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National Stock Number:
2840-01-452-0525
Federal Supply Class:
2840
National Item Identification Number:
014520525
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:
| 6078T19 | 99207 | GENERAL ELECTRIC COMPANY | | 6078T19P07 | 99207 | GENERAL ELECTRIC COMPANY | | 6078T19P10 | 99207 | GENERAL ELECTRIC COMPANY |
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Techincal Specification:
| DESIGN TYPE | AXIAL COMPRESSOR | | DIAMETER | 9.615 INCHES MINIMUM AND 9.665 INCHES MAXIMUM | | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND ABHP AND ABMZ AND FEAT | | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE | | III MATERIAL | TITANIUM ALLOY OVERALL | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 1.819 INCHES MINIMUM AND 1.821 INCHES MAXIMUM | | REFERENCE DATA AND LITERATURE | T.O. 2J-TF34-4, FIG 15A, IND 14 | | SPECIAL FEATURES | DOVETAIL BLADE ATTACHMENT METHOD; DCN 97-065 INTRODUCES COMMERCIAL STG 1 AND 2 HPT TURBINE BLADES AND ASSOCIATED BAFFLES AS SETS TO THE ENGINE PARTS LISTS; SUPERSEDES P/N 6040T44G14 | | STAGE NUMBER | 1 |
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