|
|
|
National Stock Number:
2840-01-447-2506
Federal Supply Class:
2840
National Item Identification Number:
014472506
Description:
BLADE,TURBINE ROTOR,AIRCRAFT GAS
Detail:
AN ITEM MOUNTED ON A DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO CREATE THE FLOW OF AIR IN THE TURBINE SECTION OF AN ENGINE, GAS TURBINE, AIRCRAFT.
|
Manufacturer Information:
| 1881M11P01 | 07482 | GENERAL ELECTRIC COMPANY | | KDS 2840-4003 | 3999F | DEFENSE ACQUISITION PROGRAM ADMINISTRATION, R.O.K |
|
Techincal Specification:
| BLADE ATTACHMENT METHOD | FIR TREE | | CRITICALITY CODE JUSTIFICATION | AGAV | | DESIGN TYPE | AXIAL COMPRESSOR | | ENGINE SECTION LOCATION | LOW PRESSURE TURBINE | | OVERALL LENGTH | 4.784 INCHES MINIMUM AND 4.794 INCHES MAXIMUM | | PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,LOW PRESSURE TURBINE ROTOR-STAGE 1, MACH | | MATERIAL | NICKEL ALLOY BLADE | | REFERENCE DATA AND LITERATURE | 2J-F110-14 FIG 90 IND 1 | | STAGE NUMBER | 1 |
|
|