an834 rev9

NOTICE OF INCH-POUNDCANCELLATION

AN834 REV 9NOTICE 122 April 1999

AIR FORCE/NAVY AERONAUTICAL STANDARD

TEE, BULKHEAD AND UNIVERSAL FLARED TUBE

AN834 REV 9, dated 4 August 1983, is hereby cancelled. Future acquisitions for this itemshould refer to Society of Automotive Engineers (SAE) Aerospace Standard (AS) AS1039,"Tee, Standard and Reducer, Bulkhead on Side, Flared Tube."

Table 1 provides a detailed cross-reference of cancelled AN834 Part or IdentifyingNumbers (PINs) and replacement AS1039 PINs. The use of "AS" parts is preferable, but "AN"parts may be used for a period of three years from the date of this notice to deplete existingstock. Users are cautioned to evaluate replacements for their particular application.

(DoD activities may obtain copies of SAE AS1039 from the DoDSSP, StandardizationDocument Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094. Theprivate sector and other Government agencies may purchase copies from the Society ofAutomotive Engineers International, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)

Custodians: Preparing activity: Army - AV DLA - CC Navy - AS Air Force – 99

DLA - CC (Project 4730-0419)

Review activity: Air Force - 82

1 of 3AMSC N/A FSC 4730DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

AN834 REV 9NOTICE 1

2

TABLE 1 - Cross-Reference Data

Cancelled Tube Replacement Cancelled Tube ReplacementAN PIN Size AS PIN AN PIN Size AS PIN

AN834-2 .125 AS1039-020202 AN834-8 .500 AS1039-080808AN834-2D .125 AS1039D020202 AN834-8D .500 AS1039D080808AN834-2J .125 AS1039J020202 AN834-8J .500 AS1039J080808AN834-2K .125 AS1039K020202 AN834-8K .500 AS1039K080808AN834-2S .125 AS1039S020202 AN834-8S .500 AS1039S080808AN834-2T .125 AS1039T020202 AN834-8T .500 AS1039T080808AN834-2W .125 AS1039W020202 AN834-8W .500 AS1039W080808



AN834-5 .312 AS1039-050505 AN834-16 1.000 AS1039-161616AN834-5D .312 AS1039D050505 AN834-16D 1.000 AS1039D161616AN834-5J .312 AS1039J050505 AN834-16J 1.000 AS1039J161616AN834-5K .312 AS1039K050505 AN834-16K 1.000 AS1039K161616AN834-5S .312 AS1039S050505 AN834-16S 1.000 AS1039S161616AN834-5T .312 AS1039T050505 AN834-16T 1.000 AS1039T161616AN834-5W .312 AS1039W050505 AN834-16W 1.000 AS1039W161616

AN834-6 .375 AS1039-060606 AN834-20 1.250 AS1039-202020AN834-6D .375 AS1039D060606 AN834-20D 1.250 AS1039D202020AN834-6J .375 AS1039J060606 AN834-20J 1.250 AS1039J202020AN834-6K .375 AS1039K060606 AN834-20K 1.250 AS1039K202020AN834-6S .375 AS1039S060606 AN834-20S 1.250 AS1039S202020AN834-6T .375 AS1039T060606 AN834-20T 1.250 AS1039T202020AN834-6W .375 AS1039W060606 AN834-20W 1.250 AS1039W202020

AN834 REV 9NOTICE 1

3

TABLE 1 - Cross-Reference Data (Continued)

Cancelled Tube Replacement Cancelled Tube ReplacementAN PIN Size AS PIN AN PIN Size AS PIN

AN834-24 1.500 AS1039-242424 AN834-32 2.000 AS1039-323232AN834-24D 1.500 AS1039D242424 AN834-32D 2.000 AS1039D323232AN834-24J 1.500 AS1039J242424 AN834-32J 2.000 AS1039J323232AN834-24K 1.500 AS1039K242424 AN834-32K 2.000 AS1039K323232AN834-24S 1.500 AS1039S242424 AN834-32S 2.000 AS1039S323232AN834-24T 1.500 AS1039T242424 AN834-32T 2.000 AS1039T323232AN834-24W 1.500 AS1039W242424 AN834-32W 2.000 AS1039W323232

AN834-28 1.750 Not availableAN834-28D 1.750 Not availableAN834-28J 1.750 Not availableAN834-28K 1.750 Not availableAN834-28S 1.750 Not availableAN834-28T 1.750 Not availableAN834-28W 1.750 Not available

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141L-F-5509D

I

Fx’rrnaGs, TUBE , CONNECTION

~Ag +=~ggf-aeim LB ●?proved for use by ●ll Depart-ments and Agencies of the Department of Defeme.

* 2.1 The follmnlng documents , of the issue Ln ●ffect on data ofinvitation for bids or request for proQosal, form a pare of thisspecification to the extent specified nerein.

, SPECIFICATIONS

Federal

P-c-437 Cleaning Compound, High Prasaure(Stum) Cluaaer

NN-P-530 Plyycmd, Flae PanelqQ.~-~~~//& AhmLmm Alloy Bar, Rod, Wire And

Special Shapes; Rolled, Drawn, OrCold Finished, 2014

Q@A-225;6 ~l-~mwiil AllGy Bar, RGc!,!md.wire;R#ed, Drwn, Or Cold Finished,

QQ-A-225/9 Al~num Aiioy Bar, Rod, iiire,AndSp=cial shapes; R=ll:d, Drawn! orCald Finished. 70?5

QQ-A-367 Alminum Alloy Forgings

I

KIL-F-5509D

,

I

Fdaral (Concinuad)

