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MS20756 REV G

DETAIL SPECIFICATION SHEET

FLANGE, SWIVEL, RETAINING

This specification is approved for use by all Departments and Agencies of the Department of Defense.

The requirements for acquiring the product described herein shall consist of this specification sheet and  SAE-AS4875.

MS20756G Figure 1 drawing of Type I rectangular swivel fitting flange, sizes 8 through 32
Inch to millimeter conversion
Inches mm
.005 0.13
.010 0.25
.062 1.57

FIGURE 1. Swivel fitting flange type I rectangle size 8 through 32.

Dimensional specification data

Size designator

Tubing OD and hose ID inches (mm)

A +.015 -.005 (+0.38 -0.13) inches (mm)

B +.005/-.000 (+0.13/-0.00) inches (mm)

C dia (see note 4) +.010/-.000 (+0.25/-0.00) inches (mm)

D dia (see note 4) +.005/-.000 (+0.13/-0.00) inches (mm)

E (see note 9) inches (mm)

8

.500 (12.70)

.234 (5.94)

.136 (3.45)

.750 (19.05)

.885 (22.48)

1.390 (35.31)

±.016 (0.41)

10

.625 (15.88)

.880 (22.35)

1.010 (25.65)

1.468 (37.29)

12

.750 (19.05)

1.125 (28.58)

1.260 (32.00)

1.594 (40.49)

16

1.000 (25.40)

1.375 (34.93)

1.510 (38.35)

1.750 (44.45)

20

1.250 (31.75)

1.688 (42.88)

1.854 (47.09)

2.188 (55.58)

±.020 (0.51)

24

1.500 (38.10)

.297 (7.54)

.168 (4.27)

1.938 (49.23)

2.135 (54.23)

2.375 (60.33)

32

2.000 (50.80)

2.562 (65.07)

2.760 (70.10)

3.000 (76.20)

Dimensional specification data

Size number

G ±.005 (±0.13) inches (mm)

H dia +.010/-.000 (+0.25 -0.00) inches (mm)

J radius (see note 9) ±.016 (±0.41) inches (mm)

K dia (see note 9) ±.015 (±0.38) inches (mm)

L dia ±.005 (0.25mm) inches (mm)

M ±.016 (±0.41) inches (mm)

N

8

.950 (24.13)

.205 (5.21)

.219 (5.56)

1.782 (45.26)

1.344 (34.14)

.296 (7.52)

20°

10

1.038 (26.37)

1.906 (48.41)

1.468 (37.29)

12

1.156 (29.36)

2.094 (53.19)

1.635 (41.53)

16

1.312 (33.32)

2.312 (58.72)

1.855 (47.12)

18°

20

1.656 (42.06)

.266 (6.76)

.266 (6.76)

2.875 (73.03)

2.342 (59.49)

16°

24

1.812 (46.02)

.281 (7.14)

3.094 (78.59)

2.562 (65.07)

.359 (9.12)

32

2.375 (60.33)

.328 (8.33)

.312 (7.92)

3.953 (100.41)

3.359 (85.32)

12°

FIGURE 1. Swivel fitting flange type I rectangle size 8 through 32 - Continued.

Dimensional specification data

Size number

Weight max (estimated) lbs (gram)

Steel

Al alloy

Titanium

8

.03 (14)

.01 (5)

.02 (9)

10

.05 (23)

.02 (9)

.03 (14)

12

.08 (36)

.03 (14)

.04 (18)

16

20

.14 (64)

.05 (23)

.07 (32)

24

.17 (77)

.06 (27)

.09 (41)

32

.25 (113)

.09 (41)

.13 (59)

NOTES:

  1. Dimensions are in inches.
  2. Metric equivalents are given for information only.
  3. Unless otherwise specified, tolerances linear dimensions ±.005 inch (0.13 mm) angles ±.5°.
  4. Diameters C and D shall be concentric within .010 inch (0.25 mm) full indicator movement.
  5. Unless otherwise specified, the surface roughness shall not exceed 100 microinches (25.4 µm) Ra in accordance with ASME B46.1.
  6. Break all sharp edges; remove all loose or hanging burrs and slivers that may become dislodged.
  7. For tube sizes -8 through -16, maximum operating temperature 275°F (135°C), maximum pressure 1500 psi (10 MPa).
  8. For tube sizes -20 though -32, maximum operating temperature 275°F (135°C), maximum pressure 500  psi (3.4 MPa).
  9. Reduction by forging draft angle of 7° maximum is permissible if forged.

