Att 1 - QAPS.pdf

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.

T A

B L

E

II

, M in im um

S am pl in g an d T es tin g R eq ui re m en ts fo r

Pe tr ol eu m P ro du ct s

Se ri es

, t an ke rs a nd b ar ge s1

IT

E

M W

H E

N T

O S

A M

PL

E

L O

C A

T

IO

N O

F

SA

M

PL

E T

Y

PE

O F

SA

M

PL

E

T

E

ST

R E

Q U

IR

E

D

1.

a

Prior to Loading

B ef or e ac ce pt an ce o f n ew m at er ie l an d af te r e st ab lis hm en t o f n ew ba tc h4

Ea ch sh or e st or ag e ta nk

Si ng le T an k

C om po si te o r A ll

Le ve ls A

5, 1.

b

A fte r l in e pa ck b ut p rio r t o lo ad in g A s c lo se to th e cu st od y tra ns fe r po in t a s p os si bl e

Li ne

S am pl e

C 7, D ed ic at ed

S ys te m

B

-1 N on -D ed ic at ed

S ys te m

1.

c

During Loading

Im m ed ia te ly a fte r s ta rt of lo ad in g/ sh ip m en t

A s c lo se to th e cu st od y tra ns fe r po in t a s p os si bl e Li ne S am pl e C

1.

d

A fte r f irs t i n

V es se l c ar go c om pa rtm en t(s

Sp ot

C 7, 1.

e

D ur in g lo ad in g

A s c lo se to th e cu st od y tra ns fe r po in t a s p os si bl e

Li ne

S am pl e

H ou rly V is ua l6, 8 , R et ai n10

1.

f

After Loading fte r l oa di ng v es se l c ar go c om pa rtm en t

A ll

Le ve l ( C om bi ne A ll Le ve ls to o ne

V ol um et ric C om po si te

S am pl e13

C 6, , 1

1, R em ai nd er o f B

(R et ai n fu el fo r B

-1 re fe re e te st g)

N O

T E

S:

dd iti on al re qu ire m en ts to in cl ud e re ta in sa m pl es m ay b e re qu ire d.

S ee

Q ua lit y

A ss ur an ce P ro vi si on s ( C o r E

-Q A

P) fo r f ur th er d et ai ls

2.

R ef er to

A

ST

M In te rn at io na l D fo r s am pl in g pr oc ed ur es

3.

T es t r es ul ts sh al l b e co m pa re d ag ai ns t t he q ua lit y re le as e ce rti fic at e.

A ny d is cr ep an ci es sh al l b e id en tif ie d, in ve st ig at ed

, a nd re so lv ed

4.

U po n pr oc ur em en t a t r ef in er ie s, bl en di ng in sta lla tio ns

, e tc

. a nd a t m ai n in sta lla tio ns in cl ud in g na tio na l d ep ot s & o ce an im po rti ng p oi nt s o n es ta bl is hm en t o f n ew b at ch es

5.

P rio r t o pe rf or m in g

A -le ve l t es tin g, th e ho m og en ei ty o f e ac h ba tc h sh al l b e de te rm in ed . R ef er to p ar ag ra ph

(b )(1 iii

)(C ) o f t hi s d oc um en t f or a dd iti on al d et ai ls

6.

T es t f or F

SI

I a nd S

D A o nl y if lin e in je ct ed

7.

I f s am pl e fa ils a pp ea ra nc e, p er fo rm p ar tic ul at e m at te r u sin g ap pr ov ed m et ho ds a s o ut lin ed in th e ap pl ic ab le sp ec ifi ca tio n.

8.

L ub ric ity a ls o re qu ire d fo r F

-7 on ly if li ne in je ct ed , o r d et er m in e

LI

A c on ce nt ra tio n by v ol um et ric m ea su re m en t/c al cu la

9.

F irs t i n sh al l b e do ne a fte r o ne (1

) m et er o r a fte r l in e di sp la ce m en t w hi ch ev er is th e gr ea r.

Fo r a ll ta nk er an d ba rg e, a fl ow

-p ro po rti on al sa m pl e ta ke n in a cc or da nc e w ith

M

PM

S C ha pt er

, S ec tio n

2, is p re fe rre d at th e cu sto dy tr an sf er p oi nt

. H ow ev er

, m an ua l s am pl es ta ke n in a cc or da nc e w ith M

PM

S

C ha pt er

8, S ec tio n ar e ac ce pt ab le if th ey a re ta ke n ho ur ly th ro ug ho ut th e sh ip m en t a nd th at th e qu an tit y of th e co m po si te sa m pl e m ee ts th e re qu ire m en ts in

Ta bl e I

B es t p ra ct ic e is fo r B

-1 te st co m pl et io n fo r F O

B O rig in

P ro cu re m en ts (o r T yp e A le ve l t es tin g w he n sp ec ifi ed in c on tra ct fo r F

O B

D es tin at io n

Pr oc ur em en ts

) p rio r t o ve ss el re le as e.

