Universal Joints
Airframe-Parts_Universal-Joints
Built to conform with and exceed all requirements stipulated in Spec. MIL-J-6193A. High axial and torsional strengths, high strength-weight ratio, no replacement during anticipated service life of aircraft on most installations, permanent lubrication.
Temporary torsional overloads as great as 80% of rated ultimate have been handled by these universal joints without harmful binding. Temporary axial overloads ranging up to 150% in excess of rated ultimates have been imposed without binding. These characteristics insure high safety factors under the most difficult operating conditions.
Part No. |
Nominal
Size. |
ØD
+0.000
- 0.002
in. |
L1
Overall
Length
in. |
L3
+0.031
- 0.000
in. |
ØB
+0.004
- 0.001
in.
|
L4
Insp. Hole Location
in.
|
Weight
Max. Lbs.
|
| MS20271-B6 |
3/8” |
0.372 |
2.000 |
0.500 |
0.250 |
0.437 |
0.070 |
| MS20271-B8 |
1/2” |
0.495 |
2.312 |
0.625 |
0.375 |
0.562 |
0.090 |
| MS20271-B10 |
5/8” |
0.620 |
2.750 |
0.750 |
0.500 |
0.687 |
0.180 |
| MS20271-B12 |
3/4” |
0.745 |
3.187 |
0.875 |
0.625 |
0.812 |
0.240 |
| MS20271-B14 |
7/8” |
0.870 |
3.625 |
1.000 |
0.750 |
0.937 |
0.350 |
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