Eaton Aeroquip Aerospace Catalog 110 by Murdock Industrial

Bulletin AA129

YL~eroquip Aerospace Catalog 110 Excerpts

Aeroquip Corporation Engineered Systems Group Aerospace Division Jroquip 300 S. East Avenue, Jackson, Ml 49203-1972 Phone: 517-787-8121, Fax: 517-787-5758 www.aeroquip.com Specfications 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 . 1, 11i *

I |

ÂąL. i

5i i -

883 Straight Fitting

(MS28760)

Hose Size O.D.

Part No.

Material and finish: Nut and nipple, cadmium-plated steel; socket, anodized aluminum. All materials and finishes conform to applicable specifications for end fittings used in aircraft fluid systems.

980314

Hose Size I.D.

Max. Dim. A

Dim. B

Max. Dim. D

Weight (lbs.)

.883-4

.625

.219

2.09

.82

.83

.102

883-6

.766

.344

2.45

.97

.95

.157

.438 .562

2.78 2.98

1.10 1.31

1.04 1.23

.228 .350

883-12

.859 1.031 ._. 1.219

.688

3.19

1.39

1.48

.542

883-16

1.500

.875

3.85

1.56

1.76

.813

883-8 88310

450 Fitting

(MS28780)

l______

Material and finish: Cadmium plated steel seamless tubing and bar stock except socket which is anodized aluminum alloy bar stock. Materials and finishes conform to appli--10 cable specifications for end fittings used in aircraft fluid systems.

980314-4

.625

.219

2.39

1.10

.83

.112

980314-6

766

.344

2.79

1.29

.95

.159

980314-8

.859

.438

3.15

1.45

1.03

.242

980314-12

1.031 1.219

.562 .688

3.37 4.06

1.68 2.25

1.23 1.48

.348 ;568

980314-16

1.500

.875

4.76

2.45

1.76

.841

D ma'

-980402 (MS28781)

900 Fitting

Material and finish:

980402-4 980402-6

.625 .766

.219 .344

2.26 2.64

.97 1.14

.83 .95

.114 .164

Cadmium plated steel seamless tubing and bar stock except socket which is

980402-8

.859

.438

2.99

1.29

1.03

.252

Materials and finish

980402-10

1.031

.562

980402-12

1.219

.688

3.20 4.05

1.52 2.24

1.23 1.48

.372 .614

980402-16

1.500

.875

4.82

2.52

1.76

.906

alloy

bar stock

cable specifications for end fittings used in aircraft fluid systems.

NUT

SOCKET

NIPPLE

T thread UNJF class 3B

F-_______

H(I.D)

hex.

doi

oo~

cone.,,)

(N=distance across corners)

Part No.

Dim. E

543-4

Min. Dim. H

Dim. R

Part No.

508-4D

.156

Dim. F

Dim. G

Max. Dim. K

1.495

.75

.88

543-6

.281

508-6D

1.750

.83

.95

543-8

.375

520-8D

1.975

.94

1.03

543-10

.455

520-10D

2.062

1.12

1.23

543-12

.577

520-12D

2.290

1.31

1.48

543-16

.812

520-L6D

2.810

1.62

1.76

.______

H(l.D.)

Part No.

Dim. M

Max. Dim. N

.56

.65

.69

.80

.88

1.01

1.00

1.16

A6-20

A6-18 3

%-16 7/814 1

1.25

1.45

I Ai-12

1.50

1.74

l 5Ae-12

T thread UNJF class 3B

M hex.

hex

Thread T

Rrod--. iK=dmsfnc

(N -distance across corners)

ocro05corners)

