Tab 09 Att - C and E QAPS.pdf

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DLA FORM 1889, JUL 2023

D L A FORM 0 0 1 3, AUGUST 20 22

Prescribed by: eSOP 4155.05-001 Sponsor: J3

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

DLA NOT FOR PRODUCTION

PREVIOUS EDITION IS OBSOLETE

REV

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DATE

APPROVED

REVISIONS

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

DISTRIBUTION STATEMENT - A

APPROVED FOR PUBLIC RELEASE

DISTRIBUTION IS "UNLIMITED"

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DESCRIPTION

DATE

APPROVED

REVISIONS

DISTRIBUTION STATEMENT - A

APPROVED FOR PUBLIC RELEASE

DISTRIBUTION IS "UNLIMITED"

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

9.0.0.2.20100902.2.720808

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Randy Davis

DLA DT

DLA DT

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rev: 2 description: ENERGY QAP C16.64-1 revdate: 2025-11-17 revapproved:

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DLA FORM 1889, JUL 2023

D L A FORM 0 0 1 3, AUGUST 20 22

Prescribed by: eSOP 4155.05-001 Sponsor: J3

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

DLA NOT FOR PRODUCTION

PREVIOUS EDITION IS OBSOLETE

REV

DESCRIPTION

DATE

APPROVED

REVISIONS

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

DISTRIBUTION STATEMENT - A

APPROVED FOR PUBLIC RELEASE

DISTRIBUTION IS "UNLIMITED"

REV

DESCRIPTION

DATE

APPROVED

REVISIONS

DISTRIBUTION STATEMENT - A

APPROVED FOR PUBLIC RELEASE

DISTRIBUTION IS "UNLIMITED"

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

9.0.0.2.20100902.2.720808

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Randy Davis

DLA DT

DLA DT

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description: ENERGY QAP C1.02 revdate: 2025-03-11 revapproved:

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BANISZEWSKI.DANIE

L.J.1287388698

Digitally signed by

BANISZEWSKI.DANIEL.J.1287388698

Date: 2025.01.23 14:08:16 -07'00'

CATLIN.JOSHUA.D.127

6289540

CATLIN.JOSHUA.D.1276289540

Date: 2025.01.23 09:31:39 -05'00'

MACLANE.SKYLLAR.

BRYANNA.1252141827

MACLANE.SKYLLAR.BRYANNA.1252141827

Date: 2025.01.16 14:18:25 -05'00'

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

C16.09 TURBINE FUEL, AVIATION (JET Al) (DLA ENERGY JAN 2025)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE PRODUCT CODE

9130-00-753-5026 Turbine Fuel, Aviation, Jet A1 JAl

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) PRODUCT REQUIREMENTS. Product shall conform to the latest version of ASTM Dl655: Standard Specification for Aviation Turbine Fuels with the following modifications. For European, Middle Eastern, and Asian Locations Only: product shall conform to the latest revision of Defence Standard 91-091.

(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 A1 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)

(A) MSEP shall be performed on unadditized Jet A that has a custody transfer point on the distribution system using, D7224 or D8073. If either method is not available testing may be conducted with D3948. Passing results (min 85) for D3948 will be considered acceptable. Test failures using D3948 shall be retested using D7224 or D8073. If fuel passes D7224 with a minimum limit of 85 or D8073 with a limit of 88, the fuel is acceptable with no further action.

(c) ADDITIVES: Additives shall not be premixed with other additives before injection into the fuel.

(1) FUEL SYSTEM ICING INHIBITOR (FSII). When FSII is required by contract line item

(i) The fuel shall contain 0.07 to 0.10 percent by volume FSII.

(ii) FSII shall be added to the fuel and shall be Diethylene Glycol Monomethyl Ether (DIEGME) conforming to the latest version of ASTM D4171, Standard Specification for FSIIs, Type III or MIL-DTL-85470C, dated March 5, 2024, Inhibitor, Icing, Fuel System, High Flash, NATO Code Number S-1745.

(iii) When using the 20-ounce aerosol can to introduce FSII during over the wing refueling, determine the fuel quantity and calculate the amount of required additive. This additive shall be added gradually during filling to permit proper blending in the fuel. One can of aerosol additive will inhibit 180 gallons of fuel to 0.087 percent by volume. The use of aerosol FSII is not permitted for U.S. Navy aircraft refueling.

(2) CORROSION INHIBITOR/LUBRICITY IMPROVER (CI/LI). When CI/LI is required by contract line item the additive shall conform to the latest revision of MIL-PRF-25017H with amendment 1 dated August 4,2011, revalidated May 25, 2021, and be listed in Qualified Products List (QPL)-25017. In order to obtain dosage data for QPL-25017 additives, access the Qualified Products Database (QPD)at https://qpldocs.dla.mil/. Do a search for QPL number 25017, and click the MIL-PRF-25017 Category 1 link. The dosage information is located in the "source notes" for each qualified additive as minimum effective and maximum allowable concentrations in grams per cubic meter (g/m3).

https://qpldocs.dla.mil/

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

(3) STATIC DISSIPATER ADDITIVE (SDA). When required by contract line item, SDA shall be added to the fuel and the conductivity limits of 50-600 picosiemens per meter (pS/m) at ambient temperature or 29.4˚C (85˚F), whichever is lower, unless otherwise directed by the procuring activity.

