NSN 2840-01-453-0713 · NIIN 014530713 · FSC 2840
NO DASHES 2840014530713
In Stock
BLADE,FAN,AIRCRAFT GAS TURBINE E
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F110-GE-129 AIRCRAFT GAS TURBINE ENGINE
Technical characteristics
11 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES MINIMUM 11.648 AND INCHES MAXIMUM 11.668 |
| AGAV | END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND CZCJ AND ABHP AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | FAN |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | 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 |
| MATT | MATERIAL | OVERALL TITANIUM ALLOY |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-14 |