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

T thread UNJF class 3B

F GD.)x

H_ (I

~~~~~~~~~~~~hrhe.s M

E R radius-

985402-4

.719

.127

.38

508-4D

1.495

.75

.88

985402.6

.923

.240

.50

508-6D

1.750

.83

.95

985402-8

.937

.320

.50

520-80

1.975

.94

1.03

985402-10

1.125

.397

.62

520-10D

2.062

1.12

1.23

985402-12

1.781

.509

1.25

520-12D

2.290

1.31

1.48

985402-16

2.031

710

1.50

520-16D.

2.810

1.62

| 1.76

distonce across corners)

/A620

.56

.65

.69

.80

.88

1.01

3/4-16

1.00

1.16

Me- 14

1.25

1.45

1k6-12

1.50

1.74

96-18

Ae-12

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

GIobesea Ifflareless Iareless |Fittings, Assemblies, see page 20 lobleseal see pages 22, 23

Operating Temperatures: -65° to +200° F. (-4 thru -12) -40° to +200° F. (-16)

309 / MIL-H-8788 HOSE

Identification: Smooth black cover with linear yellow marking consisting of-"8788 (or 5512), size, date of manufacture (quarter year/year) and hose manufacturer's code." Spaced 180°from this is "Aeroquip 309." Markings repeated nine inches apart. Construction: Construction: Inner tube: seamless synthetic rubber compound. Reinforcement: sizes 4 through 12 are high tensile carbon steel double wire braid; size 16 is high tensile carbon steel triple wire braid. Outer cover: smooth synthetic rubber over fabric braid.

COMPLETE ASSEMBLY PART NO.

Tube size 0.D.

309000-4-L

MS28762-4-L

1/4

309000-6-L

MS28762-6-L

.309000-8-L

Application: 3000 psi hydraulic systems in MS33620. ~~~~~Hose assemblies conform specified to MIL-H-8790 and MS28762. Hose conforms to MIL-H-8788. Aeroquip Globeseal Flareless Fittings conform to MIL-F-8789 and MS28761. Hose may be used in submerged,, applications.

HOSE

Weight 12" ass'y (Ibs.)

PART NO.

.449

MIL-H-8788-4

.631

M IL- H-8788'6

309.4

309-6

309-8

Hose size 1.D.

Hose size 0.D.

Max. oper. P.S.I.

Min. proof P.S.l.

Min. burst P.S.I.

Min. bend radii

Weight per inch (Ibs.)

.219

.625

3000

8000

16000

3.00

.024

.344

.766

3000

7000

14000

5.00

.032

MS28762-8-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

MIL-H-8788-16

.875

1.500

3000

5000

10000

9.62

.103

309000.16-L

MS28762-16-L

25309.16 2.571

All dimensions in inches.

__~

Globeseal flareless _ ~~~~~~~~~~~~~~~~~~~~~~~~~~ To mate with MS33514, MS33515

Length oF Assembly

F-

(K=distonc.e o.rosscorners)

t B

Material and finish: Nut and nipple,, cadmium-plated steel; socket, anodized aluminum. All materials and finishes conform to applicable specifications for end fittings used in aircraft fluid systems.

520 SOCKETS ~~~~~508,

th,reod UNJF clo

882 | MS28761

i'\

HOSE FITTING

Met

H(L.D.)

(N-=disto.nce

cornm.-) -crms

552 NIPPLE ASSEMBLY

NIPPLE ASSEMBLY

SOCKET

HOSE FITTING

(Globeseal)

Max. Dim. A

Dim. B

882-4

2.25

882-6

Dim. G

Max. Dim. K

PART NO.

Min. Dim. H

Dim. M

Max. Dim. N

Thread T

Weight (lbs.)

PART NO.

Dim. F

.98

.104

508-4D

1.495

.75

.828

552-4

.156

.562

.65

2.65

1.17

.161

508-6D

1.750

.83

.953

552-6

.281

.688

.80

882-8

3.01

1.33

.236

520-SD

1.975

.94

1.030

552-8

.375

.875

1.01

34-16

1.59

.368

520-IOD

2.062

1.12

1.234

552-10

1.000

1.15

7/a-14

3.26

.461

MS286-1

882-12 MS28761.12

3.46

1.67

.569

520-12D

2.290

1.31

1.484

552-12

.577

1.250

1.45

1%As-12

1.83

.856

520-16D

2.810

1.62

1.765

552-16

1.500

1.74

136-12

4.13

.812

MS28;61-16

PART NO.

/16-20

Ae'-18'

2876_-8

MS28761I16

Choose assembly base nutnber

for desired style.

Fitting A

Fitting B Type

Material

FITTING A Part No.

Page

ASSEMBLY Base No.

FITTING B Part No.

Page

Alum. Unsleeved

and Steel

882

309000

882

AE102

Alum. and Steel

882

620206

882

and

882

309017

980628

Alum. and

882

620207

980628

882

309019

980629

882

620208

980629

980628

309070

980628

and

980628

620209

980628

Unsleeved

Alum. and Steel

980628

309071

980629

AE:102 Firesleeve

Alum. and

980628

620210

980629

Unsleeved

Alum. and Steel

980629

309072

980629

AE102 Fireseeve

Alum. Steel

Firesleeve

Unsleeved

Alum. Steel

AE102 Firesleeve ___________________________________________Steel

Alum. Unsleeved

and

SteelI

L________

F~E102

Firesleeve

*Unsleeved

Alum. and

Steel Alum. and

Steel

AE102