B as ed o n

Q A

R de ci si on , v es se l m ay sa il af te r C

T es ts to m ee t s ch ed ul e re qu ire m en ts in cl ud in g to a vo id p re di ct ed w ea th er ; r em ai nd er o f B

-1 te st s t o be c om pl et ed b ef or e ar riv al a t n ex t l oa d or d is ch ar ge p or t.

Te st re po rt w ill b e pr ov id ed to d es ig na d di sc ha rg e po rt.

Ty pe

A le ve l t es tin g re qu ire d fo r F O

B D es tin at io n Pr oc ur em en ts (u nl es s o th er w is e sp ec ifi ed b y co nt ra ct

A s d ef in ed b y

A

PI

M

PM

S C ha pt er

-1 , s ec tio n 3.

Fo r p ro du ct v er ifi ca tio n pu rp os es . R es ul ts of

C -te st m us t f al l w ith in re pr od uc ib ili ty o f s ou rc e ta nk

A -le ve l r es ul ts

N ew c ar go fr om sa m e ba tc h, w ith in da ys

, w ill o nl y re qu ire

B -1 te st in g to v er ify p re vi ou s A -le ve l t es t r es ul ts . B

-1 le ve l v er ifi ca tio n te st re su lts sh ou ld fa ll w ith in g re pr od uc ib ili ty o f s ou rc e ta nk A

-le ve l r es ul ts

A

B L

E

II

, M in im um

S am pl in g an d T es tin g R eq ui re m en ts fo r

Pe tr ol eu m P ro du ct s

Se ri es

, p ip el in e, ta nk tr uc ks

, t an k ca rs , i so -c on ta in er s1, IT

E

M W

H E

N T

O S

A M

PL

E

L O

C A

T

IO

N O

F

SA

M

PL

E T

Y

PE

O F

SA

M

PL

E

T

E

ST

R E

Q U

IR

E

D

2.

a

Prior to Shipment

B ef or e ac ce pt an ce o f n ew m at er ie l a nd af r e st ab lis hm en t o f n ew b at

S hi pm en t S to ra ge T an k

Si ng le T an k

C om po si or ll Le ve ls

A 9, 2.

b

A fte r l in e pa ck b ut p rio r t o lo ad in g/ sh ip m en t

A s c lo se to th e cu st od y tra ns fe r p oi nt a s po ss ib le

Li

S am pl e

C 5, D ed ic at ed

S ys te m

B -1

N on

-D ed ic at ed S ys te m

2.

c

During Shipment

Im m ed ia te ly a fte r s ta rt of lo ad in g/ sh ip m en t A s c lo se to th e cu st od y tra ns fe r p oi nt a s po ss ib le a nd d ow ns tre am o f t he fi lte r se pa ra to r ( if eq ui pp ed

Li ne

S am pl e

C 5, 2.

d

Pi pe lin e

O nl y:

H ou rly a fte r s ta rt of lo ad in g or sh ip m en t10 lo se to th e cu st od y tra ns fe r p oi nt a s po ss ib le a nd d ow ns tre am o f t he fi lte r se pa ra to r ( if eq ui pp ed

Li ne S am pl e A pp er an ce

5, (R et ai n fu el fo r B

-1 re fe re e te st in g)

2.

e

D ai ly o n fir st fi ll an d an yt im e a ne w ta nk is pl ac ed o n is su e

(a fte r l in e di sp la ce m t)

TT

, T

C , I

SO

, R ef ue le rs o r o th er o ve r t he ro ad tr an sp or ta tio n m od es o nl y lo se to th e cu st od y tra ns fe r p oi nt a s po ss ib le (L oa di ng R ac k or F ill P oi nt

) a nd do w ns tre am o f t he fi lte r s ep ar at or

(i f eq ui pp ed

Li ne

S am pl e

C ol or (b y vi su al m et ho d) an

A pp ea ra nc e5 .

If v is ua l f ai ls p er fo rm

C

2.

f

After Loading

D ai ly fo r e ac h co nv ey an ce m od e

(N re qu ire d fo r p ip el in e op er at io ns

C ar go

C om pa rtm en t o r a no th er p oi nt th at p ro vi de s a re pr es en ta tiv e sa m pl e

A ll

Le ve l A pp ea ra nc eo n ea co pa rtm t n co m po sit e 5

,6 ,8

2.

D ru m s

Sa m pl e of e ac h lo t o f p ro du ct sh al l b e ta ke n fr om a p re de te rm ed nu be r o f r an do m ly se le ct ed d ru m s14 M ul ti-dr um

C om po

C13

O

T E

S:

1.

A dd iti on al c on tra ct ua l r eq ui re m en ts to in cl ud e re ta in sa m pl es m ay b e re qu ire d.

