Eaton Aeroquip Aerospace Catalog 110

Bulletin AA129

YL~eroquip

Aerospace Catalog 110 Excerpts

Aeroquip CorporationEngineered Systems Group

_ Jroquip Aerospace Division300 S. East Avenue, Jackson, Ml 49203-1972Phone: 517-787-8121, Fax: 517-787-5758www.aeroquip.comSpecfications subject to change without notice/Aeroquip products are protected by patents internationally

DISTRIBUTED BY

Ltho in U.S.A.

C Aeroquip Corporation 1992

HOSE FITTING

. ±L. -I AG

1, 11 i | * i , 5; | i I, 5 i i | - A

883 Straight Fitting ax(MS28760)

Hose Hose Max. Max.Size Size Dim. Dim. Dim. Weight

Part No. O.D. I.D. A B D (lbs.)

.883-4 .625 .219 2.09 .82 .83 .102

Material and finish: 883-6 .766 .344 2.45 .97 .95 .157Nut and nipple, cadmium-plated steel;socket, anodized aluminum. All materials 883-8 .859 .438 2.78 1.10 1.04 .228and finishes conform to applicable speci- 88310 1.031 .562 2.98 1.31 1.23 .350fications for end fittings used in aircraft ._.fluid systems. 883-12 1.219 .688 3.19 1.39 1.48 .542

883-16 1.500 .875 3.85 1.56 1.76 .813

980314 450 Fitting(MS28780) l______

980314-4 .625 .219 2.39 1.10 .83 .112Material and finish:

980314-6 766 .344 2.79 1.29 .95 .159Cadmium plated steel seamless tubingand bar stock except socket which is 980314-8 .859 .438 3.15 1.45 1.03 .242anodized aluminum alloy bar stock.Materials and finishes conform to appli--10 1.031 .562 3.37 1.68 1.23 .348cable specifications for end fittings used 980314-12 1.219 .688 4.06 2.25 1.48 ;568in aircraft fluid systems.

980314-16 1.500 .875 4.76 2.45 1.76 .841

_A

D ma' __

-980402 900 Fitting(MS28781)

980402-4 .625 .219 2.26 .97 .83 .114Material and finish: 980402-6 .766 .344 2.64 1.14 .95 .164Cadmium plated steel seamless tubingand bar stock except socket which is 980402-8 .859 .438 2.99 1.29 1.03 .252

Materials and finish alloy bar stock 980402-10 1.031 .562 3.20 1.52 1.23 .372cable specifications for end fittings used 980402-12 1.219 .688 4.05 2.24 1.48 .614in aircraft fluid systems.

980402-16 1.500 .875 4.82 2.52 1.76 .906

NIPPLE SOCKET NUT

F-_______ T threadUNJF class 3B

H(I.D) - hex.

(K doi oo~ m cone.,,)

(N=distance across corners)

Min. Max. Max.Dim. Dim. Dim. Dim. Dim. Dim. Dim. Dim. Thread

Part No. E H R Part No. F G K Part No. M N T

543-4 - .156 508-4D 1.495 .75 .88 .56 .65 7A6-20

543-6 - .281 - 508-6D 1.750 .83 .95 .69 .80 9A6-18

543-8 - .375 - 520-8D 1.975 .94 1.03 * .88 1.01 3%-16

543-10 - .455 - 520-10D 2.062 1.12 1.23 1.00 1.16 7/8 14

543-12 - .577 - 520-12D 2.290 1.31 1.48 1.25 1.45 I1 Ai-12

543-16 - .812 - 520-L6D 2.810 1.62 1.76 0 1.50 1.74 l5Ae-12

T thread

.______ F _ j UNJF class 3B

H(l.D.) =; G hex M hex.

Rrod--.

iK=dmsfnc ocro05 corners) (N -distance across corners)

985314-4 .352 .127 .38 508-4D 1.495 .75 .88 .56 .65 M/i6-20

985314-6 .445 .240 .50 508-6D 1.750 .83 .95 .69 .80 9/%6-18

985314-8 .456 .320 .50 520-8D 1.975 .94 1.03 .88 1.01 -4 16

985314-10 .536 .397 .62 520-10D 2.062 1.12 1.23 1.00 1.16 Ye-14

985314-12 .742 .509 1.25 520-12D 2.290 1.31 1.48 * 1.25 1.45 l/z6-12

985314-16 .815 .710 1.50 520-16D 2.810 1.62 1.76 * 1.50 1.74 1%.6-12

F T thread

H_ (I GD.)x UNJF class 3B

E M ~~~~~~~~~~~~hrhe.sR radius-

(N distonce across corners)

985402-4 .719 .127 .38 508-4D 1.495 .75 .88 .56 .65 7/A6 20

985402.6 .923 .240 .50 508-6D 1.750 .83 .95 * .69 .80 | 96-18

985402-8 .937 .320 .50 520-80 1.975 .94 1.03 * .88 1.01 3/4-16

985402-10 1.125 .397 .62 520-10D 2.062 1.12 1.23 1.00 1.16 Me- 14

985402-12 1.781 .509 1.25 520-12D 2.290 1.31 1.48 * 1.25 1.45 1k6-12. 985402-16 2.031 710 1.50 520-16D. 2.810 1.62 | 1.76 * 1.50 1.74 | Ae-12

'Nut is wvred-on and cannot be detached from nipple.