Firesleeve

Alum.

____________________________________________Steel

_______________________________________________SteelI

HOSE FITTING

882 Straight Fitting

D max.

(MS28761)

Hose Size I.D.

Max. Dim. A

882-4

.625

.219

2.25

.98

.83

.104

882-6

.766

.344

2.65

1.17

.95

.161

882-8 88210

.859 1.031

.438 .562

3.01 3.26

1.33 1.59

1.03 1.23

.236 .368

882-12

1.219

.688

3.46

1.67

1.48

.569

4.13

1.83

1.76

.856

Part No.

Material and finish:

Nut and nipple, cadmium-plated steel; socket, anodized aluminum.All materials and finishes conform to applicable specifications for end fittings used in aircraft fluid systems.

Max. Dim. D

Hose Size O.D.

1.500

882-16

.875

Dim. B

Weight (Ibs.)

980628

450 Fitting

Material and finish: Cadmium plated steel seamless tubing and bar stock except socket which is anodized aluminum alloy bar stock. Materials and finishes conform to applicable specifications for end fittings used in aircraft fluid systems.

980628-4

.625

.219

2.49

1.20

.83

.114

980628-6 980628-8

.766 .859

.344 .438

2.92 3.30

1.43 1.61

.95 1.03

.165 .252

980628-10 980628-12

1.031 1.219

.562 688 .

3.56 4.24

1.88 2.43

.366 .596

980628-16

1.500

.875

4.95

2.65

1.23 1.48 . 1.76

.885

980629

900 Fitting

Dmax.

___

980629-4

.625

.219

2.26

.97

.83

.116

980629-6 980629-8

.766 .859

.344 .438

2.64 2.99

1.14 1.29

.95 1.03

.170 .261

98062910 980629-12

1.031 1.219

.562 .688

3.20 4.05

1.52 2.24

1.23 1.48

.390 .641

980629-16

1.500

.875

4.82

2.52

1.76

.950

NIPPLE

SOCKET

NUT T threod UNJF closs3B

H(I.D,)

>$hx

G~~~~~~~~~~~~~~~~~~~~~~

hen.

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

Dim. E

Min. Dim. H

Dim. R

5524

.156

508-4D

552-6

.281

508-6D

552-8

.375

552-10

.461

552-12

.577

552-16

.812

Part No.

Dim. G

Max. Dim. K

1.495

.75

1.750

520-8D

Dim. M

Max. Dim. N

.83

.56

.65

'A7h20

.83

.95

.69

.80

9h6-18

1.975

.94

1.03

.88

1.01

3/4 .16

520-10D

2.062

1.12

1.23

1.00

1.16

7/8-14

520-12D

2.290

1.31

1.48

1.25

1.45

146-12

520-16D

2.810

1.62

1.76

1.50

1.74

1Y6-12

Dim. F

Part No.

Thread T

T thread i -_-

.!-................... F

-i

UNJF class 3B

H(I.D.)-- .:

R rr dius/

Mh. (K=distoncnocrosscorners)

(N =distonce across corners)

985628-4

.452

.127

.38

508-4D

1.495

.75

.83

985628-6

.578

.240

.50

508-6D

1.750

.83

985628-8

.610

.320

.50

520-8D

1.975

985628-10

.725

.397

.62

520-1OD

985628-12

.919

.509

1.25

985628-16

1.010

.710

1.50

.56

.65

7/,6-20

.95

.69

.80

.94

1.03

.88

1.01

3/4 -16

2.062

1.12

1.23

1.00

1.16

/e -14

520-12D

2.290

1.31

1.48

1.25

1.45

11/16-12

520-16D

2.810

1.62

1.76

1.50

1.74

lVY6-12

Is H(I.D.)

thred

14Fcos3

R rradius

|ij|hx

E~~~~~~~~~~~~Kd~.

985629-4

A6-18

.859

.127

.38

-r,

508-4D

1.495

wr-

.75

(N=distcmce across corners)

.83

.56

.65

7 9

Ar6-20

985629-6

1.111

.240

.50

508-6D

1.750

.83

.95

.69

.80

985629-8

1.156

.320

.50

520-8D

1.975

.94

1.03

.88

1.01

3/4

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

/16-18 -16

--- w~~~~~~~~~~

.**Ia @ .

E S

Choose assembly base number

!* .

Fitting B

Fitting A

. I .

Type

Material

FITTING A Part No.

Page

ASSEMBLY Base No.

FITTING B Part No.

Page

Alum.

491

360

491

Alum.

451

390A

451

Steel

491

350

491

Unsleeved

miii ]

desired style.

|for

AE102 Firesleeve

58 58

620001 620000

491 or 451 491 or 451

58 58

Alum.

491 or 451

950012

980006

Steel

491 or 451

950012

980006

___. AE102 Firesleeve

Alum. Steel

491 or 451 491 or 451

58 58

620003 620002

980006 980006

58 58

Alum.

491 or 451

950004

980005

Steel

491 or 451

950004

980005

Alum. Steel

491 or451 491 or 451

58 58

620007 620006

980005 980005

58 58

Alum

980006

950010

980006

Steel

980006

950816

980006

Alum. Steel

980006 980006

58 58

620011 620010

980006 980006

58 58

980006

950003

980005

Steel

980006

950668

980005

Alum. Steel

980006 980006

58 58

620015 620014

980005 980005

58 58

Alum.

980005

950002

980005

950680 ~~~~Steel 58 980005 ~~~~~~ ~~~~~~~

980005

620019 620018

980005 980005

58 5

Unsleeved

*___________________________

AE102 Firesleeve Unsleeved

AE1O2 Firesleeve

%IIII3L_

Alum.

