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National Stock Number:
2840-01-444-7700
Federal Supply Class:
2840
National Item Identification Number:
014447700
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.
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Manufacturer Information:
| 1807M22 | 07482 | GENERAL ELECTRIC COMPANY | | 1807M22G01 | 07482 | GENERAL ELECTRIC COMPANY | | 1807M22G03 | 07482 | GENERAL ELECTRIC COMPANY |
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Techincal Specification:
| DESIGN TYPE | AXIAL COMPRESSOR | | BLADE ATTACHMENT METHOD | FIR TREE | | CRITICALITY CODE JUSTIFICATION | AGAV | | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE | | III MATERIAL | ALUMINUM BLADE | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 3.116 INCHES NOMINAL | | OVERALL WIDTH | 1.217 INCHES MINIMUM AND 1.222 INCHES MAXIMUM | | SPECIAL FEATURES | THIS ITEM IS PART OF THE HT90 MODFOR THE TF39 ENGINE, EXTERNAL COATING PLATINUM ALUMINIDE, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 1, TRAIL | | STAGE NUMBER | 1 |
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