRED 294,000 BBLS
BARGE REQUIRED NONE REQUIRED 50,000 BBLS
PIPE REQUIRED NONE REQUIRED
0602 DFSP PEARL HARBOR, PEARL HARBOR, HI
N00604 890510000 PEARLHRBR
QUANTITY 400,000 8A QUANTITY 0 SA QUANTITY 0
** END USER CAN BE SUPPLIED THROUGH TERMINAL DFSP PEARL HARBOR
MODE RECEIPT% FSII SDA CI MAX PARCEL
MIN PARCEL
TANKER REQUIRED NONE REQUIRED 294,000 BBLS
BARGE REQUIRED NONE REQUIRED 50,000 BBLS
PIPE REQUIRED NONE REQUIRED
D. Line items 0115, 0145, 0301, 0303, 0512, 0513 and 0605 are hereby modified to include MAX PARCEL sizes for tanker and barge modes. The line items read as follows:
0115 DFSP CARSON, Carson, CA
UY7357 883245271 DFSPCARSON
QUANTITY 120,959,000 8A QUANTITY 0 SA QUANTITY 0
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
PIPE NONE NONE NONE
TANKER NONE NONE REQUIRED 248,500 BBLS
0145 NAS WHIDBEY, OAK HARBOR, WA
N00620 844905290 WHIDBEY
QUANTITY 20,112,000 8A QUANTITY 0 SA QUANTITY 18,100,800
** END USER CAN BE SUPPLIED THROUGH TERMINAL DFSP PUGET SOUND
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
BARGE REQUIRED REQUIRED REQUIRED 50,000 BBLS
0301 DFSP PEARL HARBOR, PEARL HARBOR, HI
N00604 890510000 PEARLHRBR
QUANTITY 53,189,000 8A QUANTITY 0 SA QUANTITY 0
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
TANKER REQUIRED REQUIRED REQUIRED 280,500 BBLS
PIPE REQUIRED REQUIRED REQUIRED
0303 MCAS KANEOHE, HI
N00318 890570280 KANEOHE
QUANTITY 7,814,000 8A QUANTITY 0 SA QUANTITY 0
** END USER CAN BE SUPPLIED THROUGH TERMINAL DFSP PEARL HARBOR
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
BARGE REQUIRED REQUIRED REQUIRED 50,000 BBLS
TRUCK REQUIRED REQUIRED REQUIRED
0512 DFSP PUGET SOUND, WA
N00406 845459290 PUGET
QUANTITY 8,074,000 8A QUANTITY 0 SA QUANTITY 0
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
TANKER NONE NONE REQUIRED 322,000 BBLS
BARGE NONE NONE REQUIRED 50,000 BBLS
0513 DFSP PUGET SOUND, WA
N00406 845459290 PUGET
QUANTITY 8,074,000 8A QUANTITY 0 SA QUANTITY 0
** END USER CAN BE SUPPLIED THROUGH TERMINAL DFSP PUGET SOUND
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
TANKER NONE NONE REQUIRED 322,000 BBLS
BARGE NONE NONE REQUIRED 50,000 BBLS
0605 CG SUPPORT CNTR, KODIAK, AK
Z46000 813039260 KODIAK
QUANTITY 2,200,000 *** 8A QUANTITY 0 SA QUANTITY 0
MODE RECEIPT% FSII SDA CI MAX PARCEL MIN
PARCEL
TANKER REQUIRED NONE REQUIRED 294,000 BBLS
BARGE REQUIRED NONE REQUIRED 40,000 BBLS
PIPE NONE NONE REQUIRED
E. FAR 52.216-9069 ECONOMIC PRICE ADJUSTMENT – PUBLISHED MARKET PRICE-
DOMESTIC BULK (NOV 2011) is hereby updated as follows:
I II III IV V
Heading under which Base market price market indicator Location where as of Jan 14, 2014 Name of is published and market price (excludes all taxes) Item No. Publication name of product is applicable (see note(s) below)
ROCKY PLATTS JET KERO 54 U.S. GULF COAST 2.909740
MOUNTAIN OILGRAM PIPELINE
JP8/JAA PRICE REPORT
The reference price shall be determined as follows: 100% U.S. Gulf Coast Pipeline (Average of Low and High)
ALASKA OIL PRICE PAD 5 – UNLEADED ANCHORAGE $3.105568
JP4 OR INFORMATION
JET B SERVICES
The reference price shall be determined as follows: 70% OPIS UNLEADED AVERAGE ANCHORAGE
+ 30% OPIS ANCHORAGE DELIVERED SPOT .
F. Contract provision C-0003 titled “C.16.01 TURBINE FUEL AVIATION (JP5)(BULK)(DLA ENERGY SEP 2013)” is hereby deleted in its entirety and replaced with the full clause and incorporated editorial revisions:
C-0003 C16.01 TURBINE FUEL, AVIATION (JP5) (BULK) (DLA ENERGY SEP 2013)
(a) Product shall meet MIL-DTL-5624V, dated July 11, 2013, Turbine Fuel, Aviation, Grade JP5
(b) SPECIFICATION MODIFICATION: The requirements of Table II 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) HYDROGEN CONTENT. ASTM D 5291 may be used in lieu of ASTM D 3701 or D7171.
(3) FLASH POINT TESTING. The referee procedure for performing flash point testing of JP5 shall be the manual version of ASTM D 93 as opposed to the automated version of ASTM D 93.
(4) FLASH POINT. All batches of JP5 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°C.
(5) MICRO-SEPAROMETER (MSEP) REQUIREMENTS. 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.
(6) 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 handblend containing jet fuel, FSII, CI/LI, and Antioxidant (only if required). The MSEP result on this handblend is a REPORT ONLY requirement and shall be recorded corresponding to item 750X, both on the Standardized Test Report Form (see Attachment _____) and on the DD Form 250-1. 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).”