~~~~~~~~~~~~U _

____

Unsleeved

AE102 Firesleeve

,__

491 or 451 491 or 451

EmIL]LI7in__

Alum. Steel

Unsleeved

nsleeved _

980005 AE102~~~~Alum. 980005 Steel ~~~~~~~~~~~~~~Firesleeve

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

58 58

Choose assembly base number for desired style.

Fitting A

Fitting B Material

FITTING A Part No.

Page

ASSEMBLY Base No.

FITTING B Part No.

Page

Alum.

491

360

491

Alum.

451

390A

451

Steel

491

350

491

Alum. Steel

491 or 451 491 or 451

620001

491 or 451

620000

491 or 451

Alum.

491 or 451

950234

980136

Steel

491 or 451

950234

980136

Alum. Steel

491 or 451 491 or 451

620005

980136

620004

980136

Alum.

491 or 451

950192

980137

Steel

491 or 451

950192

980137

Alum. Steel

491 or 451

620009

980137

491 or 451

620008

980137

980136

950247

980136

Steel _

980136

950817

980136

Alum. Steel

980136

620013

980136

620012

980136

Alum.

980136

950233

980137

Steel

980136

950818

980137

Alum. Steel

980136

620017

980137

980136

620016

980137

Alum.

980137

950248

980137

Steel

980137

950819

980137

0 AEI2 Alum. Firesleeve Steel

980137

620021

980137

620020

980137

Type

Unsleeved

AE102 Firesleeve

Unsleeved

AE102 Firesleeve Unsleeved

:AE102 Firesleeve

Alum. Unsleeved

AE102 Firesleeve

Unsleeved_

AE102 Firesleeve

~~~~~~~~~~Unsleeved_

HOSE FITTING

_~~~~~

491 Straight Fitting (MS24587) Hose Size O.D.

Hose Size I.D.

Max. Dim. A

Dim. B

Dim. C

Max. Dim. D

Weight (lbs.)

491-3

.453

.125

1.43

.65

.32

.63

.034

491.4

.516

.188

1.51

.65.

.35

.69

.055

491-5

.578

.250

1.64

.74

.38

.76

.071

491-6 491-8D

.672 .766

.313 .406

1.79 2.22

.77 .94

.38 .43

.88 1.00

.096 .097

1.0

1.3

.922 1.078

.500 .625

2.42 2.70

1.00 1.00

.51

I1.23

.57

1.36

Part No. Material and finish: Nut and nipple sizes -3, -4, -5 and -6 are cadmium-plated steel bar stock. Sizes -8 and up and sockets are anodized aluminum alloy bar stock. Materials and finishes conform to applicable specifica-

tions for end fittings used in aircraft f I u i d syste ms. fluid systems.

49IO92

~~~~~~491 -10D 491-12D

.135 l .185

B-

980006

450

Fitting

">'IC

Dmox

(MS27226)

Material and finish: Nut and nipple sizes .4, -5 and -6 are cadmium-plated steel seamless tubing and bar stock. Sizes -8 and up and sockets are anodized aluminum alloy seamless tubing and bar stock. Materials andfinishesconformtoapplicablespecifications for end fittings used in aircraft

fluid systems.