~-B-626

QQ-B-7213

QQ-P-35

QQ-P-416

QQ-S-637

QQ-Z?-763

PPP-B-566PPP-B-S135IJPP-B-591PPP-B-601PPP-B-621PPP-B-636PPP-B-665

ppp.B-676PPP-C-96

KiLitary

MU-P-X16?UL-P-130

?fXL-S-5002

KIL-T-5066

HIL-H-5440

tuL”F’-55l8

MIL-S-5626

MIL-H-6083

Braas, Ledad And tionleaded: Rod,Sh es, Forgin s,

x &And Flat Productn

vi Finished as (Bar And Strip)Bronze t4en aneoe; Rod, Shapea,

ng kdinatmucts(mtFOrgi s,Wire, trip, Sheet, Bar, And Plate)Pa88ivation Treatments For CorrosionResisting SteelPlacing, Catium (zlectro-&posit*d)Steel Bar, Carbon. Cold Finished(B&uiii6srd@ieuky, F*W Ua4Ma&lag)‘$teak Mru, w=, $5hapW. he!Forgings, Co=od.on-RasistingBoxes, Foldlag. PaperboardBoxes, Wood, Wirebomndhxe~, Fiberboard, Wood-CLeatedBoxes , Wood, Cleated-PlproodBoxes, Wood, Nailed And Lock-CornerBoxes, Shipping, Fiba=boardBoxes, Paperboard, MeCal Stayed(Including Stay Matarial)Boxes, Set-Up, PaperbearciCans , Metal , 28 Gauge!And Lighter

Prsaenacion-Packagin$, Methods OfPaper, Wrspping, Laminated And

CrapdSurface Treataants And InorganicCoatings For ?letal Surface8 OfWeapons SystemsTubing, Carbon Steel (1025), Seam-less And Welded (Aircraft Quality)Hydraulic Systems, Aircraft, TypesI And 11, Design And InstallationRaquirwntm ForPneumatic Systums, Aircraft; Design,Installation, And Data ReauiremencsForSteel: Chrome Molybdenum (4140)Bars, Rods, And Forging Stock (ForAircraft Applications)Hydraulic Fluid, Petroleum Base,For Presemation And OperaclonHeat Trcatmsmc Of Aluz&num AlloysTubing, Chrome-Molybdenum, 4130Steel, Seamless. And U-l&d, AircraftQuality

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MIL-P-5509D

Military (Continued)

!%n-s-6n 8,. ---- .—-

FUL-H-66?5

. KZL-P-7105.

W-A-8625uT.