3

G Iobesea If Ia reless Assemblies, see page 20lobleseal flareless |Fittings, see pages 22, 23

Operating Temperatures:309 / MIL-H-8788 HOSE -65° to +200° F. (-4 thru -12)

-40° to +200° F. (-16)

Identification:Smooth black cover with linear yellow marking con-sisting of-"8788 (or 5512), size, date of manufacture(quarter year/year) and hose manufacturer's code."Spaced 180° from this is "Aeroquip 309." Markingsrepeated nine inches apart.

Application:Construction: 3000 psi hydraulic systems specified in MS33620.Construction: ~~~~~Hose assemblies conform to MIL-H-8790 andInner tube: seamless synthetic rubber compound. MS28762. Hose conforms to MIL-H-8788. AeroquipReinforcement: sizes 4 through 12 are high tensile Globeseal Flareless Fittings conform to MIL-F-8789carbon steel double wire braid; size 16 is high tensile and MS28761. Hose may be used in submerged,,carbon steel triple wire braid. Outer cover: smooth applications.synthetic rubber over fabric braid.

COMPLETE ASSEMBLY HOSE

Tube Weight Hose Hose Max. Min. Min. Min. WeightPART NO. size 12" ass'y PART NO. size size oper. proof burst bend per inch

0.D. (Ibs.) 1.D. 0.D. P.S.I. P.S.l. P.S.I. radii (Ibs.)

309000-4-L 309.4MS28762-4-L 1/4 .449 MIL-H-8788-4 .219 .625 3000 8000 16000 3.00 .024

309000-6-L 309-6MS28762-6-L .631 M I L- H-8788'6 .344 .766 3000 7000 14000 5.00 .032

.309000-8-L 309-8MS28762-8-L 1/2 .822 M I L- H-8788-8 .438 .859 3000 7000 14000 5.75 .037

MS28762-10-L % 1.194 M3IL-H-878810 .562 1.031 3000 6000 12000 6.50 .052

MS28762-12-L 3¾ 1.683 M3IL-H8788.12 .688 1.219 3000 6000 12000 7.75 .063

309000.16-L 25309.16MS28762-16-L 1 2.571 MIL-H-8788-16 .875 1.500 3000 5000 10000 9.62 .103

All dimensions in inches.