FIGURE 1. Swivel fitting flange type I rectangle size 8 through 32 - Continued.

MS20756G Figure 1 continued, Type I rectangular swivel fitting flange dimensions
Inch to millimeter conversion
Inches mm
.005 0.13
.010 0.25
Dimensional specification data

Size designator

Tubing OD and hose ID inches (mm)

A +.015 -.005 (+0.38 -0.13) inches (mm)

B +.005/-.000 (+0.13/-0.00) inches (mm)

C dia (see note 4) +.010/-.000 (+0.25/-0.00) inches (mm)

D dia (see note 4) +.005/-.000 (+0.13/-0.00) inches (mm)

E (see note 9) inches (mm)

8

.500 (12.70)

.234 (5.94)

.136 (3.45)

.750 (19.05)

.885 (22.48)

1.538 (39.07)

±.016 (0.41)

10

.625 (15.88)

.880 (22.35)

1.010 (25.65)

1.644 (41.76)

12

.750 (19.05)

1.125 (28.58)

1.260 (32.00)

1.813 (46.05)

16

1.000 (25.40)

1.375 (34.93)

1.510 (38.35)

2.000 (50.80)

20

1.250 (31.75)

1.688 (42.88)

1.854 (47.09)

2.460 (62.48)

±.020 (0.51)

24

1.500 (38.10)

.297 (7.54)

.168 (4.27)

1.938 (49.23)

2.135 (54.23)

2.680 (68.07)

32

2.000 (50.80)

2.562 (65.07)

2.760 (70.10)

3.359 (85.32)

40

2.500 (63.50)

3.062 (77.77)

3.291 (83.59)

4.000 (101.60)

48

3.000 (76.20)

3.562 (90.47)

3.791 (96.29)

4.500 (114.30)

FIGURE 2. Swivel fitting flange type II hexagon size 8 through 48.

Dimensional specification data

Size number

H dia +.010/-.000 (+0.25/-0.00) inches (mm)

J radius (see note 9) ±.016 (±0.41) inches (mm)

K dia (see note 9) ±.015 (±0.38) inches (mm)

L dia ±.005 (0.25mm) inches (mm)

8

.205 (5.21)

.219 (5.56)

1.782 (45.26)

1.344 (34.14)

10

1.906 (48.41)

1.468 (37.29)

12

2.094 (53.19)

1.635 (41.53)

16

2.312 (58.72)

1.855 (47.12)

20

.266 (6.76)

.266 (6.76)

2.875 (73.03)

2.342 (59.49)

24

.281 (7.14)

3.094 (78.59)

2.562 (65.07)

32

.328 (8.33)

.312 (7.92)

3.953 (100.41)

3.359 (85.32)

40

.375 (9.53)

4.500 (114.30)

3.812 (96.82)

48

.625 (15.88)

5.000 (127.00)

4.312 (109.52)

Dimensional specification data

Size number

Weight max (estimated) lbs (gram)

Steel

Al alloy

Titanium

8

.03 (14)

.01 (5)

.02 (9)

10

.05 (23)

.02 (9)

.03 (14)

12

.08 (36)

.03 (14)

.04 (18)

16

20

.14 (64)

.05 (23)

.07 (32)

24

.17 (77)

.06 (27)

.09 (41)

32

.25 (113)

.09 (41)

.13 (59)

40

.45 (204)

.16 (73)

.21 (95)

48

.53 (240)

.19 (86)

.24 (109)

NOTES:

