NSN 2840-01-452-0525 · NIIN 014520525 · FSC 2840
NO DASHES 2840014520525
In Stock
BLADE,TURBINE ROTOR,AIRCRAFT GAS
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: TF34-GE-100A 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 1.819 AND INCHES MAXIMUM 1.821 |
| ABMZ | DIAMETER | INCHES MINIMUM 9.615 AND INCHES MAXIMUM 9.665 |
| AGAV | END ITEM IDENTIFICATION | TF34-GE-100A AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND ABHP AND ABMZ AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | DOVETAIL BLADE ATTACHMENT METHOD; DCN 97-065 INTRODUCES COMMERCIAL STG 1 AND 2 HPT TURBINE BLADES AND ASSOCIATED BAFFLES AS SETS TO THE ENGINE PARTS LISTS; SUPERSEDES P/N 6040T44G14 |
| MATT | MATERIAL | OVERALL TITANIUM ALLOY |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF34-4, FIG 15A, IND 14 |
Supersedes
This item replaces cancelled NIIN 011386855. An older drawing citing one of those numbers resolves here.