4

Globeseal flareless

__~ ~ ~~~~~~~~~~~~~~~~~~~~~~~~~~ _

Length oF Assembly To mate with MS33514, MS33515

| - F- |

A _

t B (K=distonc.e o.ross corners)Material and finish:

- ~~~~~508, 520 SOCKETS Nut and nipple,, cadmium-plated steel; socket, ano-dized aluminum. All materials and finishes conformto applicable specifications for end fittings used in

th,reod aircraft fluid systems.

882 | MS28761 UNJF clo i'\

HOSE FITTING LIH(L.D.) Met

(N-=disto.nce -crms cornm.-)

552 NIPPLE ASSEMBLY

HOSE FITTING SOCKET NIPPLE ASSEMBLY(Globeseal) (Globeseal)

Max. Max. Min. Max.

PART NO. Dim. Dim. Weight PART NO. Dim. Dim. Dim. PART NO. Dim. Dim. Dim. Thread

A B (lbs.) F G K H M N T

882-4 2.25 .98 .104 508-4D 1.495 .75 .828 552-4 .156 .562 .65 7/16-20

882-6 2.65 1.17 .161 508-6D 1.750 .83 .953 552-6 .281 .688 .80 9Ae'-18'

2876_-8

882-8 3.01 1.33 .236 520-SD 1.975 .94 1.030 552-8 .375 .875 1.01 34-16

MS286-1 3.26 1.59 .368 520-IOD 2.062 1.12 1.234 552-10 .461 1.000 1.15 7/a-14

882-12MS28761.12 3.46 1.67 .569 520-12D 2.290 1.31 1.484 552-12 .577 1.250 1.45 1%As-12

MS28;61-16 4.13 1.83 .856 520-16D 2.810 1.62 1.765 552-16 .812 1.500 1.74 136-12

MS28761I16

Choose assembly base nutnberfor desired style.

Fitting A Fitting B FITTING A ASSEMBLY FITTING BType Material Part No. Page Base No. Part No. Page

Alum.Unsleeved and 882 22 309000 882 22

Steel

AE102 Alum.Firesleeve and 882 22 620206 882 22Steel


Steel

AE102 Alum.Firesleeve and 882 22 620207 980628 22

___________________________________________Steel


SteelI

__ _ _ J L________ F~E102 Alum.Firesleeve and 882 22 620208 980629 22Steel

Alum.*Unsleeved and 980628 22 309070 980628 22

Steel

AE102 Alum.Firesleeve and 980628 22 620209 980628 22

____________________________________________Steel

Alum.Unsleeved and 980628 2 2 309071 980629 22

Steel

AE:102 Alum.Firesleeve and 980628 2 2 620210 980629 22

_______________________________________________SteelI

Alum.Unsleeved and 980629 22 309072 980629 2 2

Steel

AE102 Alum.Fireseeve Steel

_ -HOSE FITTING

882 Straight Fitting(MS28761) D max.


Part No. O.D. I.D. A B D (Ibs.)

882-4 .625 .219 2.25 .98 .83 .104

Material and finish: 882-6 .766 .344 2.65 1.17 .95 .161

Nut and nipple, cadmium-plated steel;socket, anodized aluminum.All materials 882-8 .859 .438 3.01 1.33 1.03 .236

and finishes conform to applicable speci- 88210 1.031 .562 3.26 1.59 1.23 .368

fications for end fittings used in aircraftfluid systems. 882-12 1.219 .688 3.46 1.67 1.48 .569

882-16 1.500 .875 4.13 1.83 1.76 .856

A

980628 450 Fitting D Am

980628-4 .625 .219 2.49 1.20 .83 .114Material and finish:

Cadmium plated steel seamless tubing 980628-6 .766 .344 2.92 1.43 .95 .165

and bar stock except socket which is 980628-8 .859 .438 3.30 1.61 1.03 .252

anodized aluminum alloy bar stock.Materials and finishes conform to appli- 980628-10 1.031 .562 3.56 1.88 1.23 .366

cable specifications for end fittings used 980628-12 1.219 688 4.24 2.43 1.48 .596

in aircraft fluid systems. . .

980628-16 1.500 .875 4.95 2.65 1.76 .885

B.

980629 900 Fitting Dmax. - ___

980629-4 .625 .219 2.26 .97 .83 .116

Material and finish:

Cadmium plated steel seamless tubing 980629-6 .766 .344 2.64 1.14 .95 .170

and bar stock except socket which is 980629-8 .859 .438 2.99 1.29 1.03 .261

anodized aluminum alloy bar stock.Materials and finishes conform to appli- 98062910 1.031 .562 3.20 1.52 1.23 .390

cable specifications for end fittings used 980629-12 1.219 .688 4.05 2.24 1.48 .641

in aircraft fluid systems.980629-16 1.500 .875 4.82 2.52 1.76 .950

7