Mm-s -88?9

MIL-L-10547

MIL-B-I3239

STANDARDS

Federal

MIL-.STD-129MIL-STD-889KS24385

MS24386

MS33649

MS33656

MS33657

!4s2365!3

~~~~me_Mnlvh&ara~rn ( b ~~~t )steel , .. ”-,”

Bars And Reforging Stock (Alrcra~tQuallty )Heat Treatment Or %eeis (AcYospacePractice, Process For)Pipe Threads, Taper, AeronauticalNational Form, Symbol ANTT, GeneralRequirements Por~q~~~ Ceat:fi~ , F~~ Al !xmfnllm ~-~~-—. .—

Alwnlnum AlloysScrew ThZ’Wads, Controlled RadiusRt5Ut‘i*itF]Il%C-tiaSetl!M~GY l!f.a.?.?t~?:General SpecL~lcation ForUners , Case , And Shtet, Overurap ;Water-Vaporproor Or Waterproof,FleAableBarrier Material, waterproofed jFlexible, All Temperatu~es , HeatSealablem.*.-bcq.+=.* ~~=ppifig, ~~e~c=~~y Ne~trQ~(?Jon_Corroslve)

SteeL: chemical Composltlon AndHardenabllltyMetals ; Test Methods

Sampling Procedures And Ta51e5 ForInspect Ion By AtrrlbutesMarking For Shipment And StoYageDisshLIlar Metals!94+64r4b~*7i~ ‘U-Id,

~~=y~~ ~~~ vnnnortl OR,-- .,------

Preclslon Type, Standard DimensionsFitting End, Bulkheat Flared TubeConnection , Precision Type,cJ~&q~~~~ ~~m~~~~~~~Bosses , FluLd Connection-InternalStraight ThreadFitting End, Standard DimensionsFor Fla~~ Tube Connection AneGasket SealFlttlng End, Standard Dimensions ForBulkhead Flared Tube ConnectionFitting End, HQSJeConnection,Standard Dimensions ?or

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Military (Continued)

.. .. .. . . . ... .. .. . .

MIL-F-5509D

JI!s33677 Fitting End: Taper Pipe Thread,Standard Dimensions For

(Copies of Specifications, standards, drawings, and publicationsrequ%md by BugwZlfif%I %ri mifiec!tlon with $pe~lflc procurement~lmctiQr&e ~he~d be Qhgaingd .fronpmcurzng acti.tity or asdirected by the uOntPaCthU offioer. )

Q 2.2 Other vubllcatlons . Th* rollowlng documents form a part ofthis specif LC8tiOn to the extent specified herein. Unless other-wise indicated, the issue in ●ffect on date of lntitatlon rOrblcis or request for proposai shall apply.

UNIFORM CLASSIFICATION COMMITTEE

Unirorm Freight Cia@ai~icat.ioriKtias

(Application for copies should be addressed to the UnlfoxmClassification Committee, Room li06, 222 South Rive=ide PiazajChicago IL 60606.)

AMERICAN NATIONAL STANDARDS INSTITUTE, INC.

fluTT y!e,~..---- SUTfSCe Texture - .Sur~ace RQU.@-neas , Waviness, and Lay

(Copies of the above publication maY be obtained from the AmericanN&tiCR=l St&Qd&ZdB ~fi~titutet Xnc.3 1430 ~roa9uaY; New York NY10018. )

SOCIETY OF AUTOMOT~ ENGINEERS, rNC.

A.MS2241 Toleranoee, Corrosion And HeatReslst8nt Steel Bars And ~ire Andy*~~A~.w~,#J*,~w+● m-+ lvm Al 1 ~lj ~=~-.&.-**-.$ .-.*-

And WireAMS 2486 Conversion Coating of Titanium

Alloys, Fluoride ?hosphase TypeAMS 4928 Tit=.i~ AIIoY BaF8 And Forgings,

6AL-L!v, Annealed, 120,000 ?S1 (82?MPa) Yield

(~q)~~s of ~& above publications Day tJpobt~inecl from the Soclet:Jof Automotive Engineers, IrIc., 400 Commonwealth Drive, WarrendalePA 15096.)

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MIL-F-5509D

3. REQUXR2JWNTS

3.i Wteriai. Fittings shali be fabricated of materiais iisteciin Table 1, as opecifled on the applicable drawings.

3.1.1 3teel. All steel shall be made by the basic oxygen openhearth ~ectric furnace procoss.

3.1.2 Heat treatment.

iiiiin”- uIGY iit~in~rn Wti nuts StaCllbs a~p~o nd tmper as ahm ~n TabL@ Zz. WINRnfitting material 18 purchaaed in other than the final temper, thedesired tcmr 18 ●ttal!aed by aging the starting temper as shownin Table 11 ●t the specified temperature for the prescr~bed time.Eaoww far a@a6 t- =d t-m-t-, PrOCeSE c~trol •ha~z be inaccordance with KIL-H-6088.

3.1.2.2 Steel. When required, steel shall be heat treated inaccordan=~h UIL41-0875.

N 3.1.4 Unless otherwise speclfled on theha~e~~ Qf &he f~~~~h~d ~afiQ~ steel

shall be Rockwell B-92 to C-31. POrcarbon steel fittings below a hardness of Rockwell C-2C, harclnesszeste EiiaU be iiisGew-iriigc?m Reek’well i?scale, irlB-hicb G=*= the----

hardness shall be within the ranproperties of copper-baee alloy

feFgnB-92 to B-99. Physicalge shall be govermed by the

properties of the material es received. Titanium aiioy pares~h=~l ~~ f’re~of o~g~fi ~~r~c~~d SUrfBCeS,

3.1.5 Except when Speclflcally allowed on the applicabledrawings, no castings of any type shall be used.

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HIL-?-S509D

~/ With bronze forgings, a soft tamper will be permitted inthe finished Pam..

2/ These alloys shall conform to FED-STD-66.~/ ;::m;y2;:: bars 9hall be colr! ?Inlshed with tolerances

Material Starting Time T’eraperature ~l~a~temper (hrs) (Opl tempe?

W -A-2?5/4 (201U) 2 340 360 TbOQ-A-367 (2014)’ T4 8 ;: 12 340 ;; 360 T~oQ-s-225/6 (2024) T42 16 to 20 370 to 38o ?622Q-A-225Y6 (202~! T351 12 to 142S-A-22;>/9 (7’375) ----

370 to 380 T9; 1.-—---- ---------- m-n.,,*

3.2 DeslFn a:ldd~menslons. The design and dimensions of thefitt:ngs s!lal: be In accordance with the applicable clrawlngs. Thebosses mod tube and hose ends of rlttlngs shal: be in accordancewith “!32L385, :.1s24366,MS336U9,NS33656, MS33657, MS33658, orr.1s33Cy7, as applicable. Dimensional requirements are applicableafter ~leaL trea~ment and protective ?inlshing.

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3.2.1shallheavymeam

MIL-F-5509D

Shape and form restrictions. K~rupt reductions of seetl~b:be avoided. Small external secttons adjoining relativelybody sections shall be Shaded Into the heavier secticns byof ample fillets. Sharp corners or Inadequate fillets,

excessive tidercuts, or ●xcessive grooves at the junction Or suchsmall secthns Kith large seszl.ons of Citti.ngs shall be consideredcause for mtJectlon. Unless othez%tise specified, drawing toler-ances shall>apply to fillet and comer radii.

3.2.2 Passages.

;2s:; i%hww” On straight flttlngs where the fluidrom eaeh end, the Ofrset between the drlllec?

