Part Number: 851641 | Manufacturer: United Technologies Corp |
NSN : 2840-01-362-7057 (2840013627057) | Item Name : disk and hub compressor aircraft |
CAGE Code: 77445 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
NIIN : 01-362-7057 (013627057) | FSG : 28 Engines Turbines and Components |
Country: USA | NCB Code: 01 |
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-362-7057 Item Description: Disk And Hub Compressor Aircraft | 2840 | 013627057 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
851641 | 3 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 6.500 INCHES NOMINAL |
ABMZ | DIAMETER | 15.000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | TF33-PW-102/A & B AIRCRAFT GAS TURBINE-FAN ENGINES |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
CZCJ | STAGE NUMBER | 1 |
FEAT | SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR |
MATT | III MATERIAL | TITANIUM ALLOY HUB |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 5, IND 1 |
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