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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-443-4068 Item Description: Hub Turbine Aircraf | 2840 | 014434068 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1385M24P05 118 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | III END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | INCONEL 718 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
FEAT | SPECIAL FEATURES | SAME AS P/N 1385M24P05 BUT ONLY TO BE USED ON THE F118 ENGINE |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
SR-5 | THE MANUFACTURERS DATA | |
CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND FEAT |
SR-5 | MANUFACTURERS CODE | 07482 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
MATT | MATERIAL | NICKEL ALLOY OVERALL |
SR-5 | DESIGN CONTROL REFERENCE | 1385M24P05-118 |
138-0000-006 | 138-0002-16 | 138-0002-03 | 138-0002-11 |
138-0002-15 | 138-0000-001 | 138-0002-07 | 138-0002-12 |
138-0002-08 | 138-0002-09 | 138-0002-02 | 138-0-0-202 |
138 0002 13 | 138-0002-17 | 138-0-0-202 | 138-0-0-202 |
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