980006-4

.516

.188

1.99

1.12

.37

.69

.069

980006-5

.578

.250

2.24

1.34

.38

.76

.094

980006-6

.672

.313

2.40

1.38

.38

.88

.126

980006-8D

.766

.406

2.82

1.55

.44

1.00

.110

980006-10D

.922

.500

3.11

1.70

.50

1.23

.159

.188

1.86

.99

.37

.69

.072

0 moz.

980005 900

Fitting

(MS27224)

Material and finish: Nut and nipple sizes -4, -5 and -6 are cadmium-plated steel seamless tubing and bar stock. Sizes -8 and up and sockets are anodized aluminum alloy seamless tubing and bar stock. Materials andfinishesconformtoapplicablespecifications for end fittings used in aircraft fluid systems.

980005-4

.516 _

980005-5

.578

.250

2.08

1.18

.38

.76

.098

980005-6

.672

.313

2.25

1.23

.38

.88

.131

980005-8D

.766

.406

2.66

1.39

.44

1.00

.113

980005-1OD

*.922

.500

2.94

1.52

.50

1.23

.164

All dimensions in inches.

NUT

SOCKET

NIPPLE

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

137

(N=distance across corners)

(K =distanceecross corners)

Part No.

251-3

Dim. E

Min. Dim. H

Dim. R

.123

UNF class3B

Part No.

Dim. F

Dim. G

Max. Dim. K

210.3D

1.000

.562

.630

Part No.

Dim. M

Max. Dim. N

290-3

.438

.51

Thread T

3/a-24 7

251-4

.170

210-4D

1.100

.625

.693

290-4

.563

.65

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

271-10D

.484

215-10D

1.800

1.125

1.234

290-10D

1.000

1.16

271-12D

.608

215-12D

2.100

1.250

1.359

290.12D

1.250

1.45

/16-20

/4-16

/8-14

1YE6-12

T thread UNJF class 3B -

( )U_ E

O--

----

RKrclla(K dst a

M hex.

crosscorners)

(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

Â˝/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) H(l.D.)

UNJF class 3B

sfl>G >

M hex.

hex

-J

R rasdius (K distoncea

ras a an )

(N=distonce across corners)

985005.4

.718

.123

.375

210-4D

1.100

.625

.693

.562

.65

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

1126

.450

.625

215-10D

1.800

1.125

1.234

1.000

1.16

a-14

985005-10D

46-20

nNut is wired-orn and cannot be detached from nipple

HOSE FITTING I

451 Straight Fitting

r~~~~Bj

D max.

(MS24587) Hose Size O.D.

Hose Size I.D.

Max. Dim. A

Dim. B

Dim. C

Max. Dim. D

Weight (lbs.)

451-16D

1.234

.875

2.34

.94

.60

1.55

.220

451-20D

1.500

1.125

2.48

1.00

.64

1.92

.422

Part No.

Material and finish:

Manodize andufinish: alloybarstock. Anodized aluminum alloy bar stock. Sockets sizes -24 and up are anodized aluminum alloy forgings. Materials and finishes conform to applicable specifications for end fittings used in aircraft fluid systems.