(7) THERMAL STABILITY. The Standard Test Method for Thermal Oxidation Stability of Aviation Fuels, ASTM D3241, shall be performed according to either Option A or B.
Regardless of which option is chosen (Option A or B above), the test temperature and the results of the test shall be recorded on the DD Form 250-1 and on the Standardized Test Report Form.
(i) OPTION A. The thermal stability test shall be performed with the temperature of the test being 260 degrees Celsius (500 degrees Fahrenheit), in accordance with the requirements of MIL-DTL-5624V, and will be the basis for the acceptance or rejection of fuel. However, an additional test shall be performed with the temperature of the test being 275 degrees Celsius (530 degrees Fahrenheit) and this result shall be REPORT ONLY.
(ii) OPTION B. The thermal stability test shall be performed with the temperature of the test being 275 degrees Celsius (530 degrees Fahrenheit). If the fuel fails the test at 275 degrees Celsius, a second test shall be performed at 260 degrees Celsius (500 degrees Fahrenheit). When both tests are performed, the results of the test at 260 degrees Celsius (500 degrees Fahrenheit) will be the basis for acceptance or rejection of the product.
(c) ADDITIVES.
(1) Additives are required for deliveries of JP5, per MIL-DTL-5624V, 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, Notice 1 dated March 24, 2004.
(2) The DD Form 250-1 for marine shipments shall cite the type, name, and amount (in milligrams per liter) of additives added to the fuel at the production or loading facility.
(3) The CI/LI additive(s) used shall be of the type and concentration cited in the Qualified Products Database (QPD). To locate this information: (1) Go to the 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, Hitec 580 15 – 22.5 Nalco Co, Nalco 5403 12 – 22.5 Nalco Co, Nalco 5405 11 – 11 Baker Petrolite, Tolad 4410 9 – 22.5 Baker Petrolite, Tolad 351 9 – 24 Dorf Ketal Chemicals, Unicor J 9 – 22.5 Spec-Aid 8Q22 9 – 24
(4) Line injection of additives (FSII and CI/LI) from shipping tank to delivery conveyance or other f.o.b. 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 shipment sample(s).
(iii) Conformance to specification requirements at the custody transfer point is required, however, prior to shipment, a laboratory handblend of jet 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-5624V, dated July 11, 2013.
(d) REPORTS. Refer to the MATERIAL INSPECTION AND RECEIVING REPORT contract provision for reporting requirements.
http://quicksearch.dla.mil/
(e) ADDITIONAL REQUIREMENT APPLICABLE TO DEEP FREEZE PROGRAM ONLY. The Deep Freeze Program is for Antarctic operation for Department of Defense and other federal agencies. JP5 sulfur content shall not exceed 0.0015mass% (15 ppm).
G. Contract provision C-0004 titled “C16.01-5 TURBINE FUEL, AVIATION (JP4)(BULK)(DLA ENERGY JAN 2012)” is deleted in its entirety and replaced with the following updated clause:
C-0004 C16.01-5 TURBINE FUEL, AVIATION (JP4) (BULK) (DLA ENERGY MAR 2014)
(a) Specification MIL-DTL-5624V, dated July 11, 2013, Turbine Fuel, Aviation, Grade JP4, applies.
The requirements of Table II 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) 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 handblend containing jet fuel, FSII, CI/LI, and Antioxidant (AO) (AO only if required). The MSEP result on this handblend is a REPORT ONLY requirement and shall be recorded corresponding to item 750X, both on the Standardized Test Report Form (see Attachment _____) and on the DD Form 250-1. 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).”
(3) THERMAL OXIDATION STABILITY. The Standard Test Method for Thermal Oxidation Stability of Aviation Fuels , ASTM D 3241, shall be performed according to either Option A or B described below:
(i) OPTION A. In addition to the thermal oxidation stability testing requirements of MIL-DTL- 5624V, an additional thermal oxidation stability test , which will not be the basis for acceptance or rejection of the fuel, shall be performed with the temperature of the test being 275 degrees Celsius (530 degrees Fahrenheit).
Shipments will not be delayed pending results of this additional thermal oxidation stability test and the result shall be
REPORT ONLY.
(ii) OPTION B. The thermal oxidation stability test shall be performed with the temperature of the test being 275 degrees Celsius (530 degrees Fahrenheit) in lieu of the normal 260 degrees Celsius (500 degrees Fahrenheit). If the fuel fails the test at this temperature, a second test will be performed at 260 degrees Celsius (500 degrees Fahrenheit). If both tests are performed, the results of the test at 260 degrees Celsius (500 degrees Fahrenheit) will be the basis for acceptance or rejection of the fuel.
(iii) Regardless of which option is chosen (Option A or B above), the test temperature and the results of the thermal oxidation stability test shall be recorded on the DD Form 250-1 and on the Standardized Test Report Form. If using the Standardized Test Report Form, the results obtained at 260 degrees Celsius shall be reported as using series “B” for item numbers 601and 602. If another temperature is used, use series “A” to report the results and item 604 to report the test temperature.
(4) EXISTENT GUM. The preferred vaporizing medium for aviation turbine fuel is steam, however, the existent gum test (ASTM D 381) may be performed using air as the vaporizing medium at the following operating temperatures: Bath: 232 to 246 degrees Celsius; Test well: 229 to 235 degrees Celsius. If air is used instead of steam while performing ASTM D 381, it must be reported. In case of a failure with air, the sample must be retested using steam.
(b) ADDITIVES.
(1) Additives are required for deliveries of JP4, per MIL-DTL-5624V, unless addition is excluded by specific solicitation line item, applicable contract clause, or other contractual requirement. Additives shall not be premixed with other additives before injection into the fuel.
