Part Number: 4067357 | Manufacturer: United Technologies Corp |
NSN : 2840-01-216-0526 (2840012160526) | Item Name : hub compressor aircraft gas turb |
CAGE Code: 77445 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
NIIN : 01-216-0526 (012160526) | FSG : 28 Engines Turbines and Components |
Country: USA | NCB Code: 01 |
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-216-0526 Item Description: Hub Compressor Aircraft Gas Turb | 2840 | 012160526 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4067357 | 3 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM |
ABMZ | DIAMETER | 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT ENGINE |
APGF | DESIGN TYPE | COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND ABHP AND ABMZ |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME NUT,DRIVE SHAFT |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
CZCJ | STAGE NUMBER | 2 |
FEAT | SPECIAL FEATURES | INTL INVOLUTE SPLINE DATA: TEETH 140; PRESSURE ANGLE 30 DEG.; T.O. 2J-F100-4, FIGURE 115, INDEX 3; USED ON THE REAR COMPRESSOR DRIVE; REIDENTIFIED FROM P/N 4047224 |
MATT | III MATERIAL | NICKEL ALLOY HUB |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB |
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