980136

450 Fitting

______

___

451-24D

1.750

1.375

2.67

1.09

.74

2.12

.504

451-32D

2.219

1.812

3.21

1.24

.93

2.64

.850

451-40D

2.875

2.375

3.48

1.45

.80

3.39

1.322

(MS27226)

Material and finish:

980136-12D

1.078

.625

3.58

1.89

.57

1.36

.220

Anodized aluminum alloy seamless tubing and bar stock. Sockets sizes -24 and -32 are anodized aluminum alloy forgings. Materials and finishes conform to applicable specifications for end fit-

980136-16D

1.234

.875

3.23

1.84

.63

1.55

.249

980136-20D

1.500

1.125

3.64

2.16

.64

1.92

.469

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

(MS27224)

Material and finish:

980137-12D

1.078

.625

3.46

1.76

.57

1.36

.226

Anodized aluminum alloy seamless tubing and bar stock. Sockets sizes -24 and -32 are anodized aluminum alloy forgings. Materials and finishes conform to applicable specifications for end fit-

980137-16D

1.234

.875

3.14

1.75

.63

1.55

.261

980137-20D

1.500

1.125

3.57

2.09

.64

1.92

.491

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

All dimensions in inches.

NIPPLE

SOCKET

NUT

Z370

UNF class 39

(K=disconc.

Part No.

Dim. E

Min. Dim. H

Dim. R

ac..

(N=distonce across corners)

Part No.

Dim. F

Dim. G

Max. Dim. K

Part No.

Dim. M

Max. Dim. N

Thread T

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

1.921

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

-12

T thread UNJF class 38 H(l.D.)

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

1.921

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 thread UNJF class 38

/I R radius /

(K_-ditanceacros

E7TheM hex.

corcrs)

(N=distance across corners)

985137-12D

1.376

.576

.844

215-12D

2.100

1.250

1.359

985137-16D

1.500

.810

.969

212-16D

1.661

1.438

985137-20D

1.782

1.042

1.188

212-20D

1.750

985137-24D

2.032

1,276

1.375

212-24D

985137-32D

2.532

1.745

1.750

212-32D

1.250

1.447

|Y1%-12

1.546

1.500

1.736

1l 16-12

1.750

1.921

2.000

2.328

1 %-12

1.845

1.938

2.124

2.250

2.621

1 Ys-12

2.250

2.438

2.640

2.875

3.343

2 h-12

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

Globeseal flareless

Assemblies, see page 66

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 marking consisting of- 8794, size, date of manufacture (quarter year/year) and hose manufacturer's code." Spaced 90° from this is a yellow indicator stripe interspersed with "Aeroquip 303" or "Aeroquip 302A." Markings repeated nine inches apart. Application: Medium pressure hydraulic, pneumatic, fuel, oil and coolant systems. Hose conforms to MIL-H-8794. Fittings conform to MIL-A-5070. Hose may be used in submerged applications.

Construction:eamiess synthetic Inner tube: seamless synthetic rubber compound. Reinforcement: synthetic-impregnated single wire braid over single cotton braid. Outer cover: synthetic impregnated oil-resistant cotton braid.

COMPLETE ASSEMBLY Tube size 0.D.

PART NO.

950532-4-L 950532-5-L

Yc 5

950532-6-L

HOSE

Weight 12" ass'y (lbs.)

PART NO. I.D.

Hose size

Hose size 0.D.

Max. oper. P.S.I.

Min. proof P.S.l.

Min. burst P.S.l.

Min bend radii'

Weight per inch (Ibs.)

.247

303I.4

.188

.516

3000

6000

12000

3.00

.011

.291

303-5

.250

.578

3000

5000

10000

3.38

.013

.430

303I-6

.313

.672

2000

4500

9000

4.00

.019

303- 8

.406

.766

2000

4000

8000

4.62

.022

950532-BDL

1/2

.440

950532-1ODL

.615

303-10 MIL-H-8794-10

500

.922

1750

3500

7000

5.50

.031

950532-12DL

.788

303-12 MIL.H-8794-12

.625

1.078

1500

3000

6000

6.50

.038

MIL-H-8794316

875

1.234

800

1600

3200

7.38

.037

950532-16DL

.897

950532-20DL

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

2Length of Assembly

I~~~~~~

To mate with MS33514, MS33515

A~~~~G hex.

istance across corners)

(K-distance aunts corerns)

Material and finish: Nut and nipple, sizes 4 through 6, cadmium-plated steel. Nut and nipple, sizes 8 up, and socket, anodized aluminum. All materials and finishes conform to applicable specifications for end fittings used in aircraft fluid systems.

210, 215 SOCKET

flyMOM24 2 440~ ~~ 440( HOSE FITTING I

lm}GT shreOd J cla Fi

~ ~ ~~~~~ .L.

H(I.D.)

M hex. (N=distance across corners) 440-3-SIZE NIPPLE ASSEMBLY

HOSE FITTING

SOCKET

(Globeseal)

PART NO.

