Attachment 2 ENERGY QAP C16.64-3 (OCT 2018) .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

8725 JOHN J. KINGMAN ROAD

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'