NIPPLE SOCKET NUT

T threodUNJF closs 3B

f i G~~~~~~~~~~~~~~~~~~~~~~ hen. H(I.D,) S >$hx

(K =dironcn ocross corners)(N=distonce across corners)



5524 - .156 - 508-4D 1.495 .75 .83 .56 .65 'A7h20552-6 - .281 - 508-6D 1.750 .83 .95 .69 .80 9h6-18

552-8 - .375 - 520-8D 1.975 .94 1.03 .88 1.01 3/4 .16

552-10 - .461 - 520-10D 2.062 1.12 1.23 1.00 1.16 7/8 -14

552-12 - .577 - 520-12D 2.290 1.31 1.48 1.25 1.45 146-12

552-16 - .812 - 520-16D 2.810 1.62 1.76 1.50 1.74 1Y6-12

T threadi -_- .!-................... F -i UNJF class 3B

H(I.D.)-- .:

R rr dius/ Mh.

(K =distoncn ocross corners) (N =distonce across corners)

985628-4 .452 .127 .38 508-4D 1.495 .75 .83 _ .56 .65 7/,6-20

985628-6 .578 .240 .50 508-6D 1.750 .83 .95 .69 .80 9A6-18

985628-8 .610 .320 .50 520-8D 1.975 .94 1.03 .88 1.01 3/4 -16

985628-10 .725 .397 .62 520-1OD 2.062 1.12 1.23 I 1.00 1.16 /e -14

985628-12 .919 .509 1.25 520-12D 2.290 1.31 1.48 1.25 1.45 11/16-12

985628-16 1.010 .710 1.50 520-16D 2.810 1.62 1.76 . 1.50 1.74 lVY6-12

Is e nT thredH(I.D.) \- 14Fcos3

R rradius |ij|hx

E~~~~~~~~~~~~Kd~- -r, wr- . (N=distcmce across corners)

985629-4 .859 .127 .38 508-4D 1.495 .75 .83 * .56 .65 7Ar6-20

985629-6 1.111 .240 .50 508-6D 1.750 .83 .95 . .69 .80 9/16-18

985629-8 1.156 .320 .50 520-8D 1.975 .94 1.03 * .88 1.01 3/4 -16

985629-10 1.391 .397 .62 520-1OD 2.062 1.12 1.23 1.00 1.16 Y/ -14

985629-12 2.031 .509 1.25 520-12D 2.290 1.31 1.48 1.25 1.45 11|16- 12

985629-16 2.306 .710 1.50 520-16D 2.810 1.62 1.76 1.50 1.74 1_6-12

--- w~~~~~~~~~~ Choose assembly base number

** . Ia @ . E S ! * . a I . u . I . |for desired style.


Alum. 491 58 360 491 58

Unsleeved Alum. 451 58 390A 451 58

Steel 491 58 350 491 58

m i i i ] _ _ ,__ _ _ _ __ _ _ _ _

AE102 Alum. 491 or 451 58 620001 491 or 451 58

Firesleeve Steel 491 or 451 58 620000 491 or 451 58

Alum. 491 or 451 58 950012 980006 58Unsleeved

Steel 491 or 451 58 950012 980006 58

EmIL]LI7in__ ___.

AE102 Alum. 491 or 451 58 620003 980006 58

Firesleeve Steel 491 or 451 58 620002 980006 58


Steel 491 or 451 58 950004 980005 58

*___________________________ U AE102 Alum. 491 or 451 58 620007 980005 58

Firesleeve Steel 491 or 451 58 620006 980005 58

Alum 980006 58 950010 980006 58Unsleeved

Steel 980006 58 950816 980006 58

%IIII3L_ i ____

AE1O2 Alum. 980006 58 620011 980006 58

Firesleeve Steel 980006 58 620010 980006 58

Alum. 980006 58 950003 980005 58Unsleeved

Steel 980006 58 950668 980005 58

AE102 Alum. 980006 58 620015 980005 58


Alum. 980005 58 950002 980005 58_ ~~~~~~~~~~~~U nsleeved _

w _ ~~~~~~ ~~~~~~~ ~~~~Steel 980005 58 950680 980005 58

- AE102~~~~Alum. 980005 58 620019 980005 58

* - ~~~~~~~~~~~~~~Firesleeve Steel 980005 58 620018 980005 5

L~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

Choose assembly base numberfor desired style.


Alum. 491 58 360 491 58

Unsleeved Alum. 451 58 390A 451 58

Steel 491 58 350 491 58

AE102 Alum. 491 or 451 58 620001 491 or 451 58Firesleeve Steel 491 or 451 58 620000 491 or 451 58

Alum. 491 or 451 58 950234 980136 60U nsleevedSteel 491 or 451 58 950234 980136 60

AE102 Alum. 491 or 451 58 620005 980136 60Firesleeve Steel 491 or 451 58 620004 980136 60


Steel 491 or 451 58 950192 980137 60

:AE102 Alum. 491 or 451 58 620009 980137 60Firesleeve Steel 491 or 451 58 620008 980137 60

Unsleeved Alum. 980136 60 950247 980136 60_ Steel 980136 60 1 950817 980136 60

AE102 Alum. 980136 60 620013 980136 60Firesleeve Steel 980136 60 620012 980136 60

Alum. 980136 60 950233 980137 60Unsleeved_Steel 980136 60 950818 980137 60