Max. Dim. A

Dim. B

Weight (Ibs.)

440-4

1.78

.94

.068

440-5

1.92

1.05

440-6

2.11

440-8D

NIPPLE ASSEMBLY (Globeseal) Min. PART NO. Dim. H

Dim. F

Dim. G

Max. Dim. K

210-4D

1.100

.625

.693

440-3-4

.170

.081

210-SD

1.200

.688

.755

440-3-5

1.11

.122

210.6D

1.300

.812

.880

2.58

1.33

.117

215-SD

1.650

.938

440-IOD

2.84

1.46

.167

215-10D

1.800

440-12D

3.14

1.47

.222

215-12D

440-16D

2.97

1.60

.286

440-20D

3.17

1.72

440-24D

3.49

1.94

All dimensions in inches.

Max. Dim. N

Thread T

.562

.65

7/16-20

.232

.625

.72

1/2-20

440-3-6

.295

.688

.80

9/16- 18

1.005

440-3-SD

.390

.875

1.01

3/4-16

1.125

1.234

440-3-1OD

.484

1.000

1.16

3s-14

2.100

1.250

1.359

440-3-12D

.608

1.250

1.45

11ie-12

212-16D

1.661

1.438

1.546

440-3-16D

.810

1.500

1.74

1516-12

.503

212-20D

1.750

1.921

440-3-20D

1.042

2.000

2.33

1%-12

.606

212-24D

1.845

1.938

2.124

440-3-24D

1.276

2.250

2.62

1Ya-12

PART NO.

Dim. M

Choose assembly base number for desired style.

Fitting A

Fitting B Type

Material

FITTING A Part No.

Page

ASSEMBLY Base No.

FITTING B Part No.

Page

Unsleeved

Alum.

440

950532

440

-r Steel

440

950532

440

AE102

Alum.

440

620053

440

Firesleeve

Steel

440

620052

440

68 68

Alum.

440

950781

980688

Steel

440

950781

980688

AE102

Alum.

440

620055

980688

Firesleeve

Steel

440

620054

980688

Alum.

440

950645

980569

Steel

440

950645

980569

Alum. Steel

440 440

68 68

620057 620056

980569 980569

68 68

Alum.

980688

950785

980688

Steel

980688

950782

980688

Alum. Steel

980688 980688

68 68

620059 620058

980688 980688

68 68

Alum.

980688

950786

980569

Steel

980688

950783

980569

Alum. Steel

980688 980688

68 68

620061 620060

980569 980569

68 68

Alum.

980569

950787

980569

Steel w

980569

950784

980569

68 -

Alum. Steel

980569 980569

68 68

620063 620062

980569 980569

68 68

_________

Un sleeved

AE102 Firesleeve

Unsleeved

AE102 Firesleeve

Unsleeved

AE102 Firesleeve Unsleeved

AE102 Firesleeve

_=_

440

HOSE FITTING

Straight Fitting

Hose Size O.D. .516

Hose Size ID. .188

Max. Dim. A 1.78

Dim. B .94

Max. Dim. D .69

Weight (lbs.) .068

.578 .672 .766

.250 .313 .406

1.92 2.11 2.58

1.05 1.11 1.33

.76 .88 1.00

.081 .112 .117

440-10D 440-12D

.922 1.078

.500 .625

2.84 3.14

1.46 1.47

1.23 1.40

.167 .222

440-16D 440-20D

1.234 1.500

.875 1.125

2.97 3.17

1.62 1.72

1.68 2.22

.286 .503

440.24D

1.750

1.375

3.49

1.94

2.62

.606

Part No. 440-4 Material and finish: Nut and nipple sizes -4, -5 and -6 are cadmium-plated steel bar stock. Sizes

440-5 440-6 440.8D

-8 and up and sockets are anodized

aluminum alloy bar stock except -24 socket is anodized aluminum alloy forging. Materials and finishes conform to applicable specifications for end fittings used in aircraft fluid systems.

A~~

980688 450 Fitting

Material and finish: Anodized aluminum alloy seamless tubing and bar stock. Materials and finishes conform to applicable specifications for end fittings used in aircraftfluid systems.

980569

900 Fitting

Material and finish: Anodized aluminum alloy seamless tubing and bar stock. Materials and finishes conform to applicable specifications for end fittings used in aircraftfluid systems.

