|
|
|
National Stock Number:
2840-01-490-0077
Federal Supply Class:
2840
National Item Identification Number:
014900077
Description:
BLADE,FAN,AIRCRAFT GAS TURBINE E
Detail:
AN ITEM MOUNTED ON A DISK, FAN, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO CREATE THE FLOW OF AIR IN THE FAN SECTION OF A ENGINE, GAS TURBINE, AIRCRAFT.
|
Manufacturer Information:
| 1782M53G01 | 07482 | GENERAL ELECTRIC COMPANY | | 1782M53G02 | 07482 | GENERAL ELECTRIC COMPANY | | 1782M53G03 | 07482 | GENERAL ELECTRIC COMPANY | | 1782M53G04 | 07482 | GENERAL ELECTRIC COMPANY | | 1782M53G05 | 07482 | GENERAL ELECTRIC COMPANY | | 1782M54P01 | 07482 | GENERAL ELECTRIC COMPANY | | 1782M54P02 | 07482 | GENERAL ELECTRIC COMPANY | | 1999M69P01 | 07482 | GENERAL ELECTRIC COMPANY | | 1999M69P07 | 07482 | GENERAL ELECTRIC COMPANY | | 1999M69P08 | 07482 | GENERAL ELECTRIC COMPANY | | 1999M69P09 | 07482 | GENERAL ELECTRIC COMPANY | | 2113M18P01 | 07482 | GENERAL ELECTRIC COMPANY | | 2113M18P02 | 07482 | GENERAL ELECTRIC COMPANY | | 2113M18P03 | 07482 | GENERAL ELECTRIC COMPANY |
|
Techincal Specification:
| DESIGN TYPE | AXIAL COMPRESSOR | | BLADE ATTACHMENT METHOD | DOVETAIL | | CRITICALITY CODE JUSTIFICATION | AGAV | | ENGINE SECTION LOCATION | FAN | | III MATERIAL | TITANIUM ALLOY OVERALL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,FAN ROTOR-STAGE 2 | | PROPRIETARY CHARACTERISTICS | PACS | | STAGE NUMBER | 2 |
|
|