S ee C on tra ct Q ua lit y A ss ur an ce

P la ns (C o r E

-Q A

Ps ) f or fu rth er d et ai ls

2.

R ef er to

A

ST

M In te rn at io na l D fo r s am pl in g pr oc ed ur es

3.

T es t r es ul ts sh al l b e co m pa re d ag ai ns t t he q ua lit y re le as e ce rti fic at e.

A ny d is cr ep an ci es sh al l b e id en tif ie d, in ve st ig at ed

, a nd re so lv ed

4.

U po n pr oc ur em en t a t r ef in er ie s, bl en di ng in sta lla tio ns

, e tc an d at m ai n in st al la tio ns in cl ud in g na tio na l d ep ot s & o ce an im po rti ng p oi nt s o n es ta bl ish m en t o f n ew b at ch es

5.

T es t f or

F

SI

I a nd

S D

A o nl y if lin e in je ct ed

6.

I f s am pl e fa ils a pp ea ra nc e, p er fo rm p ar tic ul at e m at te r u si ng a pp ro ve d m et ho ds a s o ut lin ed in th e ap pl ic ab le sp ec ifi ca tio n.

7.

T yp e

A le ve l t es tin g re qu ire d fo r F O

B D es tin at io n Pr oc ur em en ts (u nl es s o th er w is e sp ec ifi ed b y co nt ra ct

8.

I f t he c on ve ya nc e is c om pa rtm en ta liz ed

, a p ro po rti on al sa m pl e sh al l b e ta ke n fro m e ac h co m pa rtm en t s uc h th at a to ta l o f o ne li te r i s c ol le ct ed fr om th e co nv ey an ce

9.

F ilt ra tio n tim e te st in g is re qu ire d fo r J

P-

JP

-8 a nd sh al l m ee t c on tra ct re qu ire m en t.

Fo r p ip el in e sh ip m en ts

, a fl ow -p ro po rti on al sa m pl e ta ke n in a cc or da nc e w ith M

PM

S

C ha pt er

, S ec tio n 2, is p re fe rre d at th e cu sto dy tr an sf er p oi nt . H ow ev er , m an ua l s am pl es ta ke n in a cc or da nc e w ith

M

PM

S C ha pt er

Se ct io n ar e ac ce pt ab le if th ey a re ta ke n ho ur ly th ro ug ho ut th e sh ip m en t a nd th at th e qu an tit y of th e co m po si te sa m pl e m ee ts th e re qu ire m en ts in T ab

I.

. P rio r t o pe rf or m in g A

-le ve l t es tin g, th e ho m og en ei ty o f e ac h ba tc h sh al l b e de te rm in ed

. R ef er to p ar ag ra ph (b

1)

(ii i)(

C ) o f t hi s d oc um en t f or a dd iti on al d et ai ls

Lu br ic ity a ls o re qu ire d fo r F -7 on ly if li ne in je ct ed o r d et er m in e

LI

A c on ce nt ra tio n by v ol um et ric m ea su re m en t/c al cu la

Fo r p ro du ct v er ifi ca tio n pu rp os es

. R es ul ts of C

-te st m us t f al l w ith in re pr od uc ib ili ty o f s ou rc e ta nk re su lts

. A co m po si te sa m pl e of ga llo ns (8 li te rs ) f or A vi at io n

Tu rb in e

Fu el sa nd ga llo n

(4 li te rs

) f or a ll ot he r f ue ls fo re ac h lo t o f p ro du ct sh al l b e ta ke n fro m a p re de te rm in ed n um be r o f r an do m ly se le ct ed d ru m s.

T he to ta l nu m be r o f d ru m s s am pl ed p er lo t s ha ll, a t a m in im um , b e th at c ite d in T ab le

II

Io f A

PI

M

PM

S ch ap te r 8 .1

(A

ST

M d bu t m ay b e in cr ea se d at th e go ve rn m en t's o pt io

A

B L

E

II

, M in im um

S am pl in g an d T es tin g R eq ui re m en ts fo r

Pe tr ol eu m P ro du ct s

Se ri es

, p ro du ct r ec ei pt a nd d is ch ar ge s f or ta nk er s a nd b ar ge s (

FO

B

D es tin at n)

IT

M

W H

E N

T O

S A

M

PL

E L

O C

A T

IO

N

O F

SA

M

PL

E

T Y

PE

O

F

SA

M

PL

E T

E

ST

R E

Q U

IR

E

D

3.

a

Prior to Discharge

Pr io r t o di sc ha rg e

Fr om e ac h ve ss el c ar go c om pa rtm en t A ll Le ve l

A pp ea ra nc e an d

D en si ty

3.

b

Fr om e ac h ve ss el c ar go c om pa rtm en t

A ll

Le ve l (C om bi ne A ll Le ve ls

V ol um et ric C om po

Sa pl e)

3.

