MIL-G-5572 Rev. F

Downloaded from http://www.everyspec.com
tfIL-G-5572F
2-1978
MIL-G-5572E
24 July 1969
MILITARY SPECIFICATION
GASOLINE,AVIATION:
GNADES 80/87, 100/130, 115/1L5
This specificationis approved for use by s1l
Departmentsand Agencies of the Departmentof
Defense.
1.
SCOPE
1.1
~.
This specificationcovers aviation
gasoline for aircraft piston engines.
1.2
Classification. Aviation gasoline shall be
of tbe followinggrades, as specified (see 6.2):
Grade
80/87
100/130
115/145
2.
NATO Code Number
F-12
F-18
F-22
APPLICABLEDOCUMXNTS
2.1
Issues of documents. The followingdocuments,
of the issue in effect on date of invitationfor bids or request
for proposal, form a part of this specificationto the extent
specifiedherein.
SPECIFICATIONS
tlILITARY
MIL-I-25017
-Inhibitor,Corrosion,Fuel Soluble
QUALIFIEDPRODUCTS LISTS
QPL-25017
~
-ProductsQualifiedUnder Military
SpecificationMIL-I-25017,Inhibitor,
Beneficialcomments (recommendations,additions,deletions and
any pertinent data which ❑ay be of use in improvingthis document
should be addressed tn: EngineeringSpecificationsand Standards
Department (Code 9321) Naval Air EngineeringCenter Lakehurst,
New Jersey 08733, by using the self-addressedStandardization
Document ImprovementPropnsal (DD Form 1426) appearingat the
end of this document or by letter.
FSC 9130
Downloaded from http://www.everyspec.com
PfIL-G-5572F
STANDARDS
FSDSRAL
-Lubricants,Liquid Fuels,
and Related Products;Hethods
of Testing
Fed. Test Method Std No. 791
tfILITARY
MIL-STD-105
-San@ing Proceduresand
Tables for Inspectionby
Attributes
iiIL-STD-290
-Packaging,Packing and
Harking of Petroleum and
Related Products
(Copies of specifications,standards,drawings,and publications
requiredby suppliersin connectionwith specificprocurement
fuoctionsshould be obtained from the procuring activity or as
directed by the centratting officer.)
*
Other publications. The followingdocuments
2.2
form a part of this specificationto the extent specified
herein. Unless otherwiseindicated,the issue in effect on
date of invitationior bids or reque%L ffixpr~p=s~l c!.?zII
eppl:,
except for the specificissue acceptedby the Department of
Defense as listed in the current Departmentof Defense Index of
Specificationsand Standards (DODISS) AST?fdocuments listed
by specific date shall form a part of this specificationbut
may not be “listedin the current DODISS.
.4ffmIcANSOCIER FOR T55TING ~
●1
tf.4~IALs (A5TM)
ASTU D86
Distillationof PetroleumProducts,
Test for
ASTM D130
Copper Corrosion from Petroleum Products
by the Copper Strip Tarnish Test,
Detection of
ASTfiD240
Heat of Combustionof Liquid Hydrocarbon Fuels by Bomb Calorimeter,Test
for
ASTM D270
Petroleum and PetroleumProducts,
Sampling
ASTIID287
API Gravity of Crude Petroleum and
Petroleum Products (HydrometerMethod)
Test for
2
I
Downloaded from http://www.everyspec.com
tfIL-G-5572F
ASTtlD323
Vapor Pressure of PetroleumProducts
(Reid Method), Test for
ASTffD381
Existent Gum in Fuels by Jet Evaporation,Test for
ASTM D526-70
Lead in Gasoline,GravimetricMethod,
Test for
ASTM D611
Aniline Point and Hixed Aniline Point
of PetroleumProducts and Hydrocarbon
Solvents,Test for
ASTTID873
Oxidation Stabilityof Aviation Fuels
(PotentialResidue Method), Test for
ASTM D909
Snock Characteristicsof Aviation
Fuels by the SuperchargeMethod, Test
for
ASTM D91O
Aviation Gasolines,Specificationfor
ASTU D936
Aromatic Hydrocarbonsin Olefin-free
Gasolinesby Silica Gel Adsorption,
Test for
Water Reaction of Aviation Fueis, Test
for.