(2) FSII included in jet fuel shall conform to MIL-DTL-85470B revalidated on March 24, 2004.
(3) The DD Form 250-1 for marine shipments shall cite the type, name, and amount (in milligrams per liter) of additives added to the fuel at the production or loading facility.
(4) The Corrosion Inhibitor/Lubricity Improver (CI/LI) additive(s) shall conform to MIL-PRF- 25017H, Amendment 1, dated August 4, 2011, and shall be listed in the electronic Qualified Products List (QPL)- 25017 located in the Qualified Products Database (QPD). To locate this information: (1) Go to the ASSIST QuickSearch website (URL http://quicksearch.dla.mil/) or to the assistdocs.com website (URL http://assistdocs.com), (2) type "QPL-25017" in the Document ID field and press the submit button, (3) click the QPL-25017 search result under Document ID, and (4) click either the "Qualification" link (under Overview) or the "View QPD data" link (under Revision History) to be directed to QPL-25017. The concentration of CI/LI added to the fuel must be between the minimum effective concentration and the maximum allowable concentration as listed for a CI/LI in QPL-25017.
(5) For JP4 containing hydrogen-treated blending stocks, the following applies: Where a finished fuel consists of a blend of hydrogen-treated and nonhydrogen-treated components, the requirement for mandatory addition of antioxidant (MIL-DTL-5624V, paragraph 3.3.1) applies only to the portion of the blend that has been hydrogen treated. In such cases the proportion of the blend that has been hydrogen treated shall be reported.
(6) Line injection of additives (FSII and CI/LI) from shipping tank to delivery conveyance or other f.o.b. 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 samples(s) representative of the entire shipment.
(iii) Conformance to specification requirements at the custody transfer point is required, however, prior to shipment, a laboratory handblend of jet fuel with all additives required by this contract shall be tested to verify compliance with the required specification (except for Reid Vapor Pressure (RVP) and MSEP). Using a separate representative sample, RVP analysis of JP4 shall be performed without the additives present due to the sensitivity of the test to sampling and handling. MSEP analysis shall be performed per the Contractor’s election in MIL-DTL-5624V
(7) When the addition of Static Dissipater Additive (SDA) is required by the contract, the new formulation of STADIS 450 (active ingredient dinonylnaphthylsulfonic acid (DINNSA)) shall be used.
(8) With the exception of the fuel electrical conductivity test requirement, JP4 must meet the specification test requirements of MIL-DTL-5624V with all additives required by this contract included, except SDA. After verifying specification conformance, SDA, when required by this contract, shall be added proportionately to obtain a conductivity range of 150-600 picosiemens per meter. SDA will not be preblended with FSII, but may be injected simultaneously. The Contractor is not required to report or verify the conductivity level when SDA is injected while loading delivery conveyances due to the SDA equilibrium rate in JP4. The receiving activity will measure the conductivity and advise the Quality Representative to have the Contractor adjust the SDA injection quantity if necessary.
(9) SDA is required to be added to all JP4 shipped directly to an end user without passing through a terminal. SDA is not required in shipments to a terminal.
(c) REPORTS. Refer to the MATERIAL INSPECTION AND RECEIVING REPORT contract provision for reporting requirements.
H. Contract provision C-0005 titled “C16.08-1 TURBINE FUEL, AVIATION (JET A/JET A- 1)(BULK)(DLA ENERGY APR 2013)” is hereby deleted in its entirety and replaced with the following updated clause:
C-0005 C16.08-1 TURBINE FUEL, AVIATION (JET A/JET A-1) (BULK) (DLA ENERGY MAR 2014) Jet A/Jet A-1 shall conform to the requirements of ASTM D 1655, Standard Specification for Aviation Turbine Fuels, except as modified below, at the custody transfer point
(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.
(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.
(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/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)
REPORTS. Refer to the MATERIAL INSPECTION AND RECEIVING REPORT contract provision for reporting requirements.
I. Contract provision C-0006 titled “C16.09 TURBINE FUEL, AVIATION (JET A/A1/A50)(DLA ENERGY MAR 2013)” is hereby deleted in its entirety.
J. Contract provision E-0001 titled “E1CONTRACTOR INSPECTION RESPONSIBILITIES (DLA ENERGY SEP 2013)” is hereby revised to read as follows:
http://assistdocs.com/
E-0001 E1 CONTRACTOR INSPECTION RESPONSIBILITIES (DLA ENERGY SEP 2013)
(a) This contract provision applies to:
(1) All aviation fuel, lubricating oil, and additive shipments.
(2) All Bulk and Posts, Camps, and Stations non-aviation fuel shipments via pipeline or waterborne transport.
(b) QUALITY CONTROL PLAN.
(1) The Contractor is required to provide and maintain an inspection system, and a written description (Quality Control Plan (QCP)) of that system, acceptable to the Government. The Contractor has the option to provide and maintain an inspection system that, as a minimum, incorporates the requirements of ISO9001, Quality Management Systems. If the Contractor chooses to comply with the ISO9001 quality system requirements and format, all the specific Quality Assurance Provisions of this contract must be included in the resulting ISO9001 document that will serve as the QCP. A copy of the QCP, in English, shall be presented to the Government Quality Assurance Representative (QAR) for their review and acceptance prior to commencement of production or services. An acceptable QCP is required prior to Government inspection and acceptance of supplies or services. The QCP shall be reviewed and updated when deemed necessary by the Contractor or the Government, to include changes necessary to prevent the recurrence of quality problems. The Contractor must sign and date the original QCP, as well as each subsequent revision. Revisions shall also be presented to the QAR for review and acceptance prior to implementation. When acceptable to the Government, the original QCP, and any revisions, shall be signed and dated by the QAR.
(2) The Contractor shall require subcontractors to provide and maintain inspection systems adhere to all the requirements in this contract provision.