D [max.

980688-4

.516

.188

2.09

1.22

.69

.039

980688-5

.578

.250

2.35

1.45

.76

.050

980688-6 980688-8D

.672 .766

.313 .406

2.53 2.98

1.51 1.71

.88 1.00

.071 .114

980688-l0D 980688-12D

.922 1.078

.500 .625

3.29 4.05

1.88 2.36

1.23 1.36

.165 .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

980569-4

.516

1.86

.578 .672 .766 .

2.08 2.25 2.66

.99 1.18 1.23 1.39

.69 .76 .88 1.00

.039

980569.5

.188 .250 .313 .406

.052 .072 .117

D max

980569-6 980569-8D 980569-12D

1.078

.625

3.86

2.17

1.36

.236

980569-16D

1.234

.875

3.67

2.28

1.55

.276

980569-20D

1.500

1.125

3.88

2.40

1.92

.523

NIPPLE

SOCKET

NUT T thread SG

UNJFh dss 31

~~~~~~~~~~~M~Mhe.. (N=distonce across corners)

Dim. E

Part No. 440-3-4

Min. Dim. H .170

Dim. R -

Part No. 210-4D

Dim. F 1.100

Dim. G .62

Max. Dim. K .69

1.200

.69

.76

Part No. .

Dim. M .56

Max. Dim. N .65

.62

.72

Thread T 7h6-20

440-3-5

.232

210-5D

440-3-6

.295

210-6D

1.300

.81

.88

.69

.80

440-3-8D

.390

215-8D

1.650

.94

1.00

.88

1.01

440-3-10D

.484

215-lOD

1.800

1.12

1.23

1.00

1.16

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

440-3-20D

1.042

212-20D

1.750

1.75

1.92

1.276

212-24D

1.845

1.94

2.12

440-3-24D

Â˝/2-20 9

Ae-18 /4-16

Y- 14

1.50

1.74

P4/6-12

2.00

2.31

1%-12

2.25

2.62

1%8-12

T thread UNJF clans 31 H(I.D.)

E R rodius

hGe.i

~~~~~~~~~~~(K=60-1.c

985688-4

.452

.123

.38

210-4

1.100

.62

.69

985688-5

.525

.170

.44

210-5

1.200

.69

.76

985688-6

.578

.232

.50

210-6

1.300

.81

985688-8D

.610

.355

.50

215-8D

1.650

985688-10D

.725

.450

.62

215-10D

985688-12D

.800

.576

1.25

985688-16D

.855

.810

985688-20D

.962

1.042

(Ncdiv- . ..... co,.,, (N -disronceacross corners)

.56

.65

.62

.72

1/2-20

.88

.69

.80

9/16-18

.94

1.00

.88

1.01

3/4-16

1.800

1.12

1.23

1.00

1.16

215-12D

2.100

1.25

1.36

1.25

1.45

l /16-12

1.50

212-16D

1.661

1.44

1.55

1.50

1.74

l 5A6-12

1.50

212-20D

1.750

1.75

1.92

2.00

2.31

H(l D.)

Y-14 1

1%-12

T thread UNJF cloC 38

F------

~~~~Ohen.

, EG

R roedius

l0l~

h... ziM

~~~~~~~~~~~~(K=d oonce acrosscorners)

7h6-20

(N=dsrtonce across corners)

*i __

985569-4

.860

.123

.38

210-4

1.100

.62

.69

985569-5 985569-6

.1.000

.170

.44

1.200

.69

.76

1.112

.232

.50

210-5 210-6

1.300

.81

.88

.69

985569-8D

1.156

.355

.50

215-81D

1.650

.94

1.00

.88

1.01

985569-10D

1.392 1

.450

.62

215-10D

1.800

1.12

1.23

1.00

1.16

985569-12D

1.626

.576

1.25

215-12D

2.100

1.25

1.36

1.25

1.45

1lff-12

985569-16D 985569-20D

1.776 2.057

.810 1.042

1.50 1.50

212-16D 212-20D

1.661 | 1.750

1.44 1.75

1.55 1.92

1.50

1.74

P e-12

2.60

2-31

1-12

.56

.65

.62

.72 .80 |

7/16-20 1/2-20 9

6-18

A-16

Y/e-14

'Nut is wired-on and cannot be detached from

nipple.