Sulfur in PetroleumProducts (Lamp
tfethod)
, Test for
HydrocarbonTypes in Liquid Petroleum
Products by FluorescentIndicator
Adsorption,Test for
ASTM D2267
Aromatics in Light Napbthas and Aviation
Gasolinesby Gas Chromatography,Test
for
ASTM D2382
Heat of Combustionof Hydrocarbon
Fuels by Bomb Calorimeter(High-Precision
Method), Test for
AST?lD2386
Freezing Point of Aviation Fuels, Test
for
ASTM D2392
Color of Dyed Aviation Gasolines,Test
for
3
Downloaded from http://www.everyspec.com
MIL-G-5572F
ASTM D2551
Vapor Pressureof PetroleumProducts
ASTM D2599
Lead in Gasolineby X-ray Spectrometry,Test
for
ASTM D2622
Sulfur in PetroleumProducts (X-Ray spectrographic Hethod),TesL for
ASTM D2700
Knock Characteristicsof Motor and Aviation
Fuels by the Motor Method, Test for
(Copies of ASTM publicationsmay be obtained from the American
Society for testing and Materials, 1916 Race Street, Philadelphia,
Pennsylvania,19103.)
3
REQUIREMENTS
3.1
Materials. The gasoline shall consist completelyof
hydrocarboncompounds,except as otherwisespecifi.edherein.
3.2
Chemical and physical requirements. The chemical
and physical requirementsof the finishedgasoline shall conform to
those listed in table 1. Requirementscontainedherein are not subject
to correctionsfor test tolerances. If ❑ultiple determinationsare
made, results fallingwithin any specifiedrepeatabilityand reproductabilitytolerancesmay be averaged.
Water reaction. In addition to the interface rating
3.2.1
and volume change requirementsspecifiedin Table 1, the fuel shall
separate sharply from the water layer and there shall be no evidence of
an emulsion or precipitatewithin or upon either 18yer.
*
Additives. The additives listed herein ❑ay be used
3.3
singly or in combina-mounts
not to exceed those specified. ‘The
type and amount of each additive used shall be reported (see 6 .3)
*
Antioxidant. The followinginhibitorsmay be
3.3.1
blended separatelyor in combinationinto the gasoline in total concentration not in excess of 8.4 pounds of inhibitor (active ingredient)Per
1,000 barrels (42 gal.) of fuel (91 reg./gal.)(U.S.), 24 mg.lliter, or
8.4 lb./35,000gal. (U.K.) in order to prevent the formation of gum:
I
4
Downloaded from http://www.everyspec.com
F!IL-G-5572F
*
::
c.
d.
e.
f.
8.
h.
i.
j.
k.
●
1.
N ,N’-diisopropyl-pa
ra-phenylenediamine
N ,N’-disecondarybutyl-para-phenylenediamine
N, secondarybutyl,N’-phenyl ortho-phenylenediamine
2 ,6-ditertiarybucyl-4-methylphenol
2,4-dimethyl-6-tertiary
butylphenol
72 percent min. 2,4-dimethyl-6-tertiary
butylphenol
28 percent max, ❑onomethyl
and dimethyl tertiarybutylphenols
55 percent ❑ in. 2,4-dimethyl-6-tertiary
butylphenol
15 percent ❑ in. 2,6-ditertiaty
butyl-1+-methylphenol
30 percent ❑ax. ❑ ixed monomethyland
dimethyl tertiarybutylphenols
2,6-ditertiarybucylphenol
75 percent min. 2,6-ditertiarybutylphenol
25 percent ❑ ax. mixed tertiary and
ditertiary butylphenols
butylphenol
60 percent ❑ in. 2,fk-ditertiary
40 percent max. ❑ ixed tertiaty butylphenols
butyl-435 percent ❑ in. 2,fi-ditertiary
❑ethylpbenol
65 percent ❑ ax. ❑ ixed
methyl, ethyl, and dimethyl tertiary
butylphenols
55 percent ❑ in. butylatedethyl phenols
45 percent max. butylatedmethyl and
dimethylphenols.