During Discharge

W ith in m in ut es a fte r s ta rt an d ho ur a fte r u nt il co m pl et n

D oc k/

D is ch ar ge M an ifo ld H ea de r Li ne S am pl e / R et ai n Pe rf or m A pp ea ra nc e te st 2, an d th en re ta in fu el fo r R ef er ee te st in g

3.

e

After Discharge

If re m ai nd er o f f ue l w ill b e sh ip pe he r D

FS

P v es se l c om pa rtm en t w ith fu el re ai ni ng o n bo ar d A ll Le ve l

R et ai n un til d is ch ar ge at de st in at io n

N O

T E

S:

1.

T es t f or fl as h po in t o n hi gh fl as h ca rg o ta nk s i f l ow a nd h ig h fla sh c ar go es a re c ar rie d to ge th er a bo ar d th e sa m e ve ss el w ith ou t s eg re ga te d ve nt in g sy ste m s.

2.

F or a vi at io n fu el d el iv er y, F

SI

I a nd S

D A sh al l b e te ste d on ly if li ne in je ct ed

Th is re qu ire s a n ad di tio na l q ua rt sa m pl e.

3.

es t f or a dd iti ve s i f l in e in je ct ed d ow ns tre am o f t he in je ct or

If lin e in je ct in g

LI

A in to

F -7

6, te st fo r l ub ric ity

B L

E

II

, M in im um

S am pl in g an d T es tin g R eq ui re m en ts fo r

Pe tr ol eu m P ro du ct s

Se ri es

, p ro du ct r ec ei pt fr om p ip el in e (F

O B

D es tin at io n)

IT

M

W H

E N

T O

S A

M

PL

E L

O C

A T

IO

N

O F

SA

M

PL

E

T Y

PE

O

F

SA

M

PL

E T

E

ST

R E

Q U

IR

E

D 4.

c

During Receipt

D ur in g pi pe lin e re ce ip t

C us to dy tr an sf er p oi

S am pl e/

R et ai n

G al lo n M in im um

4.

d

D ur in g pi pe lin e re ce ip t, im m ed ia te ly a fte r st ar t, M id po in t a nd h ou r p rio r t o co m pl et n3 lo se to th e cu st od y tra ns fe r p oi nt a s po ss ib

4.

After Receipt

A fte r r ec ei pt o f f ue l

Ea ch re ce ip t t an k

A ll le ve l

T ef er to A

ST

M

In te rn at io na l D fo r s am pl in g pr oc ed ur es

2.

R et ai n fo r r ef er ee te st in g in th e ev en t a fa ilu re o cc ur s o n re ce ip t t an k.

R et ai n sa m pl e fo r 4 da ys

. S am pl in g is

IA

W

A

PI

M

PM

S C ha pt er

3.

F ue l f ro m a n ew b at ch w ill b e co ns id er ed a n ew re ce ip t f or q ua lit y co nt ro l p ur po se s.

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.

B L

E

IV

, C on ve rs io n ch ar t f or ta nk tr uc ks (T

T ) t an k ca rs

(T C ta nk w ag on s ( T

W ta nk tr ai le r (T

R in te rm od al c on ta in er s (

IM

C )1, L as t P ro du ct ar ri ed

PR

D U

C T

T O

B E

L O

A D

E

G as ol in es

: M U

R

M U

M , M

U P, E

FM

E8

5, , 1

, J

B vi at io n

Tu rb in e

Fu el s:

JA

A /A

1, JP

-8

, F -2

4, JP

-5

TS

1, K S1

/R /N

A vi at io n Tu rb in e Fu el 3 :

TS

P1

/R P2

0/

PF

D ie se l F ue l:

F-

FS

II

Lu br ic at in g O ils D ie se l F ue ls

D F1

, D F2

D

S1 , D

S2

D

SS

, D

SW

B

D I, M G

O G as ol in es

M

U R

, M U

M

M U

P, E

FM

, E

, 1

0, JA

B

D ra in /E m pt y St ea m

/D ry

St m m m m m m m vi at io n Tu rb in e Fu el s4, JA

A

/A 1, JP

-8

, F -2

4, -5

, T S1

, K S1

/R /N

D ra in

/E m pt y

D ra in /E m pt y St ea m

/D ry

St ea m /D ry St ea m

/D ry

St ea m /D ry St ea m

/D ry

St ea m /D ry St ea m

/D ry

A vi at io n Tu rb in e Fu el

JP

TS

D ra in /E m pt y D ra in

/E m pt y

D ra in /E m pt y D ra in

/E m pt y

St ea m m m m m

P1

/R P2

St ea m m m ra in /E m pt y St ea m m m

/D ry

St ea m /D ry St ea m

J1

0/

PF

-1 St ea m

D ry

St ea m /D ry St ea m

/D ry

St ea m D ry D ra in

/E m pt y

St ea m /D ry St ea m

/D ry

St ea m /D ry St ea m

/D ry

Pe tro le um

S ol ve nt o r P ai

Th ne r St ea m m m m m m m m m ie se l F ue l:

