MS51928 Clip, Spring Tension

Pages 1 - 2

MS51928C

TABLE I. Part Numbers and Dimensions.

PART NUMBER	TUBE OR WIRE SIZE	0A	B	C	D	E	G ±.010
MS51928-1	.188 (3/16)	.16	.14	.56	.19	.88	.025
MS51928-2 *	.250 (1/4)	.23	.19	.72	.23	.88	.025
MS51928-3	.312 (5/16)	.30	.25	.64	.22	.88	.037
MS51928-4	.375 (3/8)	.36	.30	.62	.19	.88	.037
MS51928-5	.438 (7/16)	.41	.34	.59	.22	.88	.037
MS51928-6 *	.438 (7/16)	.41	.33	.59	.91	1.55	.037
MS51928-7 *	.531 (17/32)	.52	.41	.69	.22	.97	.037
MS51928-8	.625 (5/8)	.56	.50	.72	.19	.88	.037
MS51928-9 *	.750 (3/4)	.73	.56	.88	.19	1.06	.037
MS51928-10	.500 (1/2) TO .875 (7/8)	.52	.22	1.66	.00	1.50	.037

* No longer manufactured

TABLE II. Mounting Hole Dimensions.

MATERIAL THICKNESS	HOLE SIZE
.031 to .078	.250
.093 to .172	.281
.188 to .219	.297

Notes:

1. Material: Steel, carbon, SAE 1050 in accordance with SAE AIR4127, spring tempered to a hardness of Rockwell C37-45.

2. Protective coating: Zinc plated in accordance with ASTM B633, Type II, Fe/Zn 13.

3. Unless otherwise specified, all dimensions are in inches.

4. Tolerance: Unless otherwise specified, tolerance shall be ±.03.

5. For design feature purposes, this standard takes precedence over procurement documents referenced herein.

6. Illustrations are for identification and are not intended to restrict the design or shapes not dimensioned.

7. Changes from 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.

Custodians: Preparing Activity: Army - AR DLA - IS

Navy - YD

Air Force - 99 (Project 5340-2009-028)

Review activities:

Army - AT, CR, CR4

Navy - CG, SA Air Force - 71

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.daps.dla.mil.