holes at the =etlng point of the drills shall nOt exceed 0.015inch. It shall be possible to pass through the fluid Fassage aball whose diameter Is 0.020 less then the ndn~mum diameter specl-f’ied for the paaeage. This does not man that the tirllledpassagemay be smaller than that requi=d by the detail CWawlngs.

3.2.2.2 On angle fittings, the cross-sectional area at thejunction of the fluid passages shall be not smaller than thecross-sectional area of the smaller passage.

3.2.2.3 Wall thlekness. Except as otherwise specl?lecl, the wallthickness at any point on the Fitting shall be not less than thethickneSs established by the dimensions and tolerances for theInside and outside diameters end ecceritrlcit~es spec~?led :rl zheapp~cable tirawlngs.

3.2.3 Threads. Pipe threeds shall conform to MIL-P-7105.Straight threads shall be of Unlrled form and shall conf’orm toMIL-s-0879, except as specified herein. Threads may be cut,ground, or rolled.

3,2,3.1 External threads (if rolled). The grain fiOWs in roiledthreads Shall be continuous and shall ~OllOW the general threadcontour, with the maximum density at the threat! TOOt as showr, orF’lgure I. Laps and seams, whose depths are wlthlri the lir,lts or

Table 111, are acceptable on the crest, and the nonpressure tt,reaiflank above the pitch diameter. Laps and seams are not acceptableon any part or the pre6sure thread flank, in the thread root , oron the nonpressu~ thread flank ●xtending from above to below zhepitch diameter. Stress cracks are unacceptable.

3.3 Flnlsh.

3.3.1 Aluminum alloY fittin.zs. Aluminum alloy Pittlngs, slee”~es,and nuts shall be anodized in accordance with !41Z-A-?625, Type ::,Class 2. Duplex seallng with a sodium bichromate solution toenhance cor?oslon resistance may be speclfled on Zhe applicatl?drawings.

3.3.1.1 Surface condition. The surface of aluminum alloy parts,after anodic and bichromate treatment, shall be free ??~m Fits and ‘d~scontlnultles such as scratzhes or breaks, and shall br unl~cmIn appearance. Discoloration will not be cause ?OT ?e.je:?i~r.

Page ? of 17

T -, ; -.;,,,-,+ >,.L-A d= -----”Q.”= ., ---- --- ---

MIL-F-5509D

Depth of Laps, Seams, Surface Irregularities,and Dlscontinui~ie6 in Roiled Threads

F’ittlng Size 1 bDth (i.nah ) (-~1 i1

,

I!

e .006.006 I.007.007.008 I.009.010

1I

3. 3.2 C?ir%on steel fltth~ Carbon steel fittings sleeves, andnu%s~ shall be cadmium plate~ In accordance with QQ-$-416, TypeII> Class ~. All carbon steei fYttings, rItits&?S s~=eves spa~l be.. ...-.—,-- .- UTT-UAfiR 2.

5teel flttlnt3s, nuts, ma ~A==VC=I ~IA--- -- -— ----MTT ~-5002,acco~danee .wltP...-fiti Passlvarlon shall be per QQ-p-35,

Type I.

3.3.U cm>er-kase allov flttlncs . PlatLr.g or copper-base alloyilt;~ags is 2ccQrdWce with CIQ-P-416, Type II, Class 3 isoptional. Speclflc ClnLsh requirements ror this mate~iul Ghan $eas speclrled bY the procuring activity (see S.21.

● 3.3.5 Titanium alloy Slttinus. ~jt~~~ alloy r~tt~ngs and nuts

shall be luorlde phosphate coated per AMS 2486.

Page B of 17

Andrew Colgin

Typewriter

MIL-F-5509, MAT/FIN Al ALLOY: ANOD, MIL-A-8625, II/2 CARB STL: CAD II/2 CRES: PASS Cu ALLOYs: CAD II/3 Ti ALLOY: FLUO-PHOS COAT

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PIIL-F-5509D

3“. . Ident$$i cation of Droduct. All fittings, nuts, and sleevesshal.~ bt marked in accordance with the following instructions.The marking Unaii be applied in a iocation not detrimental to thef~~~~fig ~q~ ~p.=~~~=~ ~~ AmFd-m+81 ~~ ~~~ ~Qrr~s~oR p~@~~c~~oR“. ..-.-.....#--

of the fitting. . .—-.. -. .. . . —— —-

3.41.I Ah’m KS s;vibcl, ~=... ..U... -.--.—.-.M9”,,P~**,m9w~~ +**A*m-*. unless L?t!2er-Uise Specifi d all flttinge and nuts shall be marked with thelettem AN o; ~ and the manufact-r’s ldentLfic8thn Qr trade-mark . shaves must be tradamrkod. Letken AN or ES on nkeve.are optional.

3.4.2 Material identification. Corrosion-res$Stant steel fit-tings, nut6, end sleeves shafi be marked with the ietter “Jn if-.A. P>-mm ~~k, “..*+k9 ~e~$ey n~m ~~ rn~~e ?~m t?l~s---- .rre= v--- . . -- -- ~~~j Qr

the letter “Sw if mde from Class 347 corrosion-resistant steel.All 70W-T73 eLwsimaa alloy pertx!shall be markefl with the letterau.- The letter “D” on all other alufiitnumaIley parts 1sO~tiOF.El. ~~~ t~t~~,~ mllnv par~~---., -h~~l be m!lrked with the%----letter “T.”

3.U.3 MarkLnu for Part number 61zc. A niuwrical equivalent tothe dash n-er indicating size is optional. All f%ttings andnuts larger than 3/8-inch tube size (except AN929) shall be markedwith the part nuaber, exclusive of size. AN929 fitting% may have~.ha=patu~=:p-~~ &J~~g. ?4=rki.ngor part number on sleeves isoptional.

3 .4.4 Size. .method and location of wl=kinq. WIaiiking sJhallbeaccourpfished .by embossing or Impression stamping on the f’lttlng,nut, or sleeve In a location not detrimental to the part or itscorrosion protection. When items cannot be physically markedbecause of lack of spaoe or beoauae marking would have a delete-rious e~fect) the data specified herein shall be marked on theuonta-lner In addition to the identification marking informationrequired bY MYL-S~-1~~.

3.4.5 Color ldentlficatlon. In addltlon to :he markings specl-fled In 3.4.1 3.U.2 3.~.j , aqd 3.4.4, the AN and MS ?It::ngs,nuts, and ale~ves sh;ll be ldentlfled by the ~cllw%n~ colors :

AI UI!WIUJI! alloy 2014 and 2024 -7075 -

Stee 1Copper-base alloys

Corrosion-resistant steei -Z’%t8ni)UF.&llOy

3,5 WeiRht.values on the

BlueBrownBlackNaturll cadmium plate, ifapplicableNoneCvav (re~g~~ of’ f’lgo?i~e-. -.?phosphate COatlng)

The maximum weight of ~ittings snail net exceed theapplicable drawings.

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c- ue..=.Gdu.-=------ ,--- -../.<,

Andrew Colgin

Typewriter

MIL-F-5509, MAT IDENT J 304cres K 316cres S 347cres W 7075-T73 Al alloy D ALL OTHER Al alloys T Ti alloys