F-m

/D ry

St ea m /D ry St ea m

/D ry

St ea m /D ry St ea m

/D ry

D ra in /E m pt y St ea m

/D ry

St ea m /D ry D ra in

/E m pt y

D ie se l F ue ls

4 D F1

, D F2

D

S1 , D

S2 , D

SS

, D

SW

M G

O St ea m

/D ry

St ea m /D ry

St ea m /D ry St ea m

/D ry

St ea m /D ry St ea m

/D ry

St ea m /D ry St ea m

/D ry

D ra in /E m pt y

FS

II

(S

IH

D ra in

/E m pt y

D ra in /E m pt y St ea m

/D ry

St ea m /D ry St ea m

/D ry

St ea m /D ry D ra in

/E m pt y

St ea m /D ry St ea m

/D ry

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

St ea m /D ry

St ea m /D ry

D F1

, D F2

, D S1

, D S2

, D

SS

D

SW

St ea m m

/D ry

N

O L

O A

D N

O L

O A

D N

O L

O A

D St ea m

/D ry

St ea m /D ry St ea m

/D ry

St ea m /D ry

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

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N O

L O

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St ea m /D ry

N O

L O

A D

N O

L O

A D

N O

L O

A D

N O

L O

A D

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N O

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N O

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/D ry

St ea m /D ry St ea m

/D ry

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/D ry

St ea m /D ry St ea m

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C on tin ue d, C on ve rs io n ch ar t f or ta nk tr uc ks

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LA

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2.

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on ve ya nc es (a

ll) sh al l b e dr y an d fr ee fr om lo os e ru st, sc al e, a nd irt b.

Sa ra n lin ed e qu ip m en t s ho ul d no t b e st ea m c le an ed

; w at er w as h sh ou ld su ff ic c.

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d.

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. T an k ca rs b ei ng co nv er te d fr om li qu id fe rti liz er se rv ic e to a p et ro le um p ro du ct sh al l b e ad eq ua te ly c le an ed to re m ov e al l t ra ce s o f l iq ui d fe rti liz er . A t a m in im um , t he e qu ip m en t m us t b e st cl ne d;

d rie d an d m us t b e fr ee fr om lo os e ru st

, s ca le , a nd d irt . A fte r c le an in g, b ut b ef or e lo ad in g av ia tio n tu rb in e fu el s, at le as t t w o lo ad s o f c om m er ci al g as ol in e sh al l b e ca rr ie d pr io r t o lo ad in g av ia tio n tu rb in e fu el . E qu ip m en t w ith u nl in ed c om pa rtm en ts sh ou ld h av e its c om pa rtm en ts li ne d w ith a n ap pr ov ed c oa tin g at th is ti m e.

C on ve ya nc es c ar ry in g th ei r i ni tia l l oa d of a vi at io n tu rb in e fu el fo llo w in g co nv er sio n sh al l n ot b e re le as ed fr om th e lo ad in g un til th ey h av e be en sa m pl ed a m in im um o f 2 ho ur s a fte r l oa di ng

. I n ac co rd an ce w ith M

IL

-S

TD

-3

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n) . A fte r t yp e

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T he rm al

S ta bi lit y te st s.

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Th er m al

S ta bi lit y te st (w he n re qu ire d) h as p as se d.

W he n th e ab ov e co nd iti on a pp lie s, th e

D D

-2

, W id e A re a

W or kf lo w (W

A W

F) E ne rg y R ec ei vi ng

R ep or t (

ER

R

) o r e qu iv al en t f or m sh al l b e so n ot ed

3.

To b e lo ad ed o nl y in a lu m in um o r s ta in le ss

-s te el c on ve ya nc e, o r o th er c on ve ya nc e lin ed w ith a n ap pr ov ed e po xy c oa tin g.

If e qu ip m en t i s c oa te d, c le an w ith h ot fr es h w at er n ex ce ed in g

°C

(1

°F ) a nd d ry th or ou gh ly

4.

If p re vi ou s c ar go c on ta in ed d ye m ar ke r, al l t ra ce s o f c ol or m us t b e re m ov ed

5.

If p ro du ct to b e lo ad ed d oe s n ot c on ta in d ye

, t he n th e ve hi cl e sh al l n ot c on ta in a ny tr ac es o f d ye p rio r t o lo ad in g.

6.

D ra in /e m pt y on ly w he n sa m e sp ec ifi ca tio n pr od uc t i s b ei ng lo ad ed

7.

Pr io r t o lo ad in g th e av ia tio n fu el s l is te d, th e co nv ey an ce m us t h av e ca rr ie d a pr ev io us n on

-F A

M E ca rg o an d th en b e st ea m c le an ed a nd d rie d.