  1. Dimensions are in inches.
  2. Metric equivalents are given for information only.
  3. Unless otherwise specified, tolerances linear dimensions ±.005 inch (0.13 mm) angles ±.5°.
  4. Diameters C and D shall be concentric within .010 inch (0.25 mm) full indicator movement.
  5. Unless otherwise specified, the surface roughness shall not exceed 100 microinches (25.4 µm) Ra in accordance with ASME B46.1.
  6. Break all sharp edges; remove all loose or hanging burrs and slivers that may become dislodged.
  7. For tube sizes -8 through -16, maximum operating temperature 275°F (135°C), maximum pressure 1500 psi (10 MPa).
  8. For tube sizes -20 though -48, maximum operating temperature 275°F (135°C), maximum pressure 500  psi (3.4 MPa).
  9. Reduction by forging draft angle of 7° maximum is permissible if forged.

FIGURE 2. Swivel fitting flange type II hexagon size 8 through 48 - Continued.

MS20756G Figure 2 drawing of Type II hexagonal swivel fitting flange, sizes 8 through 48
Inch to millimeter conversion
Inches mm
.005 0.13
.010 0.25
Dimensional specification data

Size number

Tubing OD and hose ID inches (mm)

A +.015/-.005 (+0.38/-(0.13) inches (mm)

B +.005/-.000 (+0.13/-.000) inches (mm)

C dia (see note 4) ±.031 (0.79) inches (mm)

D dia (see note 4) inches (mm)

H dia +.010/-.000 (+0.25/-0.00) inches (mm)

56

3.500 (88.90)

.312 (7.92)

.168 (4.27)

3.968 (100.79)

4.234 (107.54)

+.010/-.000 (+0.25/-0.000)

.328 (8.33)

64

4.000 (101.60)

4.531 (115.09)

4.797 (121.84)

80

5.000 (127.00)

.375 (9.53)

.188 (4.78)

5.531 (140.49)

5.797 (147.24)

96

6.000 (152.40)

6.531 (165.89)

6.797 (172.64)

+.020/-.000 (0.51/-.000)

112

7.000 (177.80)

.437 (11.10)

.200 (5.08)

7.594 (192.89)

7.860 (199.64)

FIGURE 3. Swivel fitting flange type III round size 56 through 112.

Dimensional specification data

Size number

K dia (see note 8) ±.015 (±0.38) inches (mm)

L dia Ref inches (mm)

P number of holes

56

5.562 (141.27)

4.875 (123.83)

8

64

6.125 (155.58)

5.438 (138.13)

80

7.125 (180.98)

6.438 (163.53)

10

96

8.125 (206.38)

7.438 (188.93)

12

112

9.188 (233.38)

8.500 (215.90)

14

NOTES:

  1. Dimensions are in inches.
  2. Metric equivalents are given for information only.
  3. Unless otherwise specified, tolerances linear dimensions ±.005 inch (0.13 mm) angles ±.5°.
  4. Diameters C and D shall be concentric within .010 inch (0.25 mm) full indicator movement.
  5. Unless otherwise specified, the surface roughness shall not exceed 100 microinches (2.54 µm) Ra in accordance with ASME B46.1.
  6. Break all sharp edges; remove all loose or hanging burrs and slivers that may become dislodged.
  7. Maximum operating temperature 275°F (135°C), maximum pressure 500 psi (3.4 MPa).
  8. Reduction by forging draft angle of 7° maximum is permissible if forged.

FIGURE 3. Swivel fitting flange type III round size 56 through 112 - Continued.

REQUIREMENTS

Design and construction: Dimensions and configuration: See figures 1, 2, and 3. For nominal use on fuel and oil systems.

Materials: Materials shall be in accordance with SAE-AS4875.

Material designators (see table I): Designators for material types shall be in accordance with  SAE-AS4875. Material and size designators shall be in accordance with table I.