3.3.2
Corrosioninhibitor. A corrosion inhibitorshall
not be added to aviationgasoline by tbe supplieror the transporting
agency unless prior approvalis obtained from the procuring agency.
When used, the corrosioninhibitorshall conform to MIL-1-25017and the
finished fuel shall ❑ eet all the requirementsspecifiedin section 3.
No limit is placed on tbe minimum amount which ❑ ay be added. The maximum allowable concentrationshall not exceed that listed in the latest
revision of QPL-25017. If a corrosioninhibitoris used, the contractor
or transportingactivity,or botb, shall maintain and upon request,make
available to the Government,evidence that the corrosioninhibitorsused
are equal in every respect to the product specifiedin MIL-1-25017.
5
Downloaded from http://www.everyspec.com
MIL-G-5572F
*
Color. Color for each grade shall be within the
3.3.3
minimum and maximum color standards for the applicablecolor when determined by the test ❑ethod indicatedin Table 1. The colors indicated for
each grade of gasoline in Table I shall be obtained by the addition of
dyes in amounts listed in Table 11. Dyes may be dissolved in xylene for
ease of mixing. When a xylene solutionis used, the maximum dye limits
in Table II are to be based on the nonvolatileportion of the dye solution. The quantitiesof dyes indicatedare the total dye content,
includingthat normally in the TSL ❑ ix. No dyes other than the following shall be present in the finished fuel:
a.
Blue - Essentially1, 4-dialkylaminoanthraquinone.
b.
Red - Essentiallyalkyl derivativeof
azobenzene-&-azo
-2-naphthol
Tetraethylleadcontent.The tetraethyllead(TEL)
3.3.4
shall be-added in the form of an antiknock❑ ixture containingnot less
than 61 percent by weight of tetrc,ethyllead
and sufficientethylene
dibromideto provide two bromine atoms per atom of lead. Tbe balance
shall contain no added ingredientsother than a hydrocarbonsolvent, an
approved oxidation inhibitor,and dyes as specifiedherein.
Workmanshi~. The gasoline shall be visually free
3.4
from undissolvedwater, sediment,and fiuspended
matter.
4.
QUALITY ABSU8AXCEPROVISIONS
.
Responsibilityfor inspection. Unless otherwise
fi.1
specifiedin the contract or purchase order, the supplier is responsible
for the performanceof all inspectionrequirementsas specifiedherein.
Except as otherwisespecified in the contractor order, the suppliermay
use his own or any other facilitiessuitable for the performanceof the
inspectionrequirementsspecifiedherein, unless disapprovedby the
Governiyent.The Governmentreservesthe right to perform any of the
inspectionsset forth in the specificationwhere such inspectionsare
deemed necessaryto assure suppliesand services conform to prescribed
requirements.
●1
4.2
Classificationof inspections. The inspectionand
testing of the aviation gasoline shall be classifiedas quality conformance inspection.
*
4.3
Quality conformanceinspectionsample. The quality
conformanceinspectionsample shall consist of samples for tests (4.3.2)
shall
and sample for ●xaminationof filled containers (4.3.3). W@es
be labeled completelywith informationidentifyingthe purpose of the
sample, name of product, specificationnumber, lot number, date of
s~lin8 and contractnumber.
6
I
Downloaded from http://www.everyspec.com
!IIL-G-5572F
*
4.3.1
Lot.
P.lot shall consist of the following:
—
Bulk lot. AU indefinitequantity of a homogeneous
4.3.1.1
—
one type of gasolzne contained in one isolated container;or
❑ anufacturedin a single plant run (not ❑ ore than 24 hours), through the
same processing equipmentwith no change in the ingredientmaterials.