(4) METAL DEACTIVATOR ADDITIVE (MDA). MDA shall not be used unless the supplier has obtained written consent from the procuring activity and user.

(i) Product shall be homogeneously mixed. Until all aviation turbine fuel tanks are coated, it is acceptable to perform stratification test in lieu of circulating tanks to homogeneity.

(d) SYNTHETIC BLEND COMPONENT (SBC) and CO-HYDROPROCESSED SYNTHESIZED KEROSENE

(1) If a fuel containing an SBC or a co-hydroprocessed synthesized kerosene is being offered, notification shall be made to the contracting point of contact with submission of relevant details regarding the blend percentage and which Annex of ASTM D7566 for the synthetic blend component used, and which feedstocks and co-processing percentage for co-hydroprocessed synthesized kerosene. Only synthetic blend components approved in ASTM D7566, MIL-DTL-83133, and MIL-DTL-5624 and co-hydroprocessed synthesized kerosene produced from approved feedstock and percentage in ASTM D1655, MIL-DTL-83133, and MIL-DTL-5624 shall be acceptable to the government

ENERGY QAP C16.09 Turbine Fuel Aviation (Jet A1) (JAN 2025) .pdf

C16.09 TURBINE FUEL, AVIATION (JET Al) (DLA ENERGY JAN 2025)

(b) SPECIFICATION MODIFICATIONS.

KNAPP.RICHARD.BRU

CE.1027134021

KNAPP.RICHARD.BRUCE.1027134021

Date: 2024.04.11 12:46:02 -04'00'

MACLEAN.SARAH.A.1

400398441

MACLEAN.SARAH.A.1400398441

Date: 2024.04.11 12:22:48 -04'00'

KARRAS.JASON.EARL

E.1129188177

KARRAS.JASON.EARLE.1129188177

Date: 2024.04.11 12:28:51 -04'00'

TABLE I, Sample Retention1

LOCATION MINIMUM QUANTITY RETENTION PERIOD 1

Bulk Tank Cars/Tank Truck/Intermodal Container

Fuels 1 gallon (4 liters) 2 15 days for fuels Lubricating Oils 0.25 gallons (1 liter) 2 45 days for lubricating oils

Drums4 2 gallons (8 liter) (multi-drum composite) 3 45 days

Shipping Tank(s)

2 gallons (8 liters) for Aviation Turbine Fuels 1 gallon (4 liters) for all other Fuels, Lubricating Oils, and Additives

45 days

Tanker/Barge/Pipeline (Composite Line at Custody Transfer Point)

5 gallon (20 liters) for all fuel types 45 days

Tanker/Barge (Composite)

F.O.B. Origin 2 gallons (8 liters) for Aviation Turbine Fuels 1 gallon (4 liters) for all other fuels

45 days

F.O.B. Destination 2 gallons (8 liters) Until shore tests on-specification Tanker/Barge (Each Compartment)

F.O.B. Origin 0.25 gallon (1 liter) 45 days F.O.B. Destination 0.25 gallon (1 liter) Until shore test on-specification

NOTES:

1. Unless otherwise noted in this document or applicable contract, 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.

3. An 8-liter composite sample of each product lot shall be taken from a predetermined number of randomly selected drums IAW Table III of API MPSM, Chapter 8.1 (ASTM D 4057).

4. Applies to DLA Energy managed procurements of products shipped in drums. Does not apply to DLA Aviation managed procurements for packaged products.

TABLE II, Minimum Sampling and Testing Requirements for Petroleum Products Series 1, tankers and barges1

ITEM WHEN TO SAMPLE LOCATION OF SAMPLE TYPE OF SAMPLE2 TEST REQUIRED3

1.a

Prior to Loading

Before acceptance of new materiel and after establishment of new batch4 Each shore storage tank Single Tank Composite or All

Levels A5, 15

1.b After line pack but prior to loading As close to the custody transfer point as possible Line Sample C7,14 Dedicated System B-1 Non-Dedicated System

1.c D uring

Loading

Immediately after start of loading/shipment point as possible Line Sample C7

1.d After first in Vessel cargo compartment(s) Spot C7,14

1.e During loading point as possible Line Sample Hourly Visual6,8, Retain10

1.f

A fter Loading

After loading

Each vessel cargo compartment All Level (Combine All Levels into one Volumetric Composite Sample13)

C 6, 8, 11,14

Remainder of B-112

(Retain fuel for B-1 referee testing)

1. Additional requirements to include retain samples may be required. See Quality Assurance Provisions (C or E-QAP) for further details.