T ru ck s t ha t h av e pr ev io us ly c ar rie d bi od ie se l c re at e a ris k of c ro ss -c on ta m in at io n of a vi at io n tu rb in e fu el w ith re si du al b io di es el c om po ne nt s.

D ie se l f ue l m ay c on ta in u p to

F A

M E w ith ou t r ep or tin g it as b io di es el

B ec au se o f t he d iff ic ul tie s i n m ak in g a lo ad -r ac k of th e pr es en ce o f F A

M E in th e pr ev io us lo ad , t he m or e st rin ge nt

St ea m

/D ry is re qu ire d.

8.

ra in a nd e m pt y if lo ad in g bi od ie se l b le nd

9.

C ar go s c ar ry in g dy ed k er os en e sh al l u se th e st ea m

/d ry c le an in g pr oc ed ur

OPPENHEIM.LEE.B.122

9310131

Digitally signed by OPPENHEIM.LEE.B.1229310131 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=OPPENHEIM.LEE.B.1229310131 Date: 2015.07.30 16:00:30 -04'00'

SHANNON.MICHAEL.J.

1229294802

Digitally signed by SHANNON.MICHAEL.J.1229294802 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=SHANNON.MICHAEL.J.1229294802 Date: 2015.07.30 14:17:00 -04'00'

SHEPHERD.SANDRA.S.

1012568459

Digitally signed by SHEPHERD.SANDRA.S.1012568459 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=SHEPHERD.SANDRA.S.1012568459 Date: 2015.07.30 15:38:32 -04'00'

Digitally signed by OPPENHEIM.LEE.B.1229310131 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=OPPENHEIM.LEE.B.1229310131 Date: 2015.06.26 13:12:16 -04'00'

SHANNON.MICHAEL.J.

1229294802

Digitally signed by SHANNON.MICHAEL.J.1229294802 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=SHANNON.MICHAEL.J.1229294802 Date: 2015.06.26 08:57:05 -04'00'

SHEPHERD.SANDRA.S.

1012568459

Digitally signed by SHEPHERD.SANDRA.S.1012568459 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, Date: 2015.06.26 12:47:33 -04'00'

Digitally signed by OPPENHEIM.LEE.B.1229310131 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=OPPENHEIM.LEE.B.1229310131 Date: 2014.04.18 09:25:13 -04'00'

SHILLINGFORD.JAME

S.V.1046542440

Digitally signed by SHILLINGFORD.JAMES.V.1046542440 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=SHILLINGFORD.JAMES.V.1046542440 Date: 2014.04.17 12:04:54 -04'00'

TRELOAR.GEORGE.C.1

033837964

Digitally signed by TRELOAR.GEORGE.C.1033837964 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=TRELOAR.GEORGE.C.1033837964 Date: 2014.04.14 07:40:29 -04'00'

SHANNON.MICHAEL.J.

1229294802

Digitally signed by SHANNON.MICHAEL.J.1229294802 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=SHANNON.MICHAEL.J.1229294802 Date: 2014.07.07 14:11:51 -04'00'

OPPENHEIM.LEE.B.122

9310131

Digitally signed by OPPENHEIM.LEE.B.1229310131 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, cn=OPPENHEIM.LEE.B.1229310131 Date: 2014.07.08 10:12:33 -04'00'

SHEPHERD.SANDRA.S.

1012568459

Digitally signed by SHEPHERD.SANDRA.S.1012568459 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=DLA, Date: 2014.07.08 10:04:48 -04'00'

ATKINS.RENRICK.L.10

24389320

Digitally signed by

ATKINS.RENRICK.L.1024389320

Date: 2025.03.11 15:58:35 -04'00'

ROSE.JAMAAL.R.10502

93366

Digitally signed by

ROSE.JAMAAL.R.1050293366

Date: 2025.03.11 14:30:04 -04'00'

BANISZEWSKI.DANIE

L.J.1287388698

Digitally signed by

BANISZEWSKI.DANIEL.J.1287388698

Date: 2025.03.13 08:11:54 -06'00'

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

C16.01 TURBINE FUEL, AVIATION (JP5) (DLA ENERGY JAN 2025)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT

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

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

JP5

Product shall meet MIL-DTL-5624X, Turbine Fuel, Aviation, Grade JP-5, dated February 12, 2024.

(a) SPECIFICATION MODIFICATION: The requirements of Table I 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) 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.

(3) FLASH POINT.

(i) All batches of JP-5 that are presented for Government acceptance at origin and for subsequent shipment through a multiproduct pipeline, shall meet a minimum flash point requirement of 62.5°C. This requirement is meant to address multiproduct commercial pipelines and does not apply to multiproduct systems within a facility.

