| Part Number: 1-100-242-09 | Manufacturer: Honeywell International Inc |
| NSN : 2840-00-157-2375 (2840001572375) | Item Name : disk turbine aircraft gas turbin |
| CAGE Code: 99193 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| Alternate P/N : 110024209 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-157-2375 Item Description: Disk Turbine Aircraft Gas Turbin | 2840 | 001572375 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1-100-242-09 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.637 INCHES NOMINAL |
| ABMZ | DIAMETER | 6.570 INCHES MINIMUM AND 6.580 INCHES MAXIMUM |
| AGAV | III END ITEM IDENTIFICATION | T-53 SERIES ENGINES |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | STEEL,AMS4135,BLACK CHROMIC ANODIZED FINISH,6.570 IN. MIN,6.580 IN. MAX O/A OD,1.637 IN. NOM O/A LG,4.082 IN. MIN,4.087 IN. MAX ID,34 BLADE GROOVES EQUALLY SPACED ON OUTER PERIPWERY,34 HOLES 0.094 IN. MIN,0.097 IN. MAX DIA BY 0.095 IN. MIN, |
| MATT | III MATERIAL | STEEL OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4135 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | ANODIZE OVERALL |
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