Aircraft Gas Tur Compressor Vane
5026T38P01
2840-00-001-9579, Aircraft Gas Tur Compressor Vane, 5026T38P01
DAC | HCC | DMIL | RNCC |
---|---|---|---|
5 | - | - | 3 |
RNVC | SADC | MSDS | RNAAC |
---|---|---|---|
2 | - | - | KE |
A component of a vane assembly, compressor, aircraft gas turbine engine. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.
INC | FIIG | Concept | Condition |
---|---|---|---|
50611 | A10700 | - | 1 |
HMIC | PMIC | ESD/EMI | Criticality |
---|---|---|---|
N | A | - | - |
UFC | HMC | LTL | LCL |
---|---|---|---|
04720 | - | W | - |
RVC | WCC | TCC | SHC |
---|---|---|---|
- | 671 | Z | 9 |
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