(ii) In the U.S. all JP-5 deliveries in California, Oregon, Washington, and Alaska shall have a minimum Flash Point of 62.5 oC at the custody transfer point.

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

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

(5) MICRO-SEPAROMETER (MSEP) REQUIREMENTS.

(i) Prior to initial production under this contract, the Contractor shall elect, on a one-time basis, which MSEP limit to meet for the balance of the contract. If the Contractor introduces Fuel System Icing Inhibitor (FSII) and/or Corrosion Inhibitor/Lubricity Improver (CI/LI) after verification of product conformance with the MSEP requirement, the product is not required to meet a fixed limit on subsequent MSEP tests.

(ii) If the Contractor elects to verify conformance with the MSEP requirement on a sample of product that does not contain

FSII and CI/LI, an additional MSEP test shall be performed on a hand blend containing jet fuel, FSII, CI/LI, and Antioxidant (only if required). The FSII shall be added to this hand blend at a concentration range between 0.08 volume percent minimum and 0.11 volume percent maximum. The amount of the CI/LI added to this hand blend shall be within the concentration range specified in QPL-25017.

(6) ADDITIONAL REQUIREMENT APPLICABLE TO DEEP FREEZE PROGRAM ONLY. The Deep Freeze Program is for Antarctic operations of the Department of Defense and other federal agencies; whereby JP-5 sulfur content shall not exceed 0.0015 mass-percent (15 ppm).

(b) ADDITIVES.

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

(2) 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,

(3) Line injection of additives (FSII and CI/LI) from shipping tank to delivery conveyance or other free on board (FOB) point is permitted under the following conditions:

(i) Additives must be proportionately injected throughout the entire loading process to ensure the additive is homogeneously blended into the jet fuel. The Contractor shall maintain records evidencing the homogeneous blending of all line injected additives. Such methods may include meter or tank gauge readings or test results taken at intervals to provide confidence in the injection process.

(ii) When FSII is required, additive concentration must be verified based on a representative sample from each shipping conveyance.

(c) Conformance to specification requirements at the custody transfer point is required, however, prior to shipment, a laboratory hand blend of JP-5 fuel with all additives required by this contract shall be tested to verify compliance with the required specification (except for MSEP). MSEP analysis shall be performed per the Contractor’s election in MIL-DTL-5624X, dated February 12, 2024.

(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

(e) 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

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

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

For each 20 mL sample provided by the Contractor, the Contractor shall also submit a Refinery Certificate of Quality (RCQ), or

Certificate of Analysis (CoA), as applicable, with the JP-5 sample when submitting to the US Naval Research Laboratory. The RCQ or CoA for each individual tank shall be representative of Level A testing for the JP-5 product.

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

QUANTITY OF SAMPLE WHEN SAMPLED SUBMISSION PERIOD

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

“Batch” Definition in accordance with MIL-STD-3004-1 latest edition, A specific quantity of product that is processed or utilized as a single unit and tested to meet test criteria and specifications.

The sample from each tank/batch shall be either an all-level sample or a composite of upper, middle, and lower samples. A copy of the batch’s full-specification test report shall accompany each sample. The sample container shall be any 20 mL amber borosilicate vial with a polytetrafluoroethylene (PTFE) lined screw cap. A tracking number for the samples shall be provided to: Terrence Dickerson at terrence.w.dickerson.civ@us.navy.mil or (301) 757-0447. Samples shall be shipped to:

Naval Air Station HAZMART 20mL TEST SAMPLE 22680 Hammond Road Bldg. 2385 Patuxent River, MD 20670

Contract Number

Contractor’s Name Product

Refinery Location Quantity of Tank/Batch

For samples containing synthetic components, include the following additional information:

Manufacturer of synthetic component

Batch Number Date of Test Report

Quantity of Tank/Batch Percent Composition

Production Process of Synthetic Component Feedstock

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).

(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 ), 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.

(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

C16.08-1 TURBINE FUEL, AVIATION (JET A) (DLA ENERGY JAN 2025)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE PRODUCT CODE

9130-00-359-2026 Turbine Fuel, Aviation, Jet A JAA

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.

(a) PRODUCT REQUIREMENTS. Jet A shall conform to the requirements of the latest version of ASTM D 1655, Standard Specification for Aviation Turbine Fuels, except as modified below, at the custody transfer point.

(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 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)

(ii) 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.

(2) Fatty Acid Methyl Ester (FAME)

(i) For offerors that will be offering Jet A FOB Destination and/or Origin TT, which involves staging jet fuel at a terminal via a multi-product pipeline, a Certificate of Quality of the issue tank must include testing for FAME for Acceptance of the fuel. The Test method to be used is either IP 585, IP 583, IP 590, IP 599, or ASTM D 7797. The Referee Method is IP 585.

Current ASTM D1655 Jet A specification allows no more than 50 parts per million of FAME in jet fuel.