2. Refer to ASTM International D4057 for sampling procedures.

3. Test results shall be compared against the quality release certificate. Any discrepancies shall be identified, investigated, and resolved.

4. Upon procurement at refineries, blending installations, etc. and at main installations including national depots & ocean importing points on establishment of new batches.

5. Prior to performing A-level testing, the homogeneity of each batch shall be determined. Refer to paragraph (b)(1)(iii)(C) of this document for additional details.

6. Test for FSII and SDA only if line injected.

7. If sample fails appearance, perform particulate matter using approved methods as outlined in the applicable specification.

8. Lubricity also required for F-76 only if line injected, or determine LIA concentration by volumetric measurement/calculation.

9. First in shall be done after one (1) meter or after line displacement whichever is the greater.

10. For all tanker and barge, 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 if they are taken hourly throughout the shipment and that the quantity of the composite sample meets the requirements in Table I

11. Best practice is for B-1 test completion for FOB Origin Procurements (or Type A level testing when specified in contract for FOB Destination Procurements) prior to vessel release. Based on QAR decision, vessel may sail after C Tests to meet schedule requirements including to avoid predicted weather; remainder of B-1 tests to be completed before arrival at next load or discharge port. Test report will be provided to designated discharge port.

12. Type A level testing required for FOB Destination Procurements (unless otherwise specified by contract).

13. As defined by API MPMS Chapter 8-1, section 3.22.

14. For product verification purposes. Results of C-test must fall within reproducibility of source tank A-level results.

15. New cargo from same batch, within 30 days, will only require B-1 testing to verify previous A-level test results. B-1 level verification test results should fall withing reproducibility of source tank A-level results.

Series 2, pipeline, tank trucks, tank cars, iso-containers1,7

ITEM WHEN TO SAMPLE LOCATION OF SAMPLE TYPE OF SAMPLE 2 TEST REQUIRED3

2.a Prior to Shipm ent

Before acceptance of new materiel and after establishment of new batch4

Each Shipment Storage Tank Single Tank Composite or All Levels A9, 11

2.b After line pack but prior to loading/shipment

As close to the custody transfer point as possible Line Sample C5,6 Dedicated System

B-1 Non-Dedicated System

2.c D uring Shipm ent

Immediately after start of loading/shipment possible and downstream of the filter separator (if equipped)

Line Sample C5, 13

2.d Pipeline Only:

Hourly after start of loading or shipment10 possible and downstream of the filter separator (if equipped) Line Sample

Apperance5, 12

(Retain fuel for B-1 referee testing)

2.e

Daily on first fill and anytime a new tank is placed on issue (after line displacement) TT, TC, ISO, Refuelers or other over the road transportation modes only possible (Loading Rack or Fill Point) and downstream of the filter separator (if equipped)

Line Sample Color (by visual method) and Appearance5.

If visual fails perform C6

2.f fter Loading

Daily for each conveyance mode (Not required for pipeline operations)

Each Cargo Compartment or another point that provides a representative sample All Level

Appearance on each compartment

C on composite 5,6,8

2.g Drums Sample of each lot of product shall be taken from a predetermined number of randomly selected drums14

Multi-drum Composite C13

1. Additional contractual requirements to include retain samples may be required. See Contract Quality Assurance Plans (C or E-QAPs) for further details.

2. Refer to ASTM International D4057 for sampling procedures.

3. Test results shall be compared against the quality release certificate. Any discrepancies shall be identified, investigated, and resolved.

4. Upon procurement at refineries, blending installations, etc., and at main installations including national depots & ocean importing points on establishment of new batches.

5. Test for FSII and SDA only if line injected.

6. If sample fails appearance, perform particulate matter using approved methods as outlined in the applicable specification.

7. Type A level testing required for FOB Destination Procurements (unless otherwise specified by contract).

8. 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.

9. Filtration time testing is required for JP-5 & JP-8 and shall meet contract requirement.

10. For 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 if they are taken hourly throughout the shipment and that the quantity of the composite sample meets the requirements in Table I.

11. Prior to performing A-level testing, the homogeneity of each batch shall be determined. Refer to paragraph (b)(1)(iii)(C) of this document for additional details.

12. Lubricity also required for F-76 only if line injected or determine LIA concentration by volumetric measurement/calculation.

13. For product verification purposes. Results of C-test must fall within reproducibility of source tank results.

14. A composite sample of 2 gallons (8 liters) for Aviation Turbine Fuels and 1 gallon (4 liters) for all other fuels for 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.

