MIL-R-6106/140
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. 0imensions 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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