Alum. 980137 60 950248 980137 60_ ~~~~~~~~~~Unsleeved_Steel 980137 60 950819 980137 60

0 AEI2 Alum. 980137 60 620021 980137 60Firesleeve Steel 980137 60 620020 980137 60

10

__ HOSE FITTING_~~~~~ . i

491 Straight Fitting (MS24587)

Hose Hose Max. Max.Size Size Dim. Dim. Dim. Dim. Weight

Part No. O.D. I.D. A B C D (lbs.)

491-3 .453 .125 1.43 .65 .32 .63 .034Material and finish:

491.4 .516 .188 1.51 .65. .35 .69 .055Nut and nipple sizes -3, -4, -5 and -6 arecadmium-plated steel bar stock. Sizes 491-5 .578 .250 1.64 .74 .38 .76 .071-8 and up and sockets are anodizedaluminum alloy bar stock. Materials and 491-6 .672 .313 1.79 .77 .38 .88 .096finishes conform to applicable specifica- 491-8D .766 .406 2.22 .94 .43 1.00 .097tions for end fittings used in aircraft 49IO92 50 24 1.0 .1 1.3 .3

f I u i d syste ms. ~~~~~~491 -10D .922 .500 2.42 1.00 .51 I1.23 .135 lfluid systems.491-12D 1.078 .625 2.70 1.00 .57 1.36 .185

A

B-

980006 450 Fitting Dmox ">'IC(MS27226)

Material and finish: 980006-4 .516 .188 1.99 1.12 .37 .69 .069Nut and nipple sizes .4, -5 and -6 arecadmium-plated steel seamless tubing 980006-5 .578 .250 2.24 1.34 .38 .76 .094and bar stock. Sizes -8 and up andsockets are anodized aluminum alloy 980006-6 .672 .313 2.40 1.38 .38 .88 .126seamless tubing and bar stock. Materialsandfinishesconformtoapplicablespeci- 980006-8D .766 .406 2.82 1.55 .44 1.00 .110fications for end fittings used in aircraftfluid systems. 980006-10D .922 .500 3.11 1.70 .50 1.23 .159

0 moz. = =

980005 900 Fitting(MS27224)

Material and finish: 980005-4 .516 .188 1.86 .99 .37 .69 .072Nut and nipple sizes -4, -5 and -6 are _

cadmium-plated steel seamless tubing 980005-5 .578 .250 2.08 1.18 .38 .76 .098and bar stock. Sizes -8 and up andsockets are anodized aluminum alloy 980005-6 .672 .313 2.25 1.23 .38 .88 .131seamless tubing and bar stock. Materialsandfinishesconformtoapplicablespeci- 980005-8D .766 .406 2.66 1.39 .44 1.00 .113fications for end fittings used in aircraftfluid systems. 980005-1OD *.922 .500 2.94 1.52 .50 1.23 .164


NIPPLE SOCKET NUT

F __ ~~~~~~UU~~~~fL ~~T thread

137 G M es UNF class 3B

(K =distance ecross corners) (N=distance across corners)



251-3 - .123 - 210.3D 1.000 .562 .630 290-3 .438 .51 3/a-24

251-4 - .170 - 210-4D 1.100 .625 .693 290-4 .563 .65 7/16-20

251-5 - .232 - 210-5D 1.200 .688 .755 290-5 .625 .72 '/2-20

251-6 - .295 - 210-6D 1.300 .812 .880 290-6 .688 .80 %/,6-18

271-8D - .390 - 215-8D 1.650 .938 1.005 290-8D .875 1.01 3/4-16

271-10D .484 - 215-10D 1.800 1.125 1.234 290-10D 1.000 1.16 7/8-14

271-12D .608 - 215-12D 2.100 1.250 1.359 290.12D 1.250 1.45 1YE6-12

T threadUNJF class 3B

H I - F ---- O--

( )U_ E L hn M hex.

RKrclla(K dst a cross corners)

(N=distonce across corners)

985006-4 .352 .123 .375 210-4D 1.100 .625 .693 .562 .65 Ve-20

985006-5 .415 .170 .438 210-5D 1.200 .688 .755 .625 .72 ½/2-20

985006-6 .444 .232 .500 210-6D 1.300 .812 .880 .688 .80 9/16-18

985006-8D .456 .355 .500 215-8D 1.650 .938 1.005 .875 1.01 /4-16

985006-10D .536 .450 .625 215-10D 1.800 1.125 1.234 1.000 1.16 7/ -14

T threcad

H(ID) IF UNJF class 3BH(l.D.)

7 > E u sfl>G hex E M hex.

R rasdius W -J

(K distonce a ras a an )


985005.4 .718 .123 .375 210-4D 1.100 .625 .693 .562 .65 | 46-20

985005-5 .844 .170 .438 210-5D 1.200 .688 .755 .625 .72 Y2-20

985005-6 .922 .232 .500 210.6D 1.300 .812 .880 .688 .80 |9A6-18

985005-8D .938 .355 .500 215-8D 1.650 .938 1.005 . .875 1.01 | 3/4-16

985005-10D 1126 .450 .625 215-10D 1.800 1.125 1.234 1.000 1.16 | a-14

nNut is wired-orn and cannot be detached from nipple