Series 3, product receipt and discharges for tankers and barges (FOB Destination)

ITEM WHEN TO SAMPLE LOCATION OF SAMPLE TYPE OF SAMPLE TEST REQUIRED

3.a

Prior to D ischarge

Prior to discharge

From each vessel cargo compartment All Level Appearance and Density1

3.b From each vessel cargo compartment

All Level (Combine All Levels into one Volumetric Composite

Sample)

3.d

D

Within 30 minutes after start and each hour after until completion

Dock/Discharge Manifold Header Line Sample / Retain Perform Appearance test2,3 and then retain fuel for Referee testing

3.e fter

If remainder of fuel will be shipped to another DFSP

Each vessel compartment with fuel remaining on board All Level Retain until discharged at destination

1. Test for flash point on high flash cargo tanks if low and high flash cargoes are carried together aboard the same vessel without segregated venting systems.

2. For aviation fuel delivery, FSII and SDA shall be tested only if line injected. This requires an additional quart sample.

3. Test for additives if line injected downstream of the injector. (If line injecting LIA into F-76, test for lubricity.)

Series 4, product receipt from pipeline (FOB Destination)1

ITEM WHEN TO SAMPLE LOCATION OF SAMPLE TYPE OF SAMPLE TEST REQUIRED

4.c D

R eceipt

During pipeline receipt Custody transfer point Line Sample/Retain 5 Gallon Minimum2

4.d During pipeline receipt, immediately after start, Midpoint and 1 hour prior to completion3 possible Line C

4.g fter

R eceipt

After receipt of fuel Each receipt tank All level A

1. Refer to ASTM International D4057 for sampling procedures.

2. Retain for referee testing in the event a failure occurs on receipt tank. Retain sample for 45 days. Sampling is IAW API MPMS Chapter 8

3. Fuel from a new batch will be considered a new receipt for quality control purposes.

TABLE III, Definitions of Test Series

I. TYPE A: Includes all specification quality conformance tests plus any additional contractual requirements.

II. TYPE B-1 & 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

AVIATION

TURBINE

MOGAS

DIESEL/

KEROSENE/

NAVAL DISTILLATE

LUBE OIL

TEST PROPERTIES B-1 C B-1 C B-1 C B-1 C B-1 C

Appearance/ workmanship

Particulate content * *8 *1 *8 Filtration Time * Color (visual) * * * * * * * * * Density/API Gravity/ Specific Gravity

Distillation * * * * Corrosion, Copper Strip * * Existent Gum * * Carbon Residue *1 Vapor Pressure * * Lead Content * *3 Freeze Point * Flash Point * * * * * FSII Content *

MSEP (JP-8, F-24, F-27,

Jet A & Jet A-1)

Conductivity (JP-5 & JP- 8, F-24, F-27 & Jet A-1)

*4

Thermal stability (B-1 requirement applies to JPTS and marine/multi-product mode receipt tank sample)

Sediment & Water Total Sediment aged Viscosity *7 Water Content * *8 *2 Emulsion *2 Foam Test * Knock Rating (RON / MON) *6 Lubricity *1

FAME *5 *1

Solid Contaminants *2

* The procedure to be used for conducting these tests will be as stated in the appropriate product specification and/or contract. For any products not covered under this table, contact Quality Assurance Representative for guidance.

NOTES:

1. F76 only.

2. Only if the specification has this requirement.

3. If contamination with leaded fuels is suspected.

4. If fuel contains conductivity additive, wait approximately 2 minutes after obtaining sample for charges in the fuel to dissipate before performing CU testing.

5. Only for product transported through multi-product systems, including marine transport.

6. Perform only if Lead Content is performed and fails and/or contamination with another product is suspected. In the case of pipeline, this test shall be performed when considered necessary.

7. For MIL-PRF-17331 and MIL-PRF-9000 viscosity is not required unless the tank has been in long term storage for 3 months.

8. Visual check.

TABLE IV, Conversion chart for tank trucks (TT) tank cars (TC), tank wagons (TW), tank & trailer (TRR), and intermodal containers (IMC)1, 2

Last Product Carried

PRODUCT TO BE LOADED5

Gasolines: MUR, MUM, MUP, EFM, E85, 100, 130, JAB

Aviation Turbine Fuels: JAA/A1, JP-8, F-24, JP-5, TS1, KS1/R/N, Aviation Turbine

Fuel3: JPTS

RP1/RP2 JP-10/PF1 Diesel Fuel: F-76 FSII Lubricating Oils

Diesel Fuels:

DF1, DF2,

DS1, DS2,

DSS, DSW,

BDI, MGO

Gasolines4 MUR, MUM, MUP, EFM, E85, 100, 130, JAB

Drain/Empty Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry

Aviation Turbine Fuels4, 9

JAA/A1, JP-8, F-24,

JP-5, TS1, KS1/R/N,

Drain/Empty

Drain/Empty

Steam/Dry

Aviation Turbine Fuel3 JPTS Drain/Empty Drain/Empty Drain/Empty Drain/Empty Steam/Dry Steam/Dry Steam/Dry Steam Dry Steam/Dry