(c) 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 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.

(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.

(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.

(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, revalidated May 25, 2021, 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 https://qpldocs.dla.mil/. 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.

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

(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

(e) REPORTS. Refer to the MATERIAL INSPECTION AND RECEIVING REPORT (QAP E40.01) contract provision for reporting requirements.

DEFENSE LOGISTICS AGENCY ENERGY

8725 JOHN J. KINGMAN ROAD

FORT BELVOIR, VIRGINIA 22060-6222

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

C16.23 FUEL, NAVAL DISTILLATE (F-76) (DLA ENERGY MARCH 2025)

NATIONAL STOCK NUMBER PRODUCT NOMENCLATURE DLA ENERGY PRODUCT CODE

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

For supplies delivered under this contract, the Contractor shall conform to all International, Federal, State, and local environmental requirements applicable to the geographic location of the receiving activity on the date of delivery. The Contractor shall also comply with all applicable International Agreements, Treaties, Conventions, and the like to which the United States is a signatory or with whose terms the receiving activity has otherwise agreed to comply, including but not limited to, the requirements of MARPOL 73/78 Annex VI Regulations 14 and 18. The Contractor shall be responsible for determining the existence of all such requirements prior to the time deliveries are made. 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. In the event that an International, Federal, State, and/or local environmental requirement, as identified above, is more stringent than a requirement contained in this contract, the Contractor shall deliver product(s) that complies with the more stringent requirement.

Product(s) that fails to meet the more stringent requirement will be considered nonconforming supply. Product(s) to be supplied shall fully meet the requirements of the applicable specification(s). In the event that compliance with the more stringent requirement causes the contractor to incur additional costs, the contractor may request an equitable adjustment.

Unless otherwise indicated by the Contractor in writing, prior to award, the product offered shall be required to fully meet all applicable specifications. The supplier shall provide to the receiving vessel a “Statutory Sample” of at least 400 mL in volume, taken from the receiving vessel’s inlet bunker manifold, together with a Bunker Delivery Note (BDN). This sample will be sealed and carry a sample tag that provides the documentation required per MARPOL 73/78, Annex VI Regulation 18.

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) 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).

2) F-76 offered from a location other than where refined (excludes synthesized material as defined in section 3.2.2 and 3.2.3 of MIL- DTL-16884P) requires testing for FAME content by test method ASTM D7963, BS EN 14078, or IP 579. ASTM D7963 is considered to be the referee test method.

3) In Australia, all deliveries of F-76 shall have a minimum Flash Point of 62.5°C at the custody transfer point.

4) Ash, mass%: All batches of F-76 shall not exceed 0.010% Ash by ASTM D482.

c) MATERIALS: 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.

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.

FORT BELVOIR, VIRGINIA 22060-6222

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

d) ADDITIVES:

1) Lubricity Improver Additive (LIA) – Lubricity additives are allowed in F-76. The LIA additive(s) used shall conform to MIL-PRF-

32490A, Performance Specification, Additive, Lubricity Improver, Distillate Fuel, dated 24 May 2019 and found in ASSIST and shall be listed in the electronic Qualified Products List (QPL)-32490, located in the Qualified Products Database (QPD) found at https://assist.dla.mil/ (or http://quicksearch.dla.mil) . Instructions on how to use ASSIST are located in QAP C1.02. Either Grade A, Grade B, or Grade C material is suitable for treatment of desulfurized F-76. Additive concentration shall not exceed the maximum allowable concentration applicable to the specific additive selected for inclusion in finished F-76.

i. For pipeline deliveries only. Most pipelines do not allow the addition of diesel lubricity additives to be shipped via their system; therefore, the following guidelines apply:

For F-76 shipped via pipeline that does not allow LIA, no LIA is to be added to the fuel. Lubricity shall not be a criteria for acceptance in this scenario. Lubricity improver will be injected into the fuel upon receipt.

2) Information pertaining to qualification of additives not currently listed on QPL-32490 may be obtained from Commander, Naval Sea Systems Command, ATTN: SEA 05S, 1333 Isaac Hull Avenue, SE, Stop 5160, Washington Navy Yard, DC 20376-5160, USA, or by e-mailing CommandStandards@navy.mil.

Dyes and Markers - Red dye required in off-highway diesel fuel in accordance with 40 CFR Part 80 as modified by the Environmental Protection Agency's interim final rule published in the Federal Register dated July 14, 1994 shall not be added to F-76. The finished product shall show no visual evidence of red dye. This F-76 product is for military, off-highway use only and must be segregated at all times from any diesel fuel used on-highway. NOTE: Red dye does not apply to Atlantic/Europe/Mediterranean or Western Pacific Overseas Bulk purchase programs unless offering refinery is located in the United States or one of its possessions.

e) ADDITIONAL SAMPLING: The government may request a sample of F-76 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:…