12

__ HOSE FITTING

I r~~~~Bj C

451 Straight Fitting D max.(MS24587)

Hose Hose Max. Max.Size Size Dim. Dim. Dim. Dim. Weight

Part No. O.D. I.D. A B C D (lbs.)

451-16D 1.234 .875 2.34 .94 .60 1.55 .220Material and finish:Manodize andufinish: alloybarstock. 451-20D 1.500 1.125 2.48 1.00 .64 1.92 .422Anodized aluminum alloy bar stock. ______ ___ ___

Sockets sizes -24 and up are anodized 451-24D 1.750 1.375 2.67 1.09 .74 2.12 .504aluminum alloy forgings. Materials andfinishes conform to applicable specifi- 451-32D 2.219 1.812 3.21 1.24 .93 2.64 .850cations for end fittings used in aircraftfluid systems. 451-40D 2.875 2.375 3.48 1.45 .80 3.39 1.322

980136 450 Fitting D ms(MS27226)

Material and finish: 980136-12D 1.078 .625 3.58 1.89 .57 1.36 .220

Anodized aluminum alloy seamless 980136-16D 1.234 .875 3.23 1.84 .63 1.55 .249tubing and bar stock. Sockets sizes -24and -32 are anodized aluminum alloy 980136-20D 1.500 1.125 3.64 2.16 .64 1.92 .469forgings. Materials and finishes conformto applicable specifications for end fit- 980136-24D 1.750 1.375 3.98 2.40 .77 2.12 .606

tings used in aircraft fluid systems. 980136-32D 2.219 1.812 4.80 2.84 .92 2.64 1.023

980137 900 Fitting D(MS27224)

C

Material and finish: 980137-12D 1.078 .625 3.46 1.76 .57 1.36 .226

Anodized aluminum alloy seamless 980137-16D 1.234 .875 3.14 1.75 .63 1.55 .261tubing and bar stock. Sockets sizes -24and -32 are anodized aluminum alloy 980137-20D 1.500 1.125 3.57 2.09 .64 1.92 .491forgings. Materials and finishes conformto applicable specifications for end fit- 980137-24D 1.750 1.375 3.92 2.34 .77 2.12 .640

tings used in aircraft fluid systems. 980137-32D 2.219 1.812 4.76 2.80 .92 2.64 1.070


13

NIPPLE SOCKET NUT

Z370 UNF class 39

(K=disconc. ac.. e) (N=distonce across corners)



251-16D - .810 - 212-16D 1.661 1.438 1.546 290-160 1.500 1.736 16-12

251-20D - 1.042 - 212-20D 1.750 1.750 1.921 290-20D 2.000 2.328 1 %-12

251-24D - 1.276 - 212-24D 1.845 1.938 2.124 290-24D 2.250 2.621 1 7h-12

251-320 - 1.745 - 212-32D 2.250 2.438 2.640 290-32D 2.875 3.343 2 2-12

251-40D - 2.199 - 212-40D 2.500 3.120 3.390 290-40D 3.375 3.920 3 -12

T threadUNJF class 38

H(l.D.)

E M hex.~7

(K distonce a a rane)

(N=cdistonce across corners)

985136-120 .623 .576 .844 215-12D 2.100 1.250 1.359 1.250 1.447 l1/A6-12

985136-16D .660 .810 .969 212- 16D 1.661 1.438 1.546 1.500 1.736 15Y,6-12

985136-20D .768 1.042 1.188 212-20D 1.750 1.750 1.921 2.000 2.328 1 %-12

985136-24D .867 1.276 1.375 212.24D 1.845 1.938 2.124 2.250 2.621 1 7/8-12

985136-32D 1.066 1.745 1.750 212-32D 2.250 2.438 2.640 2.875 3.343 2 1/2-12

T threadF UNJF class 38

/I E7The _ M hex.R radius / (K _-ditance acros corcrs)


985137-12D 1.376 .576 .844 215-12D 2.100 1.250 1.359 , 1.250 1.447 |Y1%-12

985137-16D 1.500 .810 .969 212-16D 1.661 1.438 1.546 1.500 1.736 1l5

16-12

985137-20D 1.782 1.042 1.188 212-20D 1.750 1.750 1.921 2.000 2.328 1 %-12

985137-24D 2.032 1,276 1.375 212-24D 1.845 1.938 2.124 2.250 2.621 1 Ys-12

985137-32D 2.532 1.745 1.750 212-32D 2.250 2.438 2.640 2.875 3.343 2 h-12

*Nut is wired -on and cannot be detached from nipple W

14

Assemblies, see page 66Globeseal flareless Fittings,seepages68,69

303, 302A / MIL-H-8794 HOSE Operating Temperatures:303 hose, -65° to +250'F.302A hose, -40° to +250'F.

Identification:Grey-black braided cover with linear yellow markingconsisting of- 8794, size, date of manufacture(quarter year/year) and hose manufacturer's code."Spaced 90° from this is a yellow indicator stripe inter-spersed with "Aeroquip 303" or "Aeroquip 302A."Markings repeated nine inches apart.