RP1/RP2 Steam/Dry Steam/Dry Steam/Dry Drain/Empty Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry J10/PF-1 Steam Dry Steam/Dry Steam/Dry Steam Dry Drain/Empty Steam/Dry Steam/Dry Steam/Dry Steam/Dry Petroleum Solvent or Paint Thinner Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry

Diesel Fuel: F-76 Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Drain/Empty Steam/Dry Steam/Dry Drain/Empty Diesel Fuels4 DF1, DF2, DS1, DS2, DSS, DSW, MGO

Steam/Dry Steam/Dry7 Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Drain/Empty

FSII (SIH) Drain/Empty Drain/Empty Steam/Dry Steam/Dry Steam/Dry Steam/Dry Drain/Empty Steam/Dry Steam/Dry Lubricating Oils NO LOAD NO LOAD NO LOAD NO LOAD NO LOAD NO LOAD NO LOAD Steam/Dry6 Steam/Dry Biodiesel Blends(<B15)4

DF1, DF2, DS1, DS2, DSS,

DSW

Steam/Dry7

NO LOAD

Biodiesel Blends(>B15):

DF1, DF2, DS1, DS2,

BDI

Steam/Dry8

Heavy Fuel Oils, Distillate Fuels4 FS1, FS2, FS4, FS5, FS6

Residual Fuel Oils:

ISO 8217, class F (IFOs)

Naphtha Drain/Empty Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry Steam/Dry

TABLE IV Continued, Conversion chart for tank trucks (TT) tank cars (TC), tank wagons (TW), tank & trailer (TRR), and intermodal containers (IMC)1, 2

1. For previous cargoes not listed, contact DLA Energy Quality Operations Division at DLAEnergyQualityOperations@dla.mil for acceptability/cleaning procedures.

2. General Instructions for Tank Cars and Trucks

a. Conveyances (all) shall be dry and free from loose rust, scale, and dirt

b. Saran lined equipment should not be steam cleaned; water wash should suffice.

c. Petroleum products shall not be loaded into the conveyances where the previous cargo was caustic, acid, or chlorinated solvents.

d. Tank trucks and cars in liquid fertilizer service shall not load aviation turbine fuels directly but shall carry out at least two loads of commercial gasoline prior to the aviation turbine fuel load.

e. Conversion of Government-owned tank cars from liquid fertilizer service to aviation turbine fuel service shall only be done when no other alternative exists. Tank cars being converted from liquid fertilizer service to a petroleum product shall be adequately cleaned to remove all traces of liquid fertilizer. At a minimum, the equipment must be steam cleaned; dried and must be free from loose rust, scale, and dirt. After cleaning, but before loading aviation turbine fuels, at least two loads of commercial gasoline shall be carried prior to loading aviation turbine fuel. Equipment with unlined compartments should have its compartments lined with an approved coating at this time. Conveyances carrying their initial load of aviation turbine fuel following conversion shall not be released from the loading until they have been sampled a minimum of 24 hours after loading. In accordance with MIL-STD-3004-1A, samples shall undergo type B-2 testing plus Thermal Stability Test (if required by the product specification). After type B-2 tests indicate compliance with specification requirements, the conveyance can be released pending results of the Thermal Stability tests. The conveyance shall not be unloaded until the loading point notifies the destination that the Thermal Stability test (when required) has passed. When the above condition applies, the DD-250, Wide Area Workflow (WAWF) Energy Receiving Report (ERR) or equivalent form shall be so noted.

3. To be loaded only in aluminum or stainless-steel conveyance, or other conveyance lined with an approved epoxy coating. If equipment is coated, clean with hot fresh water not exceeding 58°C (136°F) and dry thoroughly.

4. If previous cargo contained dye marker, all traces of color must be removed.

5. If product to be loaded does not contain dye, then the vehicle shall not contain any traces of dye prior to loading.

6. Drain/empty only when same specification product is being loaded.

7. Prior to loading the aviation fuels listed, the conveyance must have carried a previous non-FAME cargo and then be steam cleaned and dried. Trucks that have previously carried biodiesel create a risk of cross-contamination of aviation turbine fuel with residual biodiesel components. Diesel fuel may contain up to 5% FAME without reporting it as biodiesel.

Because of the difficulties in making a load-rack of the presence of FAME in the previous load, the more stringent “Steam/Dry is required.

