NSN 2840-01-200-6464 of Shroud Segment Turbine Aircraft - Product Details
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Alternative NSN: 2840-01-200-6464 |
Item Name:Shroud Segment Turbine Aircraft |
FSG: 28 Engines Turbines and Components |
Federal Supply Class (FSC): 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
NIIN: 012006464 |
NCB Code: USA (01) |
Manufacturers: General Electric Company , Electro Methods Inc , Columbia Manufacturing Inc , Union Machine Company Of Lynn Inc , Tecomet Albuquerque , Tss Technologies Inc , Warfighter Focused Logistics Inc , Meco Inc , Moeller Mfg Company Inc , Mcnally Industries Llc , Modern Industries Inc , General Tool Company |
Manufacturer's List for NSN 2840-01-200-6464, 2840012006464
Part Number Related To NSN 2840-01-200-6464, 2840012006464
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
1284M82G01 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
1284M82G05 | 2840-01-200-6464 | shroud segment turbine aircraft | Avl | RFQ |
Characteristics Data of NSN 2840012006464
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 12.233 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 1.890 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | F110 ACFT ENGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
CZCJ | STAGE NUMBER | 2 |
FEAT | SPECIAL FEATURES | OUTER RADIUS 2ND END 11.908 IN.; INNER RADIUS 1ST END 11.393 IN.; INNER RADIUS 2ND END 11.14 IN.; FORMED SHAPE 45 DEG. 57 MIN. 27 SEC.; 11 HOLES 0.3535 IN. DIA. COUNTERBORE 0.520 IN. DIA. W/2 CUTTER RUN OUTS PER EA HOLE |
MATT | MATERIAL | ALUMINUM ALLOY 2618 OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
SFTT | SURFACE TREATMENT | ANODIZE OVERALL |