Aircraft Gas Tu Compressor Rotor
6006T80G20
Acft eng. j-85 end item identification, axial compressor design type, agav criticality code justification, compressor engine section location, with compressor blades for stages 1-9 special features, 2j-j85-54 reference data and literature
| DAC | HCC | DMIL | RNCC |
|---|---|---|---|
| 2 | - | - | 3 |
| RNVC | SADC | MSDS | RNAAC |
|---|---|---|---|
| 2 | - | - | MB |
A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of compressor, aircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
| INC | FIIG | Concept | Condition |
|---|---|---|---|
| 50587 | A10700 | - | 1 |
Details
The national stock number or the identification information of the end equipment for which the item is a part.Details
Indicates the design type of the item.Details
The master requirement codes of those requirements which are technically critical by reason of tolerance,fit,performance,or other characteristics which affect identification of the item.Details
Indicates the location of the item on the engine section.Details
Those unusual or unique characteristics or qualities of an item not covered in the other requirements and which are determined to be essential for identification on one or more other functions.Details
Literature and references available for information pertaining to the item.| Part | CAGE | DAC | HCC | RNCC | RNVC | MSDS | RNAAC |
|---|---|---|---|---|---|---|---|
| 6006T80G07 | 99207 | 2 | - | 5 | 9 | - | MB |
| 6006T80G15 | 99207 | 2 | - | 5 | 9 | - | MB |
| 6006T80G19 | 99207 | 5 | - | 5 | 9 | - | MB |
| HMIC | PMIC | ESD/EMI | Criticality |
|---|---|---|---|
| N | A | - | - |
| UFC | HMC | LTL | LCL |
|---|---|---|---|
| 63220 | - | W | M |
| RVC | WCC | TCC | SHC |
|---|---|---|---|
| 1 | 671 | Z | 9 |
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When the NSN 2840-00-008-6166 was assigned to the Federal Catalog?
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