8. Drain and empty if loading biodiesel blend.

9. Cargos carrying dyed kerosene shall use the steam/dry cleaning procedure.

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DLA FORM 1889, OCT 2011

SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

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Supplemental Quality Assurance Provision (SQAP)

DSCC Form 2291, Feb 2004 online none standard

Quality Assurance

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SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

Supplemental Quality Assurance Provision (SQAP)

DSCC Form 2291, Feb 2004 online none standard

Quality Assurance

DLA

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REVISIONS

REV DESCRIPTION DATE APPROVED

DLA ENERGY QAP E22 9 Feb 2022 9 Feb 2022

ENERGY QAP E22 LIST OF INSPECTION OFFICES FOR DLA ENERGY CONTRACTS (DLA ENERGY) (FEB 2022)

The following lists shall be used to identify the Government inspection office assigned inspection and/or acceptance responsibility for DLA Energy contracts in a particular geographic area. These contracts include, but are not limited to, those for bulk petroleum products and additives, into-plane refueling, petroleum storage and laboratory services, coal, aerospace energy (including compressed gases), and posts, camps, and stations. The area of inspection responsibility and corresponding office code are assigned in paragraphs (a) and (b). The address and phone number of each inspection office, by office code, is provided in paragraph (c). Unless a particular inspection office is identified in another part of the contract, the assignments in this QAP shall apply.

(a) AREAS OF RESPONSIBILITY AND OFFICE CODES WITHIN THE CONTINENTAL UNITED STATES

(CONUS):

Alabama 110 Maine 110 Oklahoma 110 Arizona 120 Maryland 110 Oregon 120 Arkansas 110 Massachusetts 110 Pennsylvania 110 California 120 Michigan 110 Rhode Island 110 Colorado 120 Minnesota 110 South Carolina 110 Connecticut 110 Mississippi 110 South Dakota 110 Delaware 110 Missouri 110 Tennessee 110 District of Columbia 110 Montana 120 Texas 110 I Florida 110 Nebraska 110 Utah 120 Georgia 110 Nevada 120 Vermont 110 Idaho 120 New Hampshire 110 Virginia 110 Illinois 110 New Jersey 110 Washington 120 Indiana 110 New Mexico 120 West Virginia 110 Iowa 110 New York 110 Wisconsin 110 Kansas 110 North Carolina 110 Wyoming 120 2

Kentucky 110 North Dakota 110 Louisiana 110 Ohio 110

EXCEPTIONS:

1 The El Paso, Texas, area is assigned to Code 120 (DLA Energy Americas West).

2 The Newcastle, Wyoming, area is assigned to Code 110 (DLA Energy Americas East).

DEFENSE LOGISTICS AGENCY ENERGY

8725 JOHN J. KINGMAN ROAD

FORT BELVOIR, VIRGINIA 22060-6222

DISTRIBUTION PREPARED BY DATE ITEM

STATEMENT -A DLA ENERGY QAP E22

APPROVED FOR REVIEWED BY DATE NSN CODE IDNO.

PUBLIC RELEASE MULTIPLE 52838

DISTRIBUTION IS APPROVED BY DATE SIZE SCALE DRAWING NUMBER

"UNLIMITED"

DLA FORM 1889, OCT 2011 PREVIOUS EDITION IS USABLE Add Continuation Page SHEET 1 OF 4 PDF(DLA)

(b) AREAS OF RESPONSIBILITY AND OFFICE CODES OUTSIDE THE CONTINENTAL UNITED STATES (OCONUS) (INCLUDING ALASKA AND HAWAIi):

Afghanistan 400 Cyprus 200 Malaysia 300 Singapore 300 Africa 200 3 Egypt 400 3 Maldives 300 South America 110 Alaska 130 Europe (Continental) 200 Malta 200 South Korea 300 Antarctica 300 Georgia 200 Mauritius 200 Sri Lanka 300 Armenia 200 Greenland 200 Mexico 110 Syria 400 Ascension Island 110 Hawaiian Islands 300 Midway Island 300 Taiwan 300 Australia 300 Hong Kong 300 Mongolia 300 Tajikistan 400 Azerbaijan 200 Iceland 200 Myanmar 300 Thailand 300 Azores 200 India 300 Nepal 300 Turkey 200 Bahrain 400 Indonesia 300 New Zealand 300 Turkmenistan 400 Bangladesh 300 Ireland 200 North Korea 300 United Arab Bermuda 110 Iran 400 Oman 400 Emirates 400 Bhutan 300 Iraq 400 Pacific Islands United Kingdom 200 Brunei 300 Israel 200 (Central & South) 300 Uzbekistan 400 Cambodia 300 Japan 300 Pakistan 400 Vietnam 300 Canada 1104 Jordan 400 Papua New Guinea 300 Wake Island 300 Canary Island 200 Kazakhstan 400 Philippines 300 Yemen 400 Caribbean Islands 110 Kuwait 400 Qatar 400 Central America 110 Kyrgyzstan 400 Russia 200 Chagos Archipelago 300 Laos 300 Ryukus Islands, Japan 300 China 300 Lebanon 400 Saudi Arabia 400 Comoros 200 Madagascar 200 Seychelles Is. 200

EXCEPTIONS:

3 Except for Egypt, which is assigned to DLA Energy Middle East (Code 400), all other countries in Africa fall under DLA Energy Europe (Code 200).

4 For Canada locations, contact DLA Energy Americas East (Code 110) to confirm coverage.

(c) INSPECTION OFFICES AND CODES.