Application:Construction:eamiess synthetic Medium pressure hydraulic, pneumatic, fuel, oil andcoolant systems. Hose conforms to MIL-H-8794.Inner tube: seamless synthetic rubber compound. Fittings conform to MIL-A-5070. Hose may be usedReinforcement: synthetic-impregnated single wire in submerged applications.braid over single cotton braid. Outer cover: syntheticimpregnated oil-resistant cotton braid.

COMPLETE ASSEMBLY HOSE

Tube Weight Hose Hose Max. Min. Min. Min WeightPART NO. size 12" ass'y PART NO. size size oper. proof burst bend per inch

0.D. (lbs.) I.D. 0.D. P.S.I. P.S.l. P.S.l. radii' (Ibs.)

950532-4-L Yc .247 303I.4 .188 .516 3000 6000 12000 3.00 .011

950532-5-L 5A6 .291 303-5 .250 .578 3000 5000 10000 3.38 .013

950532-6-L .430 303I-6 .313 .672 2000 4500 9000 4.00 .019

950532-BDL 1/2 .440 303- 8 .406 .766 2000 4000 8000 4.62 .022

950532-1ODL % .615 303-10 500 .922 1750 3500 7000 5.50 .031MIL-H-8794-10

950532-12DL ¾ .788 303-12 .625 1.078 1500 3000 6000 6.50 .038MIL.H-8794-12

950532-16DL 1 .897 MIL-H-8794316 875 1.234 800 1600 3200 7.38 .037

950532-20DL 14 1.374 302A20 1.125 1.500 600 1250 2500 9.00 .043

950532-24DL 11/2 1.667 MIL-H-8794324 1.375 1.750 500 1000 2000 11.00 .056

'At maximum operating pressure.

Globeseal flareless

2 Length of Assembly I To mate with MS33514, MS33515

L A~~~~G hex.

I~~~~~~ I A M istance across corners)(K-distance aunts corerns) Material and finish:

210, 215 SOCKET Nut and nipple, sizes 4 through 6, cadmium-platedsteel. Nut and nipple, sizes 8 up, and socket, anodized

flyMOM24 W 2 aluminum. All materials and finishes conform tolm}GT shreOd applicable specifications for end fittings used in

440~ ~ ~ ~ ~ ~~~~~ J cla Fi 7 aircraft fluid systems.440( HOSE FITTING .L. -I

H(I.D.) M hex.


440-3-SIZENIPPLE ASSEMBLY

HOSE FITTING SOCKET NIPPLE ASSEMBLY(Globeseal) (Globeseal)

Max. Max. Min. Max.PART NO. Dim. Dim. Weight PART NO. Dim. Dim. Dim. PART NO. Dim. Dim. Dim. Thread

A B (Ibs.) F G K H M N T

440-4 1.78 .94 .068 210-4D 1.100 .625 .693 440-3-4 .170 .562 .65 7/16-20

440-5 1.92 1.05 .081 210-SD 1.200 .688 .755 440-3-5 .232 .625 .72 1/2-20

440-6 2.11 1.11 .122 210.6D 1.300 .812 .880 440-3-6 .295 .688 .80 9/16- 18

440-8D 2.58 1.33 .117 215-SD 1.650 .938 1.005 440-3-SD .390 .875 1.01 3/4-16

440-IOD 2.84 1.46 .167 215-10D 1.800 1.125 1.234 440-3-1OD .484 1.000 1.16 3s-14

440-12D 3.14 1.47 .222 215-12D 2.100 1.250 1.359 440-3-12D .608 1.250 1.45 11ie-12

440-16D 2.97 1.60 .286 212-16D 1.661 1.438 1.546 440-3-16D .810 1.500 1.74 1516-12

440-20D 3.17 1.72 .503 212-20D 1.750 1.750 1.921 440-3-20D 1.042 2.000 2.33 1%-12

440-24D 3.49 1.94 .606 212-24D 1.845 1.938 2.124 440-3-24D 1.276 2.250 2.62 1Ya-12


16

Choose assembly base numberfor desired style.


Unsleeved Alum. 440 68 950532 440 68

_________ -r Steel 440 68 950532 440 68


Alum. 440 68 950781 980688 68Un sleevedSteel 440 68 950781 980688 68

AE102 Alum. 440 68 620055 980688 68


Alum. 440 68 950645 980569 68

Steel 440 68 950645 980569 68


Alum. 980688 68 950785 980688 68Unsleeved

Steel 980688 68 950782 980688 68


Alum. 980688 68 950786 980569 68Unsleeved

Steel 980688 68 950783 980569 68


Alum. 980569 68 950787 980569 68Unsleevedw Steel 980569 68 950784 980569 68 -


17

_=_ HOSE FITTING

440 Straight Fitting D


Part No. O.D. ID. A B D (lbs.)440-4 .516 .188 1.78 .94 .69 .068

