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National Stock Number:
2840-01-455-4979
Federal Supply Class:
2840
National Item Identification Number:
014554979
Description:
BLADE,COMPRESSOR,AIRCRAFT GAS TU
Detail:
AN ITEM MOUNTED ON A DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO CREATE THE FLOW OF AIR IN THE COMPRESSOR SECTION OF AN ENGINE, GAS TURBINE, AIRCRAFT.
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Manufacturer Information:
| 572901 | 77445 | RTX CORPORATION |
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Techincal Specification:
| DESIGN TYPE | AXIAL COMPRESSOR | | BLADE ATTACHMENT METHOD | DOVETAIL | | CRITICALITY CODE JUSTIFICATION | FEAT AND ABKW AND ABMK AND CZBJ | | ENGINE SECTION LOCATION | COMPRESSOR | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | | III MATERIAL | TITANIUM ALLOY OVERALL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE,COMPRESSOR ROTOR | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL HEIGHT | 3.870 INCHES MINIMUM AND 3.880 INCHES MAXIMUM | | OVERALL WIDTH | 0.839 INCHES NOMINAL | | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 5, IND 8 | | SPECIAL FEATURES | THIS ITEM COMES OFF A JT3D-7 COMMERCIAL ENGINE; IT REPLACES P/N 430401; THE FORM, FIT, FUNCTION IS EXACTLY THE SAME, THE ONLY DIFFERENCE IS THE ANGLE OF THE BLADE; BLADE WILL PROVIDE 1200 POUNDS MORE THRUST WHEN IN USE; ONCE REPLACED WILL MODIFY THE TF33-PW-102B TO THE 102C; JOINT STAR AIRCRAFT PROJECT | | STAGE NUMBER | 1 |
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