(3) The QCP shall include the identification of key operational positions, a schematic diagram of plant facilities pertinent to the inspection system, indicating all inspection points, and a description of the following operations related to the supplies or services to be furnished under the contract:
(i) RECEIVING, BLENDING AND COMPOUNDING. Procedures used to ensure the quality of additives blended into product supplied under this contract. Procedures to identify and ensure the quality of component base stocks used to produce finished product. Procedures to be used for adding, prior to batching, all required additives at all locations. When procedures for in-line blending of non-aviation products in accordance with the IN-LINE BLENDING OF NON-AVIATION PETROLEUM PRODUCTS contract provision are used, the QCP will provide for establishing blend ratios, and identify the responsible personnel within the Contractor's organization authorized to establish the blend ratios. When line injection of additives is required by the contract, the QCP will provide procedures for proportionately injecting additives throughout the entire loading process to ensure the additive is homogeneously blended into the product, as well as procedures for maintaining records evidencing the homogeneous blending of all line injected additives. In addition to the testing in (iii) below, a laboratory hand blend of jet fuel with all additives required by the contract shall be tested, prior to shipment, to verify compliance with the specification;
(ii) SAMPLING. Procedures for sampling additives, blend tanks, shipping tanks, lines, and conveyances/containers in accordance with API Manual of Petroleum Measurement Standards (MPMS), Chapter 8, Section 1, (ASTM D 4057) Manual Sampling of Petroleum and Petroleum Products, and/or Section 2, (ASTM D 4177) Automatic Sampling of Liquid Petroleum and Petroleum Products. Procedures include sample location, frequency, quantity, and retention. For all tanker, barge, and pipeline shipments, a flow-proportional sample taken in accordance with MPMS Chapter 8, Section 2, is preferred at the custody transfer point. However, manual samples taken in accordance with MPMS Chapter 8, Section 1 are acceptable provided that they are taken hourly throughout the shipment and that the quantity of the composite sample meets the requirements in Table II of this contract provision. See Table I, Minimum Sampling and Testing Requirements, and Table II, Sample Retention;
(iii) TESTING. Types of test series and individual test methods/procedures to be performed on samples taken from each location identified in (ii) above. See Table I, Minimum Sampling and Testing Requirements, and Table III, Definitions of Test Series;
(iv) CALIBRATION. Program for testing and measuring equipment in accordance with ISO 10012, Measurement Management Systems – Requirements for Measurement Processes and Measuring Equipment, or equivalent local regulation, as appropriate; and, a program for meters used to determine quantity complying with the API MPMS, Chapters 4, 5, and 6, or equivalent foreign standard. For items not covered by API, ASTM, or IP publications, the applicable manufacturer's recommended calibration method(s), outlined in the applicable industry publication, shall be used if acceptable to the Government;
(v) STORAGE AND HANDLING. Procedures for quality/quantity determination. Includes a description of storage and handling equipment, such as tanks, lines, valves, and manifolds; identification of dedicated/common product systems, including description of line segregation and controls to assure capability for proper gauging, sampling, draining of water, filtration, circulation, and drying; and identification of any other process/system used in maintaining product integrity during storage and handling;
(vi) LOADING AND SHIPPING – GENERAL. Procedures for product movement and related quality/quantity checks from shipping tank(s) to custody transfer point (CTP). Description of transfer system from shipping tank to CTP. A dedicated system, including lines, pumps, loading arms, and hoses, is preferred, but an isolated common system incorporating blind flanges, spectacle plates, or double valves between systems is acceptable. An isolated common system using single valves designed to ensure positive isolation, such as twin seal single valves, are also acceptable. Systems with single valve (other than twin seal) isolation require specific procedures be included in the QCP to ensure product integrity prior to the CTP. When single valves (other than twin seal) are present in the system, the Contractor shall provide their quality control procedures, from the first single valve to the CTP, at time of bid to the Contracting Officer for a determination of acceptability. Procedures for conditioning and testing of isolated systems that last carried a product other than that intended for movement under this contract. For in-line blending of non-aviation products, where approved in this contract, requirements must comply with the IN-LINE BLENDING OF NONAVIATION PETROLEUM PRODUCTS contract provision;
(vii) LOADING AND SHIPPING – TANK CARS, TANK TRUCKS, AND INTERMODAL CONTAINERS.
For direct deliveries using Contractor-supplied tank cars and tank trucks in dedicated same grade aviation fuel service, refer to the section of API 1595 entitled “Loading of Road/Rail Cars” for loading and shipping procedures.
All other tank car, tank truck, and intermodal container loadings shall be in accordance with the following procedures: Confirm all compartments have been prepared in accordance with Table IV, Conversion Chart for Tank Cars, Tank Trucks, and Intermodal Containers, below. Whenever possible, ensure the same preparation procedures used for compartments are applied to hoses, manifolds, etc. Ensure that conveyances carrying lubricating oil are dry and free from loose rust, scale, and dirt. Provide for investigation of discrepancies in either recorded quality or quantity. When required by the contract, seal conveyance and record seal numbers on the shipping document.
Strainers and filters shall be located as near the loading or filling point as practicable and shall be used as outlined below for all deliveries except deliveries into tanker, barge, or pipeline.
(A) All aviation fuel shall be passed through strainers of 60 mesh or finer screen;
(B) All lubricating oil products, including preservatives, having a kinematic viscosity of 20.0 centistokes or less at 100 degrees Fahrenheit shall be passed through a 100 mesh or finer screen;
(C) All lubricating oil products, including preservatives, having a kinematic viscosity greater than 20.0 centistokes at 100 degrees Fahrenheit, but less than 22.0 centistokes at 210 degrees Fahrenheit, shall be passed through a 60 mesh or finer screen; and
(D) The Contractor shall furnish and periodically inspect strainers and filters pursuant to this paragraph to determine condition and perform maintenance as necessary, keeping a written record thereof.