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MIL-F-5509D

3.6 Workmanship.s,.,1~”

Mad32n: SU22$SCSS of $lttin~$ slee~s, ad nutscm burrs end longitudinal or spiral tool marks.

Unless a finer flnlsh is specified on applicable arawinm, seglicgsurfaces shall be smooth, except that Sii~~-tilZTtCO1 =ErkS IUPtQ LOQmlcroinchcs arithmetical average (AA), as defined In A~SI BQ6.1,~i~~ bs =CC=~tSbl!?* AU other machined surfaces shall not exceedL25 AA. Unmachlned surfaoes, ●uch os forgZng surfaces and barstook flats, shall be f~e from blisters, fins, folds, seams,laps, cracks, ees~gationfi, :Pw are=-*~ or other defects whichwould adversely affect their 5erviceablllty, and except forforging partlq lines shall not exceed 250 U. Surface Oefectsmay be explored ~d i) thTJY Ctiibs =mw#eC se EMy do not appearon reatehing a?ncl%Ee reqtired section thlokness can be malntaln-~& they !ehall not be cause for rejection.

4. QUALITY ASSURANCE PROV19XONS

14.1 Responsibility for lnsvection. Unlesis.etiie=Lse s?ect?iedin the contract ox’purchase order, the supplier 1s responsible forthe performance of all inspection mqulrements as specifiedherein. Except as otherwlae specifl~~h~~ the contract or or~er,the suppller may uae his cwn cm =ny ...... ~ac3.M.tZes suitable forthe perferm~nse or the .Lnepectlon requirements speclfled herein,unleme disapproved by the Government. ‘I’heGovernment reserves theright to perform any of the ln~pect”ions &et foirthIz ztiespeci.f’l-catior. where such inspections are deemed necessam to assure~Uvw_=a ~q~ serflces conform to prescribed reuulrements .-....--14m

4,’2 sasmllnq.

4.2.1 9amP 11ng for nondestruc tive tests. Sampllng ror material,threads, rinish, weight, dimensions, marking, surface defects,durability of finish, #d g~pk~~=~h~p sh=~~ be &~ ran&on ~naccC3rd&ica =i~h F!IL-STD-105$ Inspection Level S-3 with an AQL ofJJ.@percent: unless OtheWlst specified in ANA Bulletin No. ~3i.

● 11.2.2 s amulbuz ror destructive tests. Sampling for tensilestrength (4.4.2) internal strain of’copper-base allOys (4.4.3),and eXPSZISLOn te~t Of carbon Steel sleeves (4,4.4} shall .be peF-rormed in accordance with MXL-S~-105, Inspeetlcn M’:el S-3, ~~tk’an AQL of 4.0 percent. Sampling roy oxygen enriched surfaces(4.4.6) shall be performed Ln accorclamce with MIL-STD-105,Inspection Level S-1, with an AQL of ti.Opercent.

ii.z.~ Lcit. A lot shsll c~nslst of all the rlttings of a givenp~rt n=r, made from the same batch of material, and submittedfor Lnspectlon at the same time.

4..2.!4?lgteria> eertl~lcatlon. Records of chemical composition,analysis and mechanical property tests showing confomn8.nce KO thematerial requirements or this speclf~cation shall be availrible tothe Government Inspection fo? each let of fittings.

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?JIIL-F-55c9D

4.3 Exarnlnatlon of product. All fittings shall be ca~fullYexamined visually to tietermine conformance to the Requirements ~orworkmanship, flnlsh, marking, and surface defects (see 3.2.3, 3.3,3.JI, 3.4.1, 3.4.28 3.4.3, and 3.6).

4.3.1 &eight , threadu , finish md 3imensions. The fittings shallbe checked for conformance to this specification and che appli-cable drawing with respect to weight, threads, rinlsh, and dlmen-sion3 . ClaS81rlcation or derects 19 cierlned in ANA Bulletln No.431.

k.ti T8StS.

Jl,h.1 Weltit and diswnsions. Conformance of the fittings to theweight ~d dimensional n?quirements of.the %ppllcable drawingshall be determined by any suitable method.

4.4.2 Tensile strenmh of steel flttinus. Unles~ othemlsesuecified on the aDPlicable tirawings, the tensile strength of8teel rlttlngs shaii be detemined-by hardness tests of the fit-tings . Rockwell hardness readings shall be taken on a smooth flatSurrace of anY unthreaded portion o? the ?Itting f’romwhich thePlatlng has been removed. I=lardriess-tens21eStrengz> relatlonsb.ipsare speclfled in FED-STD-151.

4.4.3 Internal 6crain of copper-base alloys. Fittings Fabricatedfrom copper-base alloys, as specified herein , shall be immersed inan aqueeus solut~c~ zczcaifi:?.glCCJ-Fzc= c? ze?c’~?suz zi~=tc L-ai13 millicers nitric acid (sp.gr. 1.E3) per liter. A~ter ISminutes , the specimen shall be removed and examinec! !’orcracks.Any evidence of cracks :nclicates lnternai stra:n and sh~ll because for rejection.

4.4.U Expansion test of sarbor.steel sleeves. Sleeves shall beselectetl as required by 4.2 and submitted to an expansion test.The test shall be performed with a tapered arbor and a holdtngdevice - shown in Figure 2. The arbor shali be loaded asrequired by the values given in Table ~. The head 0: the sleeve.?hallbe expanded by the load applied through the tapered arbo?.‘-e maximum expansion of the outside diameter Shall be measuredwlbh the load applied. This measurement shall be taken In atle=t two places 90 degrees apart on the diameter. Th:5 averagemeasurement shall be recorded and compared with the mino~ diameteror the threads of the nut (AN818!. ‘T’he ave?age expanded diametershall not exceed the minimum minor diameter of the threads. ~~~test 1s In addition to end does not supplazt the required dlmen-aional inspection of carbon steel sleeves, which shail beconducted prior to the expansion test.

4,4.5 DUrablllty of flnlsh. Dyed ?Ittlngs shall w:tk.stanti!.--erslon in a cleaning solutim containing 5 to 5 ounces c? 2:-.-aner con~orm.ing ~o P-C-43 per gallon or solut:on at a tempera-.zre Of 160 to 170 Fahrenheit (F’)?or 5 minutes. me colorshall not ?ub off when wiped llghtly wl:h a clean cloc.h.

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MIL-P-5509D -1

4.4.6 Oxyize n enriehed surfaces on tltanlum fittings - ~~~1~

