1461M87G15: FRAME,TURBINE,AIRCRAFT GAS TURBI.
FRAME,TURBINE,AIRCRAFT GAS TURBI. Key specifications include OUTSIDE DIAMETER: 33.556 INCHES NOMINAL IN, END ITEM IDENTIFICATION: F110-GE-129 ACFT GAS TURBINE ENG, REFERENCE DATA AND LITERATURE: T.O. 2J-F110-4, FIG 79, IND 15 ORFIG 81, IND 19, CRITICALITY CODE JUSTIFICATION: AGAV, NUMBER OF VARIABLE GUIDE VANES: 10.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-460-8957, indicating validated use in U.S. government and defense logistics supply chains.
Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.
| OUTSIDE DIAMETER | 33.556 INCHES NOMINAL IN |
| END ITEM IDENTIFICATION | F110-GE-129 ACFT GAS TURBINE ENG |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 79, IND 15 ORFIG 81, IND 19 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| NUMBER OF VARIABLE GUIDE VANES | 10 |
| NSN | 2840-01-460-8957 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 79, IND 15 ORFIG 81, IND 19 |
| OUTSIDE DIAMETER | 33.556 INCHES NOMINAL IN |
| NUMBER OF VARIABLE GUIDE VANES | 10 |
| SPECIAL FEATURES | THIS CHANGE ADDRESSES CRACKS AND RIVET BREAKAGE IN THE TURBINE FRAME FWD OUTER LINER SUPPORTS; ROOT CAUSE IS A LACK OF THERMAL GROWTH CAPABILITY,WHICH CAUSES THE SUPPORT TO CRACK AND LOAD THE RIVETS. CHANGES WILL INCREASE SHEET METAL HOLE SIZE, SPACERS WITH LONGER STEM AND LARGER WASHERS |
| END ITEM IDENTIFICATION | F110-GE-129 ACFT GAS TURBINE ENG |
No substitute or cross-reference records for this part.