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National Stock Number:
2840-01-453-0713
Federal Supply Class:
2840
National Item Identification Number:
014530713
Description:
BLADE,FAN,AIRCRAFT GAS TURBINE E
Detail:
AN ITEM MOUNTED ON A DISK, FAN, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO CREATE THE FLOW OF AIR IN THE FAN SECTION OF A ENGINE, GAS TURBINE, AIRCRAFT.
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Manufacturer Information:
| 1476M11 | 07482 | GENERAL ELECTRIC COMPANY | | 1476M11P04 | 07482 | GENERAL ELECTRIC COMPANY | | 1476M11P06 | 07482 | GENERAL ELECTRIC COMPANY |
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Techincal Specification:
| DESIGN TYPE | AXIAL COMPRESSOR | | BLADE ATTACHMENT METHOD | SLOT | | CRITICALITY CODE JUSTIFICATION | CZBJ AND CZCJ AND ABHP AND FEAT | | ENGINE SECTION LOCATION | FAN | | III MATERIAL | TITANIUM ALLOY OVERALL | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 11.648 INCHES MINIMUM AND 11.668 INCHES MAXIMUM | | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-14 | | SPECIAL FEATURES | NEW DESIGN HAS LASER SHOCK PEENING; THIS WILL ASSIST IN ELIMINATING FATIGUE AND FOD DAMAGE; LSP INCREASES FOD TOLERENCE BY CREATING A COMPRESSIVE LAYER THAT NEUTRALIZES THE SOURCES OF VIBRATORY RESPONSES; WILL DECREASE THE FREQUENCY OF BLEND REPAIR MAINTENANCE;NEW BLADE IS PHYSICALLY BUT NOT INTERCHANGEABLE WITH THE CURRENT BLADE P/N 1476M11P03; DO NOT INTERMIX LSP BLADES WITH STANDARD BLADES, MUST BE REPLACED AS A COMPLETE SET; PROPOSED BLADES ARE SUITABLE FOR SPARE PART REPLACEMENT AND ARE BEING RELEASED AS AN ALTERNATE PART TO THE EXISTING ROTOR ASSEMBLIES; ALL BLADES TREATED WITH LASER SHOCK PEENING (LSP) WILL HAVE A VISUAL IDENTIFIER, A LARGE CIRCULAR DOT ON THE INBOARD CONVEX PLATFORM | | STAGE NUMBER | 1 |
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