alloy parts with unmachlned hex, round, or forged surfaces shallbe selected as required by 4.2; samples shall be sectioned,mounted, polished, Bul%ablY ●tched, ad ●x~ned at 100X ma=lr~-aation fer evldenoe of oxygen enriched siirfaces.

TAB&E 277

Load Values for Standard MS20819Equivalent Cation Steel Sleeves

v91ze - Load in Pounds (D1us or dnw 10 pounds )

1,?OQ -8 4,200 -2 II 15,350:~ 2, 20Q - N 4,100 -28 16,950

1,950 -12 7,400 -32-5

18,7001,950 -16 8,400

-6 2,050 -20 11,?00

4.5 Rejection and retest. Rejected lots shall be resubmitted forretest and acceptance in accordance with MIL-STD-105. Those flt-tlngs subJected to individual ●xaminatlan other than teete (see4.3) and ~a~l~ng to meet the requirements shal~ be rejected.CoppeT-base alloy flttlngs that have been mubJected to the lncer-nal strain test (4.4.3) and steel rlttlngs which have been sub-jected to the hardness test (&.&.2) anali be discarded, whethe~they pass the test or not.

4.6 Packaglnu inspection. Preservation-packaging, packing andcontainer marung De examined for conformance to Section 5,Sampllng shall be performed in uccordanoe with MIL-STD-105,Inspection Level S-3, with an AU of 4.0 percent. Classl~lcatlonof ~efects shall be-is shown In Table V.

● TABLE V

Exterior and interior Kissing, incomect, incomplete,markings illegible, of Improper size, location,

sequence . or method of RVplicntion

Any nonconforming component; componentor otherwise defective

Workmanship I Inadetauate assembly of components4

Exterior and lnterlor Number per container 1s more or less Iweight or content then stipulated; gross or net weight

exceeds the requirement

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P41L-F-5509D

Arborsliita.Fm7For size1/8 through 2 Inches WI

8:

wt;:3+8:

\Optional to 9ultDmalgn 0? Equipment

~Varying S:rienPer Chart

Dimensions In Inches

A c“Size I +.003

IBDIA

-.000 KTN MIr’1

I I DIA I II

I

Figure 20 Fixture for Testing Sleeves

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.—. .- .J .. ,.=r a...=.., . ==:.>:=-& .- -— A----------- > - -. .,-- .- e-.

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* 5. PACKAGING

‘ 5.1 Preservation-packaging shall belevel A or

# 5.1.i Level A.

● 5.1.1.1 Plttinzs unit eontelnere. All fittings , except nuts ,sleeves, and caps, shall be unit packaged in accordance withF4ethod XC-1 of MIL-P-116, except as modl fied herein. The quantityper tit paakage nhall be one. After bagging, rlttlngs greaterthan 3-1/2 inches in anY dimension shall be lncllvldually over-packed in cartons conforming to PPP-B-566, p?p-B-636, ppp-B-665,or PPP-B-676. If it Lm neoemaazy to wrap the fittings prior toinserting in bar top=mnt ~, rittin~Ns;~~l~pw;$~%~dwith barrier ma erlals ~8TIfo~g to UIL-P- --,

● 5.~. l.l.l Altesnete Unit vrotectlon. Five fittings of one typeand size, up to and incl uding 1-1/2 inches In any dlmenslon, shallbe packaged In perforated tear-apart cartons in accordance withMethod III of HIL-P-116. Each carton shall have Interior separa-tions capable of Supporting and aeparatlng each lndlvldual flttlngIn such a manner as to prevent movement Or contact of the rit’tlngswith each other. All surfaces of the carton cornlng in directcontact with the item shall be coated w;tl? z neutral bm~lercapable of Wlthstencllng $Ugtit abrasion. Fittings over 1-1/2inches Sriall be ;z:kaze~ :.n~~”.~.tiwily 1= ~~e:r~~qee ~l:b C 7 ~.1,----

s 5 .1.1.2 ~lt’t~ngg intermediate containers , IJnltpackages Shall bepackaged In intenaediate containers conforming to ?P?-B-566 ,Ppp-B-6 36. pppI-&661j, or ppp-B_676. The quantity of unit packagesper int; ~diate container shall be as speclfled In Table VI,except that intermediate containers am not requl=d for flttlngsIndlvldually packed In unit cartons In accordance with 5.1.1.>.

TABLE VI

Quantity of PackagesQuantity Or Unit Quantity ef Tear-ApartPuckagea per Cartons per IntennedlateIntenmedlate Container

Size (Inches) Centsinerthrough 4 100 Z@

5/16 through 1/2 25 105/8 through 1 10 51-lIJI through 3-1/2 5 1

● 5.1.1.3 Nuts . sleeves . and caps unit containers. Nuts , sleeves ,and caps of one type end size shall be unit packaged in accordancewith Method XC-1 of tvfIL-P-116, or in friction-top hermeticallysealed cans conforming to PPP-c-96. The quantity per unit con-tainer shall be = speclrled In Table VII.

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* 5. 1.3 Preservative mmlicatlon. No preservative compound shallbe applled to the fittings, except that cadJBIUm plated steel partsmhall be dipped in 011 as specified in 3.3.2.

● ~~e ~%&A Before packaging, all parts shall be free from, or any other roreign matter except as noted In

5.1.3.

● 5.2 Pack%nc. Packing shall be level A, B, or C, as specl~led(see ~

containers , inio~ar as possibie, s“naii contain the S~e number 0?articles , shall be Unirorm In shape and size end snugly packed,shall be of minimum cube and tare consistent with the protectionxwqulred, and shall contain Identical Qu~tltle3. The crosswei@ t ~~ ~Lh:fully packsd extericr s?.lpping cen.t=iner shell netexceed approximately 200 pounds, except fiberboard concalners,which shall not exceed the weight llmltatlons of the applicablecontainer specification. Plywood, when used, shall be type I orII, class 2, or NN-P-530. Strapping and closures shall be inaccordance with the appendix to the applicable container specifi-cation. Containers conforming to PPP-B-585 or PPP-B-621 shall beprovided with a case Mner confomlrtg to HIL-L-1054?, except thatmaterial shall con~orm to MIL-B-13239, and shall be sealed inaccordance with the appendix to MIL-L-105~7. No case llner 1s-quired when material conforming to class 2 of ?PP-B-536 1s usedM m intsrmedizte conttirler.