❑ ixture of
*
4.3.1.2
Packaged lot. An indefinitenumber of 55-gallon
drums or smaller unit containersof identicalsize and type offered for
acceptanceand filled from one isolated tank containinga homogeneous
mixture of material.
*
4.3.2
Sample for test. Each bulk lot of materials shall
liesampled for verificationof product quality in accordancewith ASTM
Method D270 and tested as specified in h.5.
*
Sample for inspectionof filled containers. Each
4.3.3
lot of filled containersshall be sampled in accordancewith !fILSTD-105, InspectingLevel 1, AcceptableQuality Level (AQL) 2.5 percent
defective,and inspectedas specified in 4.5.2.2.
*
4.4
Quality cnnfonuanceinspectingtests. The quality
conformanceinspectiontests shall include testing of the sample (4.3.2)
for conformanceto the requirementsof this specification,and an inspection of samples of containers (h.3.3) for confanrance to the packaging,
packing, and ❑arking requirements.
*
4.5
Methods of inspectionand test.
*
4.5.1
Samples for test (4.3.2) shall be tested in accordance with Table I to determineconformancewith 3.2 and samples fnr
inspectionof filled containers (4.3.3)shall be examined in accordance
with 4.5.2 to determine conformancewith 5.1.
*
4.5.2
Inspection. Inspectionshall be in accordancewith
Method 9601 of Federal Test Method Standard No. 791.
*
4.5.2.1
Prior to filling,each empty unit containershall be
visually inspected for cleanlinessand suitability.
*
4.5.2.2
After filling,each unit cnntainershall be visually
inspected for marking, fill, closure, sealing, leakage,and conformance
to MIL-STD-290
5.
PACSAGING
5.1
Packaging,packing, and markins. Packaging,packing, and marking shall be in accordancewith HIL-STD-290.
7
Downloaded from http://www.everyspec.com
M I L - G - 5572F
. 6.
NOTSS
Intendeduse. The gasoline coveredby this specifi6.1
cation is intended for use in aircraftpiston engines.
6.2
Ordering data. Procurementdocuments should specify
the following:
Title,number, and date of this specification
(b) Gradeand NATO Code Number of gasoline
required (see 1.2)
(c) Quantity requiredand size containers
desired.
(d) Levels of packaging and packing required
(see 5.1).
(a)
6.3
Precautionsfor mixing inhibitors. To prevent any
possible reactionbetween the concentratedform of different inhibitors, the fuel supplier is cautionednot to mix inhibitorsprior to
addition to the gasoline.
6.4
Internationalstandardizationagreement. Certain
provisionsof this specificationare the subject of internationalstandardizationagreementNATO STANAG No. 1135 and ASCC AIR STD 15/1. When
amendmtnt,revision, ox cancellationof this specificationis proposed
which will affect or violate the internationalagreementsconcerned,the
preparingactivity will take appropriatereconciliationaction through
international standardizationchannels includingdepartmentalstandardizationoffices, if required.
6.5
Marginal indicia. The ❑argins of this specification
are marked to indicatewhere changes,deletions,or additionsto the
previous issue have been made. This is done as a convenienceonly and
the Governmentassumesno liabilitywhatsoever for any inaccuraciesin
these notations. Figures are not so ❑arked. Bidders and contractors
are cautionedto evaluate the requirementsof this documentbased on the
entire content as written, irrespectiveof the marginal notations and
relationshipto the last previous issue.
Preparing activity:
Navy - AS
Custodians:
Army -tfB
Navy - AS
Air Force 11
(ProjectNo. 9130-0088)
Reviewer activities:
Army - Av, HII,MI
Air Force- 68
DLA - PS
Internationalinterest (see 6.4)
8
●
Downloaded from http://www.everyspec.com
M I L - G - 5572F
6
g:
.
9
Downloaded from http://www.everyspec.com
M I L - G - 5572F
*&
CNUJJ
.: ,4..4
c)
+
~
. ..-..--,>,
>1
. .
l-la?
Downloaded from http://www.everyspec.com
tlIL-G-5572F
W’ASLS II. Dye concentrations.
