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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-187-3182 Item PartTypeName: DISK,COMPRESSOR,AIRCRAFT GAS TUR | 2840 | 011873182 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9940M55P13 | 6 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | OVERALL WIDTH | 1.180 INCHES MINIMUM AND 1.190 INCHES MAXIMUM |
| ABMZ | DIAMETER | 17.000 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 1.5000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG F108 |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | DISK,COMPRESSOR ROTOR-STAGE 3 |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 3 |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME DISK,TURBINE,TURBINE ENGINE |
| MATT | MATERIAL | TITANIUM OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-F108-14 FIG 72-31-00-1 IND 120D |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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