5.2.2 Level B. Fittings packaged as specified herein shall bepacked ~stic-type shipping containers conrormlng to P?p-B-595, PPP-B-591, PPP-B-601, I?F’F’-3-621,or P?P=B=635- c~~s~~~sshall be in accordance with the appendix to the applicable con-tainer speclflcatlon. Fiberboard, when used, shall ha”~e a !zlnLmumMullen test or not less than 275 pounds. The gross weigh: of’ theshipping container, when packed for shipment, shall not ●xceed 200pounds; riberbOard containers shall not exceed the weight :Lmfta-:Lons gpecified In the applicable container speci?icatioz.

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KLL-F-Y9WYU

5.2.3 Level C. Package6 which require overpacklng for acceptanceby the ~ shall be ?acked in commercial exterior shlpptngcontainers in a manner that will insure safe transportation a% thelowest rate to the point of delivery. Contalmrs shall be inaccertience with SF.LTc2P_Pre@ht Classifleation Rules or rejyla-tions of other common carriers as applicable to the mode of trans-portation.

5.3 )4arklng of shlDments. If tear-apart containers are used,each section of the unit container shall be marked with the partnunber of the item. In ●ddition to any other npeclcal markingreauired by the contract or order, mark~ng for shipment shall bein-accord~ce with MIL-STD-129.

6. NOTES

6.1 Intended use. Fittings covered byintended for use in all types of fltids

this apeclfication areand are considered criti-

cal for procuzwaent purpoees. Pipe thrend ~ittings are generally~WzZri=tz& ~q tke~r ~mpiic~hle ClxxgwlngatQ O~g’en SYS%e- &ndground service eqtipment. Flared tube fittings of alumlnum from-2 through -12 size and carbon steel, titanium and corrosion-resistant steel fittings from -2 through -16 size are intended tcmeet the ZWqUiiWMSntS of M1b~-5440 Type 11, Class 3000 poundsper square inch (psi) and MIL-P-551~, Type A or B, Class 2 (3000psi). Larger size ~lttings through -32 size are intended forclass 1500 psi and Class 1 i1500 psi). Other specialized itemalso use this procurement specification. Tltanlum ~tzlngs andnuts shall not be used on oxygen systems. Disalmllar metals asderined by MIL-STD-889 shall not be used in direct contact w;theach other.

6.1.1 Supplemental ~nforma tion. me above listed capabilitiesfor flared Ittlnm are for ?ellablle fitting Joints as deflnec?in3.2 based upon teats and operational experience using AN and MSrittings, nuts, and sleeves. Using nonstandard design Joints(i.e., thicker walled nuts or flttlngs, special seals), burstpressures of 20,000 co 25,000 psi have been obtained with corres-pondingly high proof Pressures. Flttlngs may be uaecl at moresevere conditions than intended but Just as with etiemal condi-tions (load, tibratlon, corrosion, etc. ) the design and supportingtest data are the designer’s responsibility and must receive prio?approval rrom the procuring activity.

6.2 Ordering data. Procurement documents should speclry thefollowing:

a.

b.

c.

d.

?Itle, number, and date of this specification,

Part number required (see 1.2 and 3.2).

Plating, 1S aeslred for copper-base alloy parts (see3.3.I!}.

Applicable levels of p=servation-packaging and packingrequired (see 5.1 and 5.2).

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6.3 International standardization, Certain protislons of thisspeci ~ ect o international standardizationagreement ABC AiF Standard 17/15. When amendment, revision, orcancellation of this specification Is proposed, the departmenta~custodians will lnfonn their respective Departmental Standa?CLza-tion 0fflce3 so that appropriate action may be taken respectingthe international agreement concerned.

+ 6.4 Chanfitesfrom Previous issue. ‘T’he margins of this specifi-cation are marked with m asterisk to indicate where changes(additions, modifications, corrections, deletions) from the pre-tious issue were made. This was done as a convenience only antithe Government assumes no liability whatsoever for any inaccura-cies in these notations. Bidders and contractors are cautionedto ●valuate the requirements of this document based on the entirecontent irrespective of the marginal notations and relationship tothe last prwvious iSSUe.

Custodians: Preparing Actlvlty:Army - AV Mr Force - ?9Navy - ASAlr ?orce - 99 Agent :

DLA - CsReview Activities:

Army - ME (Project NO 4730-0706:

Navy - ASAir Force - 11DLA - CS

Zntematlonal Interest: (see 5.3)

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NOTICE OF INCH-POUNDCANCELLATION MIL-F-5509D(4) SUPP 1 NOTICE 2

30 September 1998

MILITARY SPECIFICATION

FITTINGS, FLARED TUBE, FLUID CONNECTION

MIL-F-5509D(4), dated 30 November 1987; and MIL-F-5509D, Supplement 1, dated16 June 1978, are hereby canceled. Future acquisitions for these products should refer to thefollowing standard(s) as applicable to the specific fittings. Each replacement standard citessuperseding information for known fittings that have MIL-F-5509 designated as a procurementspecification. The attached cross-reference listing is provided to indicate which AN or MS fromMIL-F-5509D, Supplement 1, applies to the superseding procurement specifications.

AS4841, Fittings, 37° Flared, Fluid ConnectionAS4842, Fittings and Bosses, Pipe Threaded, Fluid ConnectionAS4842/1, Fittings, 37° Flared to Pipe Threaded, Fluid ConnectionAS4843, Fittings, Beaded, Fluid ConnectionAS4843/1, Fittings, Beaded to 37° Flared, Fluid ConnectionAS4843/2, Fittings, Beaded to Pipe Threaded, Fluid ConnectionAS4875, Fittings, Straight Threaded Boss or Flanged, Fluid ConnectionAS4875/1, Fittings, Straight Thread Boss or Flanged to 37° Flared, Fluid ConnectionAS4875/2, Fittings, Flanged to Beaded, Fluid Connection

(DoD activities may obtain copies of these standards from the Defense Printing ServiceDetachment Office, Building 4D (Customer Service), 700 Robbins Avenue, Philadelphia, PA19111-5094. The private sector and other Government agencies may purchase copies from theSociety of Automotive Engineers International, 400 Commonwealth Drive, Warrendale, PA15096).