110. DLA Energy Americas East ATTN: Quality Manager 5

Federal Building, Suite 1005 2320 LaBranch Street Houston, TX 77004-1091 Phone: (713) 332-4113

FAX: (713) 718-3891

SUPPLEMENTAL QUALITY ASSURANCE PROVISION

(SOAP)

DISTRIBUTION STATEMENT -A

SIZE SCALE CODE IDNO.

52838

DRAWING NUMBER

DLA FORM 1889, OCT 2011 PREVIOUS EDITION IS USABLE Add Continuation Page SHEET 2 OF 4 PDF(DLA)

120. DLA Energy Americas West

S , CA 90

Phone: (424) 347-3101/3102

FAX: (424) 347-3120

130. DLA Energy Americas North

1480 Sijan Street, Suite 300 Joint Base Elmendorf-Richardson, AK 99505 Phone: (907) 384-7180

FAX: (907) 384-1086

200. DLA Energy Europe and Africa

Military Mailing Address:

DLA Energy Petroleum Lab

CMR422

APO AE 09067-0422

Phone: 49-63 l-3406-2285/2286 6

FAX: 49-631-3406-2289 6

Commercial Shipping Address:

DLA Energy Petroleum Lab ATTN: Quality Manager Bldg. 320, Rhine Ordinance Barracks Am Opelkreisel 67663 Kaiserslautern, Germany

300. DLA Energy lndo-Pacific

Bldg. 17000, Room 21

APO AP 96543

Phone: (671) 366-7762

FAX: (671) 366-7767

[Location: Guam]

DLA FORM 1889, OCT 2011 PREVIOUS EDITION IS USABLE Add Continuation Page SHEET 3 OF 4 PDF(DLA)

400. DLA Energy Middle East

PSC 851, Box 180

FPO AP 09834-2800

Phone: 973-1785-6493 6

FAX: 973-1785-4650 6

[Location: Bahrain]

5 Designated location of the DLA Energy Regional Quality Manager/Pre-Award Survey Monitor.

6 Dial 011 before these numbers when calling from the U.S. When calling these numbers from outside the U.S., use the appropriate international long distance prefix for the country where the call originates.

DLA FORM 1889, OCT 2011 PREVIOUS EDITION IS USABLE Add Continuation Page SHEET 40F 4 PDF(DLA)

2022-02-09T15:07:40-0500

MILLS.KEITH.1050183110

2022-02-09T15:07:59-0500

MILLS.KEITH.1050183110

2022-02-14T08:44:39-0500

KNAPP.RICHARD.BRUCE.1027134021

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SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)

Supplemental Quality Assurance Provision (SQAP)

DSCC Form 2291, Feb 2004 online none standard

Quality Assurance

DLA

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October 2011 (added Energy; updated supply center names)

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JUN 2014 08 JUL 2014

8 Jul 2014.

PREVIOUS EDITION IS OBSOLETE.

DLA FORM 1889, JUL 2023 Page 1 of 3

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Prescribed by: eSOP 4155.05-001 Sponsor: J3

ENERGY QAP C16.01 02/06/2026

C16.01 TURBINE FUEL, AVIATION (JP5) (DLA ENERGY FEB 2026)

National Stock Number: Product Nomenclature: DLA Energy Product Code:

9130-00-273-2379 Turbine Fuel, Aviation, JP-5 JP5

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

(a) Product shall meet MIL-DTL-5624X, Turbine Fuel, Aviation, Grade JP-5 (NATO F-44), dated February 12, 2024.

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

(1) PROPERTIES:

(i) 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 Micro- Separometer (MSEP)). MSEP analysis shall be performed per the Contractor's election in MIL-DTL-5624X, dated February 12, 2024.

(2) SYNTHETIC BLEND COMPONENT (SBC) and CO-HYDROPROCESSED SYNTHESIZED KEROSENE:

(i) If a fuel containing an SBC or a co-hydroprocessed synthesized kerosene is being offered, notification shall be made to the contracting point of contact with submission of relevant details regarding the blend percentage and which Annex of ASTM D7566 for the SBC used, and which feedstocks and co-processing percentage for co-hydroprocessed synthesized kerosene. Only SBCs approved in ASTM D7566, MIL-DTL-83133L, MIL-DTL-5624X, and co-hydroprocessed synthesized kerosene produced from approved feedstock and percentage in ASTM D1655, MIL-DTL-83133L, and MIL-DTL-5624X shall be acceptable to the government

(3) TEST MODIFICATIONS:

(i) Filtration 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.

(ii) 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.

(iii) Micro-Separometer Testing:

(A) 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. This process will be repeated if the composition of the fuel changes due to changes in processing or blending operations.