(viii) LOADING AND SHIPPING – TANKERS AND BARGES.
(A) For f.o.b. destination Contractor-supplied tankers/barges. Procedures for the preparation of vessel cargo systems, in accordance with Energy Institute (EI) HM 50, Guidelines for the Cleaning of Tanks and Lines for Marine Tank Vessels Carrying Petroleum and Refined Products, that ensure the vessel is suitable to load the intended product(s).Particular attention should be given to vessels that previously carried a Fatty Acid Methyl Ester (FAME) cargo. As a minimum, f.o.b. destination Contractors must ensure that all cargo systems on the vessel intended for loading product under this contract, to include tanks, lines, manifolds, and pumps, are washed, gas freed, and inspected. In the event a solvent de-greaser is utilized in the tank preparation process, a minimum of two rinses must be performed by the vessel prior to loading Aviation Turbine Fuel. Vessels that will be carrying JP8 will be allowed to load without cleaning based upon the following criteria: the last cargo prior to loading JP-8 is Jet A/A1, and the second and third to last cargoes were clean middle distillate or lighter petroleum products (no black oils, lubricating oils, vegetable oils, palm oils, biodiesel with FAME content greater than or equal to 15 % or other similar products). The vessel will drop all lines and strip dry all cargo tanks of the previously carried Jet A/Jet A1 prior to loading JP-8. These procedures, and others deemed necessary by the Contractor, shall be included to ensure that the product meets the specification requirements at the CTP.
(B) For f.o.b. origin Government-supplied tankers/barges. Procedures for maintaining a time log of all significant events/delays including vessel notice of readiness, vessel arrival, mooring, vessel deballasting, inerting and conditioning of cargo tanks, inspections, hose connections and disconnections, starts, stops, vessel release, or any other event that affects laytime of the vessel. Procedures for assuring condition of loading line (full of tested product, all air bled, and pressure packed) and gauging shore tanks, both before and after loading. In the event an automated metering system is to be used as the means of shore quantity determination, manual gauges of all storage tanks designated for shipment shall be taken prior to commencement of loading. Procedures for preload discussion between Contractor, vessel, and QAR to include, but not be limited to, prior two cargoes, cleaning procedures, loading plan, loading rates, sampling requirements, and after loading sampling and gauging. [Prior to loading -gauge, sample, and test intransit cargoes designated for load on top. Gauge and sample (1 gallon) any other product on board, except for JPTS, and retain those samples.] All cargo quantities shall be calculated and volume corrected both before and after loading. Procedures for commencement of loading into one tank (up to 3 feet), then switching to at most two other vessel tanks while first-in sampling and testing is being accomplished (Table I). Procedures for the transportation of samples from the vessel to the testing facility. Monitoring the loading (including line blending and additive injection) from source to vessel, investigating irregularities immediately and stopping loading, if necessary. Procedures for investigating discrepancies in quality (mandated if off-specification or out of testing tolerance) and quantity (mandated if shore to ship variance is in excess of the following: 0.2% (0.002) for cargos not requiring cleaning, gas freeing, or drop/strip; 0.3% (0.003) for cargos requiring drop/strip; or 0.5% (0.005) for cargos requiring cleaning and gas freeing, or figures are suspect) on loaded conveyance.
(C) For both f.o.b. origin and destination tankers/barges. Procedures for immediately notifying the QAR when irregularities occur or are suspected, and on all occasions when loading is interrupted. Authority to release a Government-furnished vessel rests with the Government QAR after compliance and completion by the Contractor of all required operations, including the preparation of the DD Form 250-1.
(ix) RECORDS AND REPORTS. Procedures for completing and distributing required documentation both prior to and after the release of the vessel. Documentation shall include, as a minimum, test reports for all products and additives, additive blending and/or injection records, vessel notice of readiness, customs documents, bills of lading, vessel ullage reports, and the DD Form 250/DD Form 250-1 and continuation sheet(s) (or the Paperless Ordering and Receipt Transaction System [PORTS] or equivalent). Other documentation may be required on an as needed basis, such as vessel port logs, calibration records, and results of quality or quantity discrepancy investigations. These records and reports will include by whom, where, and how they were prepared, as well as retention information. The DD Form 250-1 and DD Form 250-1 continuation sheet(s) will be signed by the Contractor and the vessel representative in the appropriate blocks before presenting them to the QAR for signature. The DD Form 250 and DD Form 250-1 shall identify the type, brand name, and amount of all additive(s).
(x) CORRECTIVE ACTION. Actions to be followed to effect correction of any deficiency affecting product quality or quantity, such as handling of off-specification product (waivers, conveyance rejections, etc.). The corrective action procedures shall include notification of the QAR.
(4) The QCP shall identify one individual to serve as a point of contact for quality/quantity matters relating to the inspection system description in the plan.
(5) The Contractor is responsible for all inspection systems, QCPs, and product quality and quantity.
(c) The Contractor shall perform all inspections and acceptance tests required by the specifications of the supplies to be furnished under this contract or, shall have such tests performed, in a laboratory acceptable to the Government.
For f.o.b. destination Contractor-supplied tankers/barges, the Contractor shall provide the QAR, prior to the first shipment, with the name and location of the laboratory to be used for testing at each discharge point. The Contractor shall also notify the QAR of any subsequent laboratory changes prior to the affected shipments. If any laboratory is determined to be unacceptable to the Government, the Contractor must designate another laboratory that is acceptable, before acceptance testing can take place. Acceptance tests will normally be performed at the acceptance point. However, when such tests are performed at origin on supplies to be accepted at destination, documentation that will enable verification of the original test results shall be provided to the Government prior to acceptance at destination. Regardless of the method of delivery, products furnished under this contract must meet all specification requirements at the CTP.
