Aircraft Universal Joint
1680-01-655-7886, Aircraft Universal Joint, AE77832V
| DAC | HCC | DMIL | RNCC |
|---|---|---|---|
| D | - | - | 3 |
| RNVC | SADC | MSDS | RNAAC |
|---|---|---|---|
| 1 | - | - | ZZ |
A flexible connection designed for aircraft applications which permits rotary motion to be transmitted between two shafts located at an angle to each other. The angle between the shafts may be continually varied within certain limits; the connecting ends must have either a flange, hub, or splined stub shaft; the plain portion of a splined stub shaft must not exceed the length of the splines. Excludes:drive or propeller shafts with joint(s) at one or both ends. See universal joint,geared.
| INC | FIIG | Concept | Condition |
|---|---|---|---|
| 52077 | A521W0 | - | 1 |
| HMIC | PMIC | ESD/EMI | Criticality |
|---|---|---|---|
| N | A | A | - |
| UFC | HMC | LTL | LCL |
|---|---|---|---|
| 64100 | - | M | - |
| RVC | WCC | TCC | SHC |
|---|---|---|---|
| - | 671 | Z | 9 |
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