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Page Title:
Figure 1. Relay, outline drawing - Continued. |
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|  MIL-R-6106/14D
Inches
mm
Inches
mm
Inches
mm
.045
1.14
.30
7.62
1.250
31.75
.055
1.40
.31
7.87
1.300
33.02
.06
1.52
.312
7.92
1.406
35.71
.100
2.54
.32
8.13
1.500
38.10
.170
4.32
.380
9.65
2.000
50.80
.218
5.54
.40
10.16
2.100
53.34
.22
5.59
.500
12.70
2.400
60.96
.224
5.69
.600
15.24
2.750
69.85
.250
6.35
.625
15.88
3.400
86.36
1.200
30.48
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for general information only.
3. Unless otherwise specified, tolerance is .010 (0.25 mm) for three place decimals and .03 (0.8 mm) for two
place decimals.
4. The main contact terminals shall be designed so that two number 6 SAE-AS25036 terminal lugs may be
attached back to back on each terminal without contacting the relay case.
5. Terminal protection: The relay shall have a terminal cover with integral barriers.
6. Reparability: All functional parts shall be capable of being removed and replaced.
7. Shelf life: The unit shall have a shelf life of 5 years, provided that the unit is cycled 25 times at rated inductive
load in accordance with MIL-PRF-6106 before use in the aircraft.
8. Terminal numbers need not appear on relay headers, provided that a legible circuit diagram is affixed to the
relay that positively and permanently identifies each terminal.
9. Coil and auxiliary contact pins shall have equivalent positions to those of MIL-PRF-83536/15, 16, and 17.
FIGURE 1. Relay, outline drawing - Continued.
2
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