| Part Number: 635498 | Manufacturer: United Technologies Corp |
| NSN : 2840-01-458-2759 (2840014582759) | Item Name : hub compressor aircraft gas turb |
| CAGE Code: 77445 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NIIN : 01-458-2759 (014582759) | FSG : 28 Engines Turbines and Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-458-2759 Item Description: Hub Compressor Aircraft Gas Turb | 2840 | 014582759 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 635498 | 3 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 12.726 INCHES NOMINAL |
| ABMZ | DIAMETER | 16.741 INCHES MINIMUM AND 16.743 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND ABHP AND ABMZ AND CZBJ |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | P/N NOT TO BE PROCURED; P/N TAKEN OFF ENGINE AND PUT INTO SUPPLY THEN REWORKED UP TO P/N 753538 (01-160-6504); DEPENDING ON REPAIR IT WILL GET ASSIGNED A DIFFERENT P/N; IF THIS P/N HAS CRACKS IN THE TIE ROD HOLES WILL BE ASSIGNED P/N 784473 |
| MATT | III MATERIAL | STEEL OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 6, IND 51 |
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