Quadrant Control Assembly
1680-01-655-5251, Quadrant Control Assembly, 251T1602-18
DAC | HCC | DMIL | RNCC |
---|---|---|---|
D | - | - | 3 |
RNVC | SADC | MSDS | RNAAC |
---|---|---|---|
1 | - | - | ZZ |
A cockpit mounted, manually operated item, designed to regulate aircraft functions, which may include throttle, afterburner, flaps, trim tabs, and the like. May consist of lever(s), grip(s), switch(es), and fulcrum(s). Excludes:wire rope and push-pull assemblies, and all quadrants or levers that are engine mounted.
INC | FIIG | Concept | Condition |
---|---|---|---|
39947 | A529V0 | - | 1 |
HMIC | PMIC | ESD/EMI | Criticality |
---|---|---|---|
N | A | A | - |
UFC | HMC | LTL | LCL |
---|---|---|---|
- | - | - | - |
RVC | WCC | TCC | SHC |
---|---|---|---|
- | - | - | - |
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