NSN 2840-00-769-1608 of Cover Oil Turbine R - Parts Details
| Alternative NSN: 2840007691608 |
| Item Name: Cover Oil Turbine R |
| FSG: 28 Engines Turbines and Components |
| Federal Supply Class (FSC): 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NIIN: 007691608 |
| NCB Code: USA (00) |
| Manufacturers: Electromethods Inc , Flanagan Brothers Inc , United Technologies Corporation , Turbo Power Marine Systemes , Beta Engineering Inc |
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 358049 under NSN 2840-00-769-1608 of Cover Oil Turbine R manufactured by Electromethods Inc, Flanagan Brothers Inc, United Technologies Corporation, Turbo Power Marine Systemes, Beta Engineering Inc.
Federal Supply Class of NSN 2840-00-769-1608 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 2840-00-769-1608, 2840007691608
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Part No Manufacturer Item Name QTY RFQ 358049 Electromethods Inc cover oil turbine r Avl RFQ 358049 Flanagan Brothers Inc cover oil turbine r Avl RFQ 358049 United Technologies Corporation cover oil turbine r Avl RFQ 358049 Turbo Power Marine Systemes cover oil turbine r Avl RFQ 358049 Beta Engineering Inc cover oil turbine r Avl RFQ
Characteristics Data of NSN 2840007691608MRC Criteria Characteristic ADAV OVERALL DIAMETER 6.350 INCHES NOMINAL CXCY III PART NAME ASSIGNED BY CONTROLLING AGENCY COVER-OIL TURBINE REAR BEARING ASSY OF FEAT SPECIAL FEATURES INSIDE DIAMETER: 5.665 MINIMUM AND 5.675 MAXIMUM SPCL SPECIAL TEST FEATURES 20 HOLES EQUALLY SPACED AND LOCATED WITHIN .005 OF TRUE POSITION, .276-.286 DIAMETER SUPP III SUPPLEMENTARY FEATURES SPECIFICATION: PWA 11-15 TEXT GENERAL CHARACTERISTICS ITEM DESCRIPTION SURFACE ROUGHNESS AS SPECIFIED; SEE SPEC PWA 351,ALL DIA MUST BE CONCENTRIC WITHIN DIO FOR UNLESS OTHERWISE SPECIFIED,STRESS RELIEVE AT 1200F FOR 1HR AFTER WELDING AND BEFORE MACHINING, WELD I/A/W WITH SPEC PWA 15-2 MATING PARTS MAY BE FITT
| MRC | Criteria | Characteristic |
|---|---|---|
| ADAV | OVERALL DIAMETER | 6.350 INCHES NOMINAL |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | COVER-OIL TURBINE REAR BEARING ASSY OF |
| FEAT | SPECIAL FEATURES | INSIDE DIAMETER: 5.665 MINIMUM AND 5.675 MAXIMUM |
| SPCL | SPECIAL TEST FEATURES | 20 HOLES EQUALLY SPACED AND LOCATED WITHIN .005 OF TRUE POSITION, .276-.286 DIAMETER |
| SUPP | III SUPPLEMENTARY FEATURES | SPECIFICATION: PWA 11-15 |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | SURFACE ROUGHNESS AS SPECIFIED; SEE SPEC PWA 351,ALL DIA MUST BE CONCENTRIC WITHIN DIO FOR UNLESS OTHERWISE SPECIFIED,STRESS RELIEVE AT 1200F FOR 1HR AFTER WELDING AND BEFORE MACHINING, WELD I/A/W WITH SPEC PWA 15-2 MATING PARTS MAY BE FITT |