100 / 130
80/87
SEQUIRFMSNT
BINSDYS
=er
❑g/gal.(U.S.) ‘
mgjge.1.
(U.K.)
lb/1000barrels
MD DYE
~ter
mg/gd. (U.S.)
❑g/gal. (U.K.)
lb/1000 barrels
GSADE
115 / 145
tlin
tlax
Min
Max
----—----
0.131
0.500
0.596
0.046
0.80
3.03
3.64
0.28
0.713
1.51
2.70
5.70
3.24
6.85
0.528 0.250
1.2’4
4.10
5.64
0.435
---
0.502
0.864
-------
1.90
2.28
0.176
3.27
3.93
0.303
1.83
2.29
6.93
8.24
0.642
8.66
10.40
0.802
---
11
—- –
-----
Uin
Max
Downloaded from http://www.everyspec.com
●
DEPARI?4ENT
OF THE NAVY
Naval Air EngineeringCenter
Lakehurst,NJ 08733
PPICIAL
Wswm
hti*CU PAID
Navy Department *
m
DoD-316
u
@OSTAaC
C.
c., ”..,,
●
.0.
P“, VA,,
“s,
mm
EngineeringSpecificationsand Sca”dards Department
Naval Air EngineeringCenter
Lakehurst,NJ
08733
(Code
93)
Downloaded from http://www.everyspec.com
TANDARD I ZAT I ON
INfl’RU,fX’10NS:
q
mmtIu.
DOCUMENT
llhbrmisprovided
I MPROVEMENT
totcdicitb.eficial
●
PROPOSAL
mnmentswhich
~.y
improve
this docunmnta.d
sc
bD-nw.ctim,
covemment nctirities, mnufscturen,
vendom, otother ptmwrn,ve.wmof
thedocument
weinvitad
tos.bmit
comme.U
~thegovernme.1.
Fold onlines onmw=side,
stipleintor.er,
nndcend toptepming
activity.
Attc.ch uIypertinent
damwhichnuybcof
.Sti.
improving thi. doc.me.t.
lf
the= ue~diU.ti
Wm,.tmch
t. fommdpbm
bo&in@n
e"velow
.ddrdto
prepuing.ctiti1y.
A
msponsetil!bemwldd
tothes.bmitter,
whe.nameand*dd--kpt.rided,
-ithi.
aod.ysind,catinq
that
the1426- mc.ived
md whenanyappropnati
aclicm
o“itwill
becompleted.
NOTE ~iformtil notk-dti s.btitmquesk
forwaiwm,
devi*l;om
orcl-ifi-tio.
ofsFXi~tio.
~.ire~n~Onc.wnt_.*~cu.~mmen~subml~~dOnthlSf.rm
dOnOtc..,~tu*.
:implY~utho,izati.n
towsive
anyporli.m
oflhereferenced
document(
s).,
toamendcontrmct.d requirements.
CUMENT
IOENTIGIE.
(N..nti.)
AND
TITLE
MIL-G-5572F GASOLINC, AVIATION:GRADES 80/87, 100/130, 115/145
ME OF ORGANIZbTlON
I
AND
ADDIIES3
OF SUBMITTER
❑ USER
vENDOR
❑ MANUFACTURER
HAS ANYP&. TOFT"EOOCUMENT
CREATED
PR08LEMS
c
E7
0tSANYPAn70F
A.
G, VEVb
RAG RA?H
B,
RECOMMENCE
C.
REASON
FOR
tT700n,G10,
NUMBER
D WORDING
RECOMMENDED
RESTRlcTl.E,
ORBEOU!UED
L00SE0RAM6lGu0u37
lNIERPRETATlON
4NOWOFIDING
CHANGE
CHANGEISI
D B“ ,tin,,.ior
,y.,d
Mm, md.ddm”-OPtie”sJ,
BMITI%
TELEPHONENO.
DATE
1,:-.1426
tNPROC"REMEN7
pLEASEEXPLS4NBELOW
EOITI ON OF *
JAN72w1LL
BE USED UNTIL EXIIAUSTED.
I