TABLE I. Material and size designators. 1/

Table I. Material and size designators

Table I. Material and size designators

Size number

Size number with letter material designator

Steel (Blank)

Aluminum alloy

CRES

Titanium 2/

8

-8

-W8

-R8

-T8

10

-10

-W10

-R10

-T10

12

-12

-W12

-R12

-T12

16

-16

-W16

-R16

-T16

20

-20

-W20

-R20

-T20

24

-24

-W24

-R24

-T24

32

-32

-W32

-R32

-T32

40

-40

-W40

-R40

-T40

48

-48

-W48

-R48

-T48

56

-56

-W56

-R56

-T56

64

-64

-W64

-R64

-T64

80

-80

-W80

-R80

-T80

96

-96

-W96

-R96

-T96

112

-112

-W112

-R112

-T112

1/ Materials and designators blank/none, “W”, “R”, and “T” are in accordance with  SAE-AS4875.

2/ Titanium shall not be used in oxygen systems.

Finishes: Finish and finish designators shall be as specified in table II. All plating’s shall be capable of meeting a minimum of 96 hours salt spray test in accordance with ASTM B117. The fittings shall show no evidence of red corrosion after 96 hours of salt spray. Fluid passages, other openings and internal threads shall not be subject to the plating thickness requirement and may have bare areas provided they are protected with a light film of oil.

TABLE II. Flange finish code. 

Table II. Flange finish code

PIN code dash letter

Material

Plating finish

Blank

Steel

Cadmium plating in accordance with SAE-AMS-C-81562, type  II, class 3 or SAE-AMS-QQ-P-416, type II, class 2. 1/

Aluminum 2/

Anodize in accordance with MIL-A-8625, type II.

CRES

No additional finish. Passivation in accordance with SAE-AMS2700, type 6 or 7.

Titanium 3/

Fluoride phosphate in accordance with SAE-AMS2486. 4/

-A

Steel

Aluminum-nickel in accordance with ASTM F1136/F1136M,  grade 3, NC

-D

Aluminum 2/

Anodize in accordance with MIL-A-8625, type II then apply NAVAIR trivalent chromium pretreatment (TCP) in accordance  with MIL-DTL-81706, type II, class 1A.

DA

Aluminum 2/

Chemical conversion coating in accordance with,  MIL-DTL-5541, type II, class 3

-G

Steel

Zinc plating with colorless passivate in accordance with ASTM B633, type V, Fe/Zn 25. 6/

-H

Steel

Zinc phosphate finish in accordance MIL-DTL-16232 type Z,  class 1. 6/

-J

Steel

Zinc plating in accordance with ASTM B633; type II or III, Fe/Zn  5, or ASTM B695, type II, class 5. 6/

-R

Steel

Zinc plating in accordance with ASTM B633; type III or V, Fe/Zn 8. 6/

-T

Titanium 4/

Anodized in accordance with SAE-AMS2488, type 2

-V

Steel

Zinc-nickel in accordance with SAE-AMS2417, type 1. 5/ 6/

-Z

Steel

Zinc plating in accordance with ASTM B695, type II, class 8. 3/ 6/

-ZN

Steel

Zinc may be any zinc plating’s from PIN codes R, V, Z. 6/

1/ Cadmium shall not be used in oxygen or potable water systems. Cadmium is prohibited from use in  NAVSEA owned shipboard systems.

2/ Aluminum alloy 7075 shall be dyed brown.

3/ Titanium shall not be used in oxygen systems.

4/ A pretreatment, a modification of the fluoride treatment, or a post treatment shall be applied so the final color of the fittings shall be similar to SAE-AMS-STD-595 colors 36076 through 36293. Titanium shall not be used in oxygen or potable water systems.

5/ The zinc-nickel alloy plate shall contain 12% to 16% nickel. The coating thickness shall be 315µ inches (8µm) minimum. Hexavalent chromium free. Finish shall be ROHS compliant.

6/ Not for use in Aircraft. Requires approval from the Program Office for all applications. Zinc-plated  materials should be avoided in hydraulic systems with water-glycol fluids. Reference ASTM MNL37 - Fuels and Lubricants Handbook, "water glycol fluids are highly alkaline due to the presence of amine based corrosion inhibitors. As a result, these fluids can attack zinc, cadmium, magnesium, and non anodized aluminum, forming sticky or gummy residues. Consequently, these metals should be avoided when selecting system components."