DLA Land & Maritime DLA Troop Support DLA Aviation DLA Energy

DEFENSE LOGISTICS AGENCY, ENERGY

8725 JOHN J. KINGMAN RD

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C16.01 TURBINE FUEL, AVIATION (JP5)

REVIEWED BY DATE

02/10/2026

NSN

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APPROVED BY DATE

SIZE

SCALE

1:1

DLA FORM 1889, JUL 2023 Page 2 of 3

(4) LOCATION:

(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, Washington, and Alaska shall have a minimum Flash Point of 62.5oC at the custody transfer point.

(iii) All JP-5 procured for delivery to Australia shall have a minimum Flash Point of 61.5°C at the origin custody transfer point.

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

(v) For the deep freeze program, 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).

(c) ADDITIVES: Additives are required for deliveries of JP-5, per MIL-DTL-5624X, dated February 12, 2024, unless addition is excluded by specific solicitation line item, applicable contract clause, or another contractual requirement.

(1) FSII included in jet fuel shall conform to MIL-DTL- 85470C, Inhibitor, Icing, Fuel System, High Flash, dated March 5, 2024. 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.

(2) 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.

(d) OTHER REQUIRMENTS:

(1) ADDITIONAL SAMPLING: The government may request a sample of JP5 during each quarter of contract performance not to exceed 5 gallons. Samples shall be shipped in a 5-gallon epoxy lined can (preferred) or five 1-gallon epoxy lined cans. (NOTE: These samples are in addition to those required in accordance with Quality Assurance Provision (QAP) E1). The sample shall be shipped to

Naval Air Station HAZMART 5-Gallon TEST SAMPLE 22680 Hammond Road Bldg. 2385 Patuxent River, MD 20670 Attn: Terrence Dickerson, AB44100 Fuels & Lubricants Phone: (301) 757-0447; Email: terrence.w.dickerson.civ@us.navy.mil

(SQAP)

DLA FORM 1889, JUL 2023 Page 3 of 3

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

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

The Sample shall be shipped within 30 days of the procurement batch delivery. A batch is defined as: A specific quantity of product that is processed or utilized as a single unit and tested to meet test criteria and specifications.

(i) 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 Air Station. The RCQ or CoA for each individual tank shall be representative of Level A testing for the JP-5 product.

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

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: Terrence Dickerson at terrence.w.dickerson.civ@us.navy.mil or (301) 757-0447. Samples shall be shipped to:

20mL TEST SAMPLE 22680 Hammond Road Bldg. 2385 Patuxent River, MD 20670

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

Untitled

DRAFT

SAMPLE

PREVIOUS EDITION IS OBSOLETE.

DLA FORM 1889, JUL 2023

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Prescribed by: eSOP 4155.05-001 Sponsor: J3

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DISTRIBUTION STATEMENT - A APPROVED FOR PUBLIC RELEASE DISTRIBUTION IS "UNLIMITED"

9.0.0.2.20120627.2.874785

DLA Form 1889, "SUPPLEMENTAL QUALITY ASSURANCE PROVISION (SQAP)"

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Revisions - Description: ENERGY QAP C16.01

Revisions - Date: 02/06/2026

Revisions - Approved:

Comments:

DLA Land & Maritime - Select for address and Code ID Number:

DLA Troop Support - Select for address and Code ID Number:

DLA Aviation - Select for address and Code ID Number:

DLA Energy - Select for address and Code ID Number:

address_item: DEFENSE LOGISTICS AGENCY, ENERGY

8725 JOHN J. KINGMAN RD

FORT BELVOIR, VIRGINIA 22060-6222

Select to clear address and Code ID Number:

PREPARED BY (enter signature):

PREPARED BY (enter date): 2/10/2026 item: C16.01 TURBINE FUEL, AVIATION (JP5)

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REVIEWED BY (enter date): 02/10/2026 nsn: MULTIPLE

CODE ID NUMBER: 52838

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ENERGY QAP C16.23 02/06/2026

C16.23 FUEL, NAVAL DISTILLATE (F-76) (DLA ENERGY FEB 2026)

National Stock Number: Product Nomenclature: DLA Energy Product Code:

9140-00-273-2377 Fuel, Naval Distillate F76

(a) Naval Distillate Fuel (F-76) shall conform to the requirements of Military specification MIL-DTL-16884R dated 03 Jan 2025. Nomenclature for Naval Distillate Fuel (F-76) is shown above.

(b) SPECIFICATION MODIFICATIONS:

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

(2) SYNTHETIC COMPONENTS:

(i) For F-76 containing a synthetic component, the synthetic component shall be certified to Tables A-I and A-II of MIL- DTL-16884R; for synthesized iso-paraffins, the synthetic component shall be certified to Tables B-I and B-II of MIL-DTL-16884R.

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

(3) TEST MODIFICATIONS:

(i) Flash Point: All batches of F-76 that are presented for Government acceptance at origin shall meet a minimum flash point requirement of 62.5 degrees Celsius (°C).

(ii) FAME: F-76 offered from a location other than where refined (excludes…