(d) Prior to loading, the Contractor shall inspect all shipping conveyances for suitability to load the supplies furnished under this contract, except for Government-furnished tankers and barges Authorization for the Contractor to participate in the inspection of Government-supplied tankers and barges rests with QAR. The QAR has the right to inspect any Government-supplied conveyance prior to loading and, in the event the Contractor and the QAR disagree on the suitability to load such a conveyance, the determination of the QAR shall govern. If the SHIPMENT AND ROUTING contract provision is included in the contract, Government-furnished transportation equipment that is unsatisfactory for loading shall be reported by the Contractor in accordance with the provisions contained in that contract provision. Procedures to determine suitability to load tank trucks and tank cars shall include, but not be limited to, visual inspection of interior compartments to assure cleanliness and dryness. Manifolds and hoses must be drained and be clean and dry for the intended product. If the Contractor intends to witness operations at any point up to, and including, government acceptance, the Contractor is responsible for contacting the facilities to be visited and obtaining the required access.
(e) When requested by the U.S. Government, the Contractor shall furnish no more than five (ten in the case of jet fuel) 1-gallon samples of liquid product from any individual batch or lot of the supplies to be furnished under this contract. Such samples shall be furnished without charge to the Government and shall be packed, marked, and shipped by the Contractor, at their expense.
(f) The Contractor shall keep all quality and quantity records related to the performance of this contract complete and available to the Government during the performance of this contract and for three years after final payment under this contract. These records shall include, but not be limited to, DD Form 250-series documents, documentation of internal inspections of all conveyances, laboratory certificates for all required testing (including those for the shipping tanks for f.o.b. destination tankers/barges), and documentation of quantity determinations.
(g) When a common system is to be used for shipment in accordance with paragraph (a)(3)(vi) above, the Contractor shall provide a list of all products carried by that system during the past year to the Contracting Officer, at the time of offer, for a determination of acceptability.
(h) The inspection system and related operations provided or performed pursuant to this provision shall be subject to surveillance by the QAR.
(i) The contractor may provide transportation to/from/between contractor facilities and operations to the QAR or DLA Energy representative performing official duties relating to the administration of the contract and the contract price shall include the cost of any such transportation.
TABLE I
MINIMUM SAMPLING AND TESTING REQUIREMENTS (1) (9)
LOCATION
WHEN SAMPLED TYPE OF SAMPLE TYPE OF TEST
(SERIES OR
INDIVIDUAL)
1. Refinery/Terminal (Each Shipping Tank)
Each Batch Prior to Start of Shipment
All Level or Multi-Level Composite
A (2)
2. All Modes (Shipping Line)
a. Dedicated Line
b. Common Line
Prior to Loading/Shipping
Spot
C
B
3. All Modes (except Tank Car/Tank Truck)/Intermodal Container) (Custody Transfer Point)
Immediately After Start of Loading/Shipping
Spot C
4. a. Tanker/Barge or Pipeline (F.O.B.
Origin) (Custody Transfer Point)
b. Tanker/Barge (F.O.B Destination) (Custody Transfer Point)
During Loading or Pipeline Shipping
During Discharge
Representative Line Sample [See Paragraph (b)(3) (ii)]
Representative Line Sample [See Paragraph (b)(3) (ii)]
Retain Only
Retain Only – Discard After Shore Tests are On- Specification
5. Tanker/Barge/Pipeline (Custody Transfer Point)
Hourly During Loading/Shipping
Spot Visual (3) plus additive analysis for FSII & SDA, if line injected
6. Tanker/Barge (First-In)
After loading 3 feet or the line displacement quantity, whichever is greater
Spot C (4) - plus additive analysis for FSII & SDA, if line injected
7. Tanker/Barge (F.O.B. Origin only)
a. Each Compartment
b. Composite
After Loading
All-Level or Multi-Level Composite
Multi-Tank Volumetric Composite (6) of Each Product Loaded
Sample to be retained in case composite fails. If composite fails perform Workmanship & Density on each compartment sample. For JP5, flash point must also be performed.
B (except gum for Aviation Turbine Fuel) (except carbon residue for Diesel/Kerosene) (plus FAME (7))
8. Tanker/Barge (F.O.B. Destination only)
a. Origin (vessel) Composite
b. Destination (vessel) Composite
c. Destination (vessel) Each Compartment
(SEE NOTE 5 FOR ADDITIONAL
REQUIREMENTS)
After loading
Prior to Discharge
Prior to discharge
Multi-Tank Volumetric Composite (6) of Each Product Loaded
Multi-Tank Volumetric Composite (6) of Each Product to be Discharged
All-level or Multi-level composite
A (plus FAME (7))
A
For retain in case composite fails. If composite fails perform Workmanship & Density on each compartment sample. For JP5 perform flash point also.
9. Tank Car/Tank Truck/Intermodal Container (Loading Rack)
After change of source tank.
Spot C plus additive analysis for FSII & SDA, if line injected
10. Tank Cars/Tank Truck/ Intermodal Container
After Loading/Filling All-Level or Low Point Drain/Bottom Line (10)
Workmanship (C - when loading lubes and FSII)
11. Drum After Filling Multi-drum Composite (8) C
NOTES FOR TABLE I:
(1) AT THE GOVERNMENT'S OPTION, FULL SPECIFICATION TESTING MAY BE REQUIRED AT THE
CUSTODY
TRANSFER POINT. IT IS THE CONTRACTOR'S RESPONSIBILITY TO FURNISH THE GOVERNMENT
WITH
SATISFACTORY EVIDENCE OF SPECIFICATION COMPLIANCE.
(2) PRIOR TO PERFORMING A-LEVEL TESTING, THE HOMOGENEITY OF EACH BATCH SHALL BE
DETERMINED.
