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National Stock Number:
2840-01-445-2811
Federal Supply Class:
2840
National Item Identification Number:
014452811
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:
| 4085104 | 77445 | RTX CORPORATION |
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Techincal Specification:
| BLADE ATTACHMENT METHOD | FIR TREE | | CRITICALITY CODE JUSTIFICATION | FEAT AND ABMZ AND ABHP AND CZBJ | | DESIGN TYPE | AXIAL COMPRESSOR | | DIAMETER | 29.004 INCHES MINIMUM AND 29.404 INCHES MAXIMUM | | ENGINE SECTION LOCATION | TURBINE | | HARDNESS RATING | 45.0 ROCKWELL C MINIMUM AND 55.0 ROCKWELL C MAXIMUM OVERALL | | OVERALL LENGTH | 6.771 INCHES MINIMUM AND 6.781 INCHES MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | PWA658 MFR REF SINGLE MATERIAL RESPONSE OVERALL | | MATERIAL | NICKEL ALLOY OVERALL | | SPECIAL FEATURES | T.O. 2J-F100-14, FIG 130, IND 9; INTERIM BLADE REPLACES P/N 4067004 AND IS REPLACED BY P/N 4084804 PER ECP 95-NA027 | | STAGE NUMBER | 4 |
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