AMSC N/A FSC 4730DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

MIL-F-5509D(4) SUPP 1NOTICE 2

MIL-F-5509D, SUPPLEMENT 1, Cross-Reference Listing

Military Replacement Procurement Air Force - Navy Replacement ProcurementStandard Specification Aeronautical Standard Specification

MS20756...................AS4875 AN775....................................AS4875MS20757...................AS4875/2 AN776....................................AS4875/1MS20760...................AS4875/1 AN777....................................AS4875/1MS20819...................AS4841 AN778....................................AS4875/1MS20822...................AS4842/1 AN779....................................AS4875/1MS20823...................AS4842/1 AN786....................................CanceledMS20825...................AS4842/1 AN807....................................AS4843/1MS20826...................AS4842/1 AN816....................................AS4842/1MS20913...................AS4842 AN817....................................AS4841MS21946...................AS4875 AN818....................................AS4841MS21955...................AS4875/1 AN838....................................AS4843/1MS21958...................AS4875 AN839....................................AS4843/1MS21959...................AS4875 AN840....................................AS4843/2MS21960...................AS4875 AN842....................................AS4843/2MS24387...................AS4875/1 AN844....................................AS4843/2MS24388...................AS4875/1 AN846....................................AS4843MS24389...................AS4875/1 AN848....................................AS4843MS24390...................AS4841 AN849....................................AS4843MS24391...................AS4875 AN910....................................AS4842MS24392...................AS4841 AN911....................................AS4842MS24393...................AS4841 AN912....................................AS4842MS24394...................AS4841 AN914....................................AS4842MS24395...................AS4841 AN915....................................AS4842MS24396...................AS4841 AN916....................................AS4842MS24397...................AS4875 AN917....................................AS4842MS24398...................AS4875/1 AN918....................................AS4842MS24399...................AS4841 AN924....................................AS4841MS24401...................AS4841 AN929....................................AS4841MS24402...................AS4841 AN933....................................AS4842MS24403...................AS4841 AN937....................................AS4875MS24404...................AS4841 AN938....................................AS4875MS24487...................AS4875/1 AN939....................................AS4875MS27769...................AS4842 AN941....................................AS4875MS33583...................None, cited in AS4841 AN6204..................................AS4875MS33584...................Canceled, Use AS4330 AN6285-1..............................AS5166

2


Air Force - Navy Replacement Procurement Aeronautical Standard Specification

AN6285-2..............................AS5167 AN6289..................................AS4841

The following documents also specify MIL-F-5509 as the procurement document, but are notcited in the MIL-F-5509D Supplement 1. The superseding procurement specifications areprovided for additional cross-referencing:

Military Replacement Procurement Standard Specification MS21950................................AS4875/1

Air Force - Navy Replacement Procurement Aeronautical Standard Specification AN774....................................AS4875/1 AN783....................................AS4875/1 AN784....................................AS4875/1 AN804....................................AS4841 AN806....................................AS4841 AN814....................................AS4875 AN815....................................AS4841 AN821....................................AS4841 AN824....................................AS4841 AN827....................................AS4841 AN832....................................AS4841 AN833....................................AS4841 AN834....................................AS4841 AN837....................................AS4841 AN893....................................AS4875 AN894....................................AS4875/1 AN919....................................AS4841

NAS Standard Replacement Procurement SAE Standard Replacement Procurement Specification Specification

NAS424...............................AS4875 AS1031..................................AS4875/1 NAS551...............................AS4875 AS1032..................................AS4875/1 NAS552...............................AS4875/1 AS1033..................................AS4841

3


NAS Standard Replacement Procurement SAE Standard Replacement Procurement Specification Specification

NAS553...............................AS4875/1 AS1034..................................AS4841 NAS554...............................AS4875/1 AS1035..................................AS4841 NAS555...............................AS4875/1 AS1036..................................AS4841 NAS1410.............................AS4875 AS1037..................................AS4841 NAS1564.............................AS4841 AS1038..................................AS4841 AS1039..................................AS4841 AS1040..................................AS4841

Custodians: Preparing Activity: Army - AR DLA - CC Navy - AS Air Force - 99 (Project 4730-0858)

Review Activities: Army - AV, EA, GL, MI Air Force - 82

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Documents