AT A MINIMUM, UPPER, MIDDLE, AND LOWER SAMPLES SHALL BE TESTED FOR DENSITY/API
GRAVITY AND COMPARED TO THE SPECIFICATION REQUIREMENT FOR HOMOGENEITY. IF NO
SPECIFICATION REQUIREMENT EXISTS, HOMOGENEITY SHALL BE DEFINED AS WHEN THE TEST
RESULTS FOR THE UPPER, MIDDLE, AND LOWER SAMPLES ALL FALL WITHIN THE REPEATABILITY
LIMIT(S) OF THE TEST METHOD USED TO DETERMINE DENSITY/API GRAVITY. IN ANY CASE,
WHEN DEEMED NECESSARY BY THE GOVERNMENT, TESTS IN ADDITION TO DENSITY/API
GRAVITYMAY BE REQUIRED TO CONFIRM BATCH HOMOGENEITY.
(3) CONTINUOUS IN-LINE ANALYZERS (I.E., DENSITY AND/OR FLASH POINT) ARE ACCEPTABLE, IN
LIEU OF
HOURLY EVALUATIONS, IF QUALITY IS ASSURED. WHEN CONTINUOUS IN-LINE ANALYZERS ARE
PRESENT
IN THE SYSTEM, THE CONTRACTOR SHALL PROVIDE ITS QUALITY CONTROL PROCEDURES AT
TIME OF
OFFER TO THE CONTRACTING OFFICER FOR DETERMINATION OF ACCEPTABILITY.
(4) TESTING FOR PARTICULATE CONTAMINATION SHALL BE REQUIRED BY THE GOVERNMENT IF
VISUAL
EXAMINATION OF THE SAMPLE FAILS WORKMANSHIP FOR SEDIMENT/SUSPENDED MATTER.
(5) FOR FOB DESTINATION SHIPMENTS DESTINED FOR MULTIPLE LOCATIONS IN CLOSE
PROXIMITY TO ONE
ANOTHER (WITHIN 24 HOURS SAILING TIME BETWEEN LOCATIONS) THE A-TYPE TESTING
REQUIRED PRIOR TO DISCHARGE SHALL ONLY BE REQUIRED AT THE INITIAL DISCHARGE POINT, WITH ONLY C-TYPE TESTING REQUIRED PRIOR TO DISCHARGE AT SUBSEQUENT DISCHARGE
POINTS. HOWEVER, IF CARGO INTEGIRTY CHANGES BETWEEN DISCHARGE POINTS, SUCH AS
THROUGH CARGO TRANSFERS, CONTAMINATION, ETC., THEN A-TYPE TESTING SHALL BE
REQUIRED AT THE NEXT DISCHARGE POINT. A COPY OF THE FULL SPECIFICATION TEST REPORT FOR THE VESSEL, AFTER LOADING, SHALL BE PROVIDED TO THE RECEIVING ACTIVITY AT EACH
DISCHARGE POINT, PRIOR TO DISCHARGE.
(6) COMPRISED OF ALL-LEVEL OR MULTI-LEVEL COMPOSITES FROM EACH COMPARTMENT.
(7) CONTRACTORS DELIVERING INTO THE GPSS,CEPS, NIPS, AND DFSP ATHENS (MOH) SHALL
PERFORM FAME
CONTENT TESTING IN ACCORDANCE WITH TEST METHOD IP 585 OR IP 590, AND REPORT THE
RESULTS TO THE DESTINATION CONSIGNEE PRIOR TO VESSEL ARRIVAL.
(8) A ONE LITER COMPOSITE SAMPLE OF EACH LOT OF PRODUCT SHALL BE TAKEN FROM A
PREDETERMINED
NUMBER OF RANDOMLY SELECTED DRUMS. THE TOTAL NUMBER OF DRUMS SAMPLED PER LOT
SHALL, AT A MINIMUM, BE THAT CITED IN TABLE III OF API MPMS CHAPTER 8.1 (ASTM D 4057), BUT MAY BE INCREASED AT THE GOVERNMENT’S OPTION.
(9) THE SIZE OF ALL THE SAMPLES REQUIRED IN THIS TABLE, EXCEPT FOR THOSE DESIGNATED
“RETAIN ONLY”,
SHALL BE DETERMINED BY THE CONTRACTOR AND SHALL BE OF SUFFICIENT QUANTITY TO
PERFORM ALL THE TESTS REQUIRED BY THIS TABLE. THE SIZE REQUIREMENTS FOR RETAIN
SAMPLES CAN BE FOUND IN TABLE II, SAMPLE RETENTION.
(10) THE LOW POINT DRAIN/ BOTTOM LINE OPTION ONLY APPLIES TO TANK CAR AND TANK
TRUCK SHIPMENTS
OF FUEL – SHIPMENTS OF LUBRICATING OILS AND ADDITIVES MUST UTILIZE ALL-LEVEL
SAMPLING PROCEDURES. IF INITIAL FUEL SAMPLES USING THE LOW POINT DRAIN/BOTTOM LINE
OPTION ARE NOT CLEAR AND BRIGHT, ADDITIONAL SAMPLES SHALL BE TAKEN UNTIL A CLEAR
AND BRIGHT SAMPLE IS OBTAINED.
