NSN 2840-01-616-6608 of Shroud Segment Turbine Aircraft - Parts Details
Alternative NSN: 2840016166608 |
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: 016166608 |
NCB Code: USA (01) |
Manufacturers: Yulista Aviation Inc , Boeing Company |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers 7-511141611-018, 7 511154651 101, 7 511141611 018 under NSN 2840-01-616-6608 of Shroud Segment Turbine Aircraft manufactured by Yulista Aviation Inc, Boeing Company.
Federal Supply Class of NSN 2840-01-616-6608 is FSC 2840 contains part details of Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Quote for your desired part numbers.
Part Number's List for NSN 2840-01-616-6608, 2840016166608
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Part No Manufacturer Item Name QTY RFQ 7-511141611-018 Yulista Aviation Inc shroud segment turbine aircraft Avl RFQ 7 511154651 101 Boeing Company shroud segment turbine aircraft Avl RFQ 7 511141611 018 Boeing Company shroud segment turbine aircraft Avl RFQ
Characteristics Data of NSN 2840016166608MRC Criteria Characteristic ABPX MATERIAL THICKNESS 0.032 INCHES NOMINAL AGAV END ITEM IDENTIFICATION 7-610000000-1 CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY SHROUD ASSY,ENGINE NACELLE,AFT FEAT SPECIAL FEATURES FENCE,SHROUD, RH MATT III MATERIAL NICKEL ALLOY OVERALL MDCL MATERIAL DOCUMENT AND CLASSIFICATION AMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
MRC | Criteria | Characteristic |
---|---|---|
ABPX | MATERIAL THICKNESS | 0.032 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | 7-610000000-1 |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD ASSY,ENGINE NACELLE,AFT |
FEAT | SPECIAL FEATURES | FENCE,SHROUD, RH |
MATT | III MATERIAL | NICKEL ALLOY OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |