MS18200B
|
Retaining plate designator |
Connector size (number of contacts) |
A ±.005 (0.13 mm) |
B ±.005 (0.13 mm) |
C (mm) |
D (mm) |
E (mm) |
F ±.005 (0.13 mm) |
G (mm) |
H (mm) |
|
MS18200-1 |
66 |
2.984 (75.79) |
1.969 (50.01) |
1.718 (43.64) |
1.125 (28.58) |
1.688 (42.88) |
.500 (12.70) |
.125 (3.18) |
3.296 (83.72) |
|
MS18200-2 |
104 |
3.500 (88.90) |
2.375 (60.33) |
2.125 (53.98) |
1.486 (37.74) |
2.000 (50.80) |
.875 (22.23) |
.150 (3.81) |
3.875 (98.43) |
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for information only.
3. Unless otherwise specified, tolerances are ±.016 inch (0.41 mm).
4. Material aluminum alloy in accordance with SAE AMS4016M, temper H32, .040 inch
(1.02 mm) thick.
5. Finish anodize in accordance with MIL-A-8625, type I or type II.
FIGURE 1. Retaining plate - Continued.
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.
Referenced documents. In addition to MIL-DTL-28748, this document references the following:
MIL-A-8625
SAE AMS4016M
CONCLUDING MATERIAL
Custodians: Preparing activity: Army - CR DLA - CC
Navy - EC
Air Force - 85 (Project 5935-2009-167) DLA - CC
Review activities:
Army - AM, AR, AT, CR4, MI Navy - AS, MC, OS, SH
Air Force - 99
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.
2
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