SPECIAL PROCEDURES & WRENCHABILITY

Trivalent wrenchability: Applies to aluminum fittings that receive the NAVAIR TCP coating in accordance with MIL-DTL-81706, type II. When the finish has been damaged due to poor wrenchability, the surface of the flange shall be touched up using the brush plating process below. The term "trivalent wrenchability" is used to evaluate the ability of the finish to withstand abrasion from an excessive amount of wrenching.

Brush plating: Brush plating of NAVAIR TCP shall be in accordance with MIL-DTL-81706, type 2, class 1A, material form 1 through 6, application method B. Example of a PIN: M817062A6B.

PART IDENTIFICATION NUMBER (PIN) SPECIFICATION

MS 20756 -W12 -D [2]
MS
Military Standard prefix
20756
Specification sheet number
-W12
Material and size designator (see Table I)
-D
Material finish code (see Table II)
“Blank” / “2”
“Blank” for Type I rectangle, Type II hexagon sizes 40 & 48, and round. “2” for Type II hexagon sizes 8 through 32 only.
PIN Examples:
MS20756-W12-D indicates: Flange, .750 inch (19.05 mm) tube ID, aluminum anodized then NAVAIR TCP applied, type I rectangle.
MS20756-W12-D2 indicates: Flange, .750 inch (19.05 mm) tube ID, aluminum anodized with NAVAIR TCP, type II hexagon.
MS20756-56 indicates: Flange, 3.500 inch (88.90 mm) tube ID, steel, cadmium plating in accordance with SAE-AMS-C-81562, type II, class 3 or SAE-AMS-QQ-P-416, type II, class 2, type III round.

GENERAL GUIDANCE & ENVIRONMENTAL REQUIREMENTS

Marking: The complete PIN shall be permanently marked on an unfinished surface.

Guidance on alternative parts: Guidance on use of alternative parts with less hazardous or nonhazardous materials. This specification provides for a number of alternative plating materials via the PIN. Users should select the PIN with the least hazardous material that meets the form, fit and function requirements of their application.

Cadmium prohibition: Cadmium is prohibited from use in NAVSEA owned shipboard systems in accordance with the requirements of T9070-AL-DPC-020/077-2.

Ozone depleting substances: Class I and II ozone depleting substances (ODS) shall not be used in MS20756 or any referenced procedures.

Order of precedence: Referenced documents shall be of the issue in effect on date of invitations for bid. This standard takes precedence over documents referenced herein.

SUPERSESSION & REVISION DATA

Supersession data:

• Aluminum alloys 2014 and 2024 "D" designator is cancelled. For new and existing designs, use aluminum alloy 7075 "W" designator.

• CRES alloy 304 "J" designator is cancelled. For new and existing designs, use CRES alloy 321 "R" designator.

Application: For nominal use on fuel and oil systems.

Previous issue: Marginal notations are not used in this revision to identify changes with respect to the previous issue, due to the extent of the changes.

REFERENCED DOCUMENTS

In addition to SAE-AS4875, this document references the following:

MIL-A-8625 MIL-DTL-5541 MIL-DTL-16232 MIL-DTL-81706 ASME B46.1 ASTM B117 ASTM B633 ASTM B695 ASTM F1136/F1136M ASTM MNL37 SAE-AMS-C-81562 SAE-AMS2417 SAE-AMS2486 SAE-AMS2488 SAE-AMS2700 SAE-AMS-QQ-P-416 T9070-AL-DPC-020/077-2 SAE-AMS-STD-595 Colors (36076, 36081, 36099, 36118, 36134, 36152, 36170, 36173, 36176, 36231, 36251, 36270, 36280, 36293)

CONCLUDING MATERIAL

Custodians

Army – AT

Navy – AS

Air Force – 99

DLA – CC

Preparing Activity

DLA – CC

(Project 4730-2018-042)

Review Activities

Navy – SA

Air Force – 85

NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https://assist.dla.mil.

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