Fastening Devices: MS3217-4098, MS3217-4193, MS35489-1

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
MS3217-4098
MS32174098
5325-01-128-5300Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4118
MS32174118
5325-01-480-0737Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4125
MS32174125
5325-00-404-2661Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4137
MS32174137
5325-00-488-4860Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4150
MS32174150
5325-01-124-0179Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4156
MS32174156
5325-01-062-3607Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4175
MS32174175
5325-00-216-1117Ring, RetainingMaterial: Cres ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4193
MS32174193
5325-00-075-3211Ring, RetainingMaterial: Cres, std data, any acceptable
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3217-4200
MS32174200
5325-01-539-1631Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A1 straight gap
Cross-Sectional Shape Style: D1 round
Military Standards (96906)

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MS3217B-4156
MS3217B4156
5325-01-062-3607Ring, RetainingMaterial: Steel, ams 5520
Ring Style: A41 external
Usage Design: External
Military Standards (96906)

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MS3280 5325-01-559-7444Insert, Screw ThreadMaterial: Steel corrosion resisting overall
Surface Treatment: Oxide film overall
III End Item Identification: 1025-01-445-0991, 155MM howitzer, medium, towed
Society of Automotive Engineers Inc. (81343)

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MS33537 5325-01-557-9667Insert, Screw ThreadIII Part Name Assigned By Controlling Agency: Insert, screw thread, helical coil
Military Standards (96906)

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MS345489-099
MS345489099
5325-01-560-9815Grommet, NonmetallicMaterial: Rubber synthetic overall
Color: Black overall
Flange Thickness: 0.089 inches nominal
Military Standards (96906)

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MS345489-6
MS3454896
5325-00-263-6632Grommet, NonmetallicHole Diameter: 0.250 inches nominal
Groove Width: 0.062 inches nominal
Flange Thickness: 0.062 inches nominal
Bosch Rexroth GMBH Lohmann (D9182)

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MS3498-1
MS34981
5325-00-817-0510Grommet, MetallicMaterial: Aluminum alloy overall
Surface Treatment: Anodize overall
Color: Any acceptable overall
National Aerospace Standards (80205)

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MS3498-1
MS34981
5325-01-009-7353Stud Assembly, Turnlock FastenerMaterial: Aluminum alloy 2011 barrel aluminum alloy 2011 grommet steel corrosion resisting stud
Surface Treatment: Anodize overall
Material Document and Classification: Ams 5640 assn std single material response stud
Military Standards (96906)

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MS3498-3
MS34983
5325-01-190-7737Insert, Screw ThreadSurface Treatment: Anodize overall
Length: 0.174 inches minimum and 0.184 inches maximum
Surface Treatment Document and Classification: MIL-A-8625 mil spec single treatment response overall
Military Standards (96906)
National Aerospace Standards (80205)

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MS35439-9
MS354399
5325-00-276-6228Grommet, NonmetallicMaterial: Rubber synthetic overall
Material Document AND Classification: Astm D2000 BG515A14B24C32E036F19Z assn std single material response overall
Color: Black overall
Bosch Rexroth GMBH Lohmann (D9182)

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MS35489 5325-00-276-6059Grommet, NonmetallicHole Diameter: 1.234 inches minimum and 1.266 inches maximum
Groove Width: 0.109 inches minimum and 0.141 inches maximum
Flange Thickness: 0.188 inches nominal
Military Standards (96906)

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MS35489-007
MS35489007
5325-01-177-0959Grommet, NonmetallicMaterial: Rubber synthetic overall
Material Document and Classification: MIL-G-3036, composition a mil spec single material response overall
Color: Black overall
Military Standards (96906)

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MS35489-1
MS354891
5325-01-413-5574Grommet, NonmetallicNonmetallic Hardness Rating: 45.0 nominal shore durometer a and 55.0 minimum shore durometer a
Hole Diameter: 0.125 inches nominal
Groove Width: 0.062 inches nominal
Military Standards (96906)
National Aerospace Standards (80205)

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