Material and finish: 440-5 .578 .250 1.92 1.05 .76 .081Nut and nipple sizes -4, -5 and -6 are 440-6 .672 .313 2.11 1.11 .88 .112cadmium-plated steel bar stock. Sizes 440.8D .766 .406 2.58 1.33 1.00 .117-8 and up and sockets are anodizedaluminum alloy bar stock except -24 440-10D .922 .500 2.84 1.46 1.23 .167socket is anodized aluminum alloy forg- 440-12D 1.078 .625 3.14 1.47 1.40 .222ing. Materials and finishes conform toapplicable specifications for end fittings 440-16D 1.234 .875 2.97 1.62 1.68 .286used in aircraft fluid systems. 440-20D 1.500 1.125 3.17 1.72 2.22 .503

440.24D 1.750 1.375 3.49 1.94 2.62 .606A~~

980688 450 Fitting D [ m ax.

980688-4 .516 .188 2.09 1.22 .69 .039

980688-5 .578 .250 2.35 1.45 .76 .050Material and finish: 980688-6 .672 .313 2.53 1.51 .88 .071Anodized aluminum alloy seamless tub- 980688-8D .766 .406 2.98 1.71 1.00 .114ing and bar stock. Materials and finishesconform to applicable specifications for 980688-l0D .922 .500 3.29 1.88 1.23 .165end fittings used in aircraftfluid systems. 980688-12D 1.078 .625 4.05 2.36 1.36 .210

980688.16D 1.234 .875 3.80 2.41 1.55 .264

980688-20D 1.500 1.125 4.06 2.58 1.92 .502

980569 900 Fitting D max

980569-4 .516 .188 1.86 .99 .69 .039980569.5 .578 .250 2.08 1.18 .76 .052

Material and finish: 980569-6 .672 .313 2.25 1.23 .88 .072Anodized aluminum alloy seamless tub- 980569-8D .766 .406 2.66 1.39 1.00 .117ing and bar stock. Materials and finishes .conform to applicable specifications forend fittings used in aircraftfluid systems. 980569-12D 1.078 .625 3.86 2.17 1.36 .236

980569-16D 1.234 .875 3.67 2.28 1.55 .276980569-20D 1.500 1.125 3.88 2.40 1.92 .523

18

NIPPLE SOCKET NUTT thread

F SG h UNJF dss 31

0 ha ~~~~~~~~~~~M~Mhe..



Part No. E H R Part No. F G K Part No. M N T440-3-4 - .170 - 210-4D 1.100 .62 .69 . .56 .65 7h6-20

440-3-5 - .232 - 210-5D 1.200 .69 .76 .62 .72 ½/2-20440-3-6 - .295 - 210-6D 1.300 .81 .88 .69 .80 9Ae-18440-3-8D - .390 - 215-8D 1.650 .94 1.00 .88 1.01 3/4-16

440-3-10D - .484 - 215-lOD 1.800 1.12 1.23 1.00 1.16 7Y- 14

440-3-12D - .608 - 215-12D 2.100 1.25 1.36 1.25 1.45 1 116-12

440-3-16D - .810 - 212-16D 1.661 1.44 1.55 1.50 1.74 P4/6-12440-3-20D - 1.042 - 212-20D 1.750 1.75 1.92 . 2.00 2.31 1%-12

440-3-24D 1.276 - 212-24D 1.845 1.94 2.12 2.25 2.62 1%8-12

T thread

UNJF clans 31H(I.D.) '

E hGe.i

R rodius // ~~~~~~~~~~~(K=60-1.c (Ncdiv- . ..... co,.,,

(N -disronce across corners)

985688-4 .452 .123 .38 210-4 1.100 .62 .69 .56 .65 7h6-20985688-5 .525 .170 .44 210-5 1.200 .69 .76 . .62 .72 1/2-20

985688-6 .578 .232 .50 210-6 1.300 .81 .88 .69 .80 9/16-18

985688-8D .610 .355 .50 215-8D 1.650 .94 1.00 .88 1.01 3/4-16

985688-10D .725 .450 .62 215-10D 1.800 1.12 1.23 1.00 1.16 Y-14

985688-12D .800 .576 1.25 215-12D 2.100 1.25 1.36 1.25 1.45 l 1/16-12

985688-16D .855 .810 1.50 212-16D 1.661 1.44 1.55 . 1.50 1.74 l 5A6-12985688-20D .962 1.042 1.50 212-20D 1.750 1.75 1.92 . 2.00 2.31 1 %- 12

T threadH(l D.) - F------ UNJF cloC 38

/ , E G ~~~~Ohen. > N.

R roedius l0l~ ziM h...

6 ~~~~~~~~~~~~(K=d oonce across corners) J |(N=dsrtonce across corners)

985569-4 .860 .123 .38 210-4 1.100 .62 .69 * .56 .65 7/16-20985569-5 .1.000 .170 .44 210-5 1.200 .69 .76 .62 .72 1/2-20

985569-6 1.112 .232 .50 210-6 1.300 .81 .88 .69 .80 | 9 6-18985569-8D 1.156 .355 .50 215-81D 1.650 .94 1.00 .88 1.01 3A-16

985569-10D 1.392 1 .450 .62 215-10D 1.800 1.12 1.23 1.00 1.16 Y/e-14

985569-12D 1.626 .576 1.25 215-12D 2.100 1.25 1.36 * 1.25 1.45 1 lff-12*i 985569-16D 1.776 .810 1.50 212-16D 1.661 1.44 1.55 * 1.50 1.74 P e-12__ 985569-20D 2.057 1.042 1.50 212-20D | 1.750 1.75 1.92 * 2.60 2-31 1-12

'Nut is wired-on and cannot be detached from nipple.

19

Documents

Eaton Aeroquip Aerospace Catalog 110