|
|
National Stock Number: 2840-01-444-7680
Federal Supply Class: 2840
National Item Identification Number: 014447680
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:
1807M20 | 07482 | GENERAL ELECTRIC COMPANY | 1807M20G01 | 07482 | GENERAL ELECTRIC COMPANY | 1807M20G03 | 07482 | GENERAL ELECTRIC COMPANY |
|
Techincal Specification:
DESIGN TYPE | AXIAL COMPRESSOR | BLADE ATTACHMENT METHOD | FIR TREE | CRITICALITY CODE JUSTIFICATION | FEAT | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | III MATERIAL | NICKEL ALLOY OVERALL | PROPRIETARY CHARACTERISTICS | PACS | SPECIAL FEATURES | ST.O. 2J-T39-4, FIG 59 IND 6; REPL P/N 9198M37G04, NOT TO BE GRPED; OLD CONF REPL BY TCTO KIT K0216914A WITH ALEADING AND TRAILING NOZZLES ON THE HPT ROTOR ONLY; OLD CONFIG BEING THROWN AWAY, NOT MODIFIED, ALL NEW CONFIGURATION | STAGE NUMBER | 1 |
|
|