TABLE II
SAMPLE RETENTION (1)
LOCATION
MINIMUM QUANTITY RETENTION PERIOD(1)
1. Bulk Tank Cars/Tank Trucks/Intermodal Containers
Additives
Fuels and Lubricating Oils
2 Liters (2)
1 Liter (2)
Until Receipt and Quality Verification of Each Lot/Batch
15 Days – 45 Days for Lubricating Oils
2. Drums
Avgas
1 Liter – multi-drum composite (3)
45 Days
3. Shipping Tank(s) 20 Liters - for Aviation Turbine Fuels
10 Liters - for all other Fuels, Lubricating Oils, and Additives
45 Days
4. Tanker/Barge/Pipeline (Composite Line at Custody Transfer Point)
20 Liters - for Aviation Turbine Fuels
10 Liters - for all other Fuels
45 Days
5. Tanker/Barge (Composite)
F.O.B. Origin
F.O.B. Destination
20 Liters - for Aviation Turbine Fuels
10 Liters - for all other Fuels
20 Liters
45 Days
Until Shore Tests On-Specification
6. Tanker/Barge (Each Compartment)
F.O.B. Origin
F.O.B. Destination
0.5 Liter
1 Liter
45 days
Until Shore Tests On-Specification
NOTES FOR TABLE II:
(1) UNLESS OTHERWISE NOTED, THE RETENTION PERIOD SHALL BE FOR THE STATED NUMBER OF
DAYS AFTER
THE SAMPLE HAS BEEN TAKEN FROM THE LOCATION INDICATED.
(2) IF THE CONVEYANCE IS COMPARTMENTALIZED, A PROPORTIONAL SAMPLE SHALL BE TAKEN
FROM EACH
COMPARTMENT SUCH THAT A TOTAL OF ONE LITER IS COLLECTED FROM THE CONVEYANCE.
(3) A ONE LITER COMPOSITE SAMPLE OF EACH LOT OF PRODUCT SHALL BE TAKEN FROM A
PREDETERMINED NUMBER OF RANDOMLY SELECTED DRUMS IN ACCORDANCE WITH TABLE III OF
API MPMS CHAPTER 8.1 (ASTM D 4057).
TABLE III
DEFINITIONS OF TEST SERIES
I. TYPE A: Includes all specification quality conformance tests plus any additional contractual requirements.
II. TYPE B & C: As shown in the table below for each product. Properties and test methods will be in accordance with the product specification for each grade identified in the solicitation/contract.
AVGAS TURBINE
FUEL
MOGAS DIESEL/
KEROSENE
BURNER
FUEL
LUBE OIL FSII
TEST
PROPERTIES
B C B C B C B C B C B C C
Workmanship * * * * * * * * * * * Particulate content * * * (1) * Filtration Time * Color * * * * * * * * * * Density or API Gravity or Specific Gravity
* * * * * * * * * (2) * (2) *
Distillation * * * * Corrosion, Copper Strip
Existent Gum * * Carbon Residue * * Lean or Rich Ratings * Reid Vapor Pressure * * (3) * Water Reaction * * Lead Content * Freeze Point * Flash Point * * * * * * * * FSII Content * Microseparometer * Conductivity * Sediment & Water * * Viscosity * * * Water Content * * * * Water Tolerance * Foam Test * *
* THE PROCEDURE TO BE USED FOR CONDUCTING THESE TESTS WILL BE AS STATED IN THE
APPROPRIATE
PRODUCT SPECIFICATION AND/OR CONTRACT.
NOTES FOR TABLE III:
(1) F76 ONLY.
(2) GRADES 1, 2, AND 4 (L) ONLY.
(3) JP4 ONLY.
TABLE IV
CONVERSION CHART FOR TANK CARS, TANK TRUCKS, AND INTERMODAL CONTAINERS (1)
PRODUCT TO BE LOADED (6)
LAST
PRODUCT
CARRIED (2)
JP-4
JET B
AVGAS
JP-5, JP-8
TS-1
JET A/A1
JPTS (7)
RP1/RP
JP-10/PF-
F76 FSII LUBRICATI
NG
OILS
JP-4, JET-B
MOGASE85,
AVGAS
DRAIN
EMPTY
STEAM
DRY
STEAM
DRY
STEAM
DRY
STEAM
DRY
STEAM
DRY
STEAM
DRY
STEAM DRY
JP-5, JP-8, TS-1
JET A/A1,
KS1/R/N
DRAIN
EMPTY
DRAIN
EMPTY
(4)
STEAM
DRY
STEAM
DRY
STEAM
DRY
DRAIN
EMPTY (4)
STEAM
DRY
STEAM DRY
JPTS DRAIN
EMPTY
DRAIN
EMPTY
DRAIN
EMPTY
DRAIN
EMPTY
STEAM
DRY
DRAIN
EMPTY
STEAM
DRY
STEAM DRY
RP1/RP2 STEAM
DRY
STEAM
DRY
STEAM
DRY
DRAIN
EMPTY
STEAM
DRY
STEAM
DRY
STEAM
DRY
STEAM DRY
JP-10/PF-1 STEAM
DRY
STEAM
DRY
STEAM
DRY
STEAM
DRY
DRAIN
EMPTY
STEAM
DRY
STEAM
DRY
STEAM DRY
F-76, MGO
LS-1/2/S/W,
DS-1/2/S/W, DF-2
HS-1/2, FS-1/2
FL-2/4
STEAM
DRY
STEAM
DRY
STEAM
DRY
DRAIN
EMPTY (4)
STEAM
DRY
STEAM DRY
FSII DRAIN
EMPTY
DRAIN
EMPTY
STEAM
DRY
STEAM
DRY
STEAM
DRY
DRAIN
EMPTY
DRAIN
EMPTY
STEAM
DRY
LUBRICATING
OILS
NO
LOAD
NO
LOAD
NO
LOAD
NO
LOAD
NO
LOAD
STEAM
DRY
NO
LOAD
DRAIN
EMPTY (3)
BIODIESEL
BLENDS <B15
STEAM
DRY (4)
STEAM
DRY (4)
STEAM
DRY
(4)
STEAM
DRY
(4)
STEAM
DRY (4)
STEAM
DRY (4)
STEAM
DRY (4)
STEAM
DRY (4)
BIODIESEL
BLENDS >B15
S…
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