NSN 2840-01-448-7539 · NIIN 014487539 · FSC 2840
NO DASHES 2840014487539
In Stock
DISK,TURBINE,AIRCRAFT GAS TURBIN
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
Technical characteristics
10 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 1.809 AND INCHES MAXIMUM 1.811 |
| ABMZ | DIAMETER | INCHES MINIMUM 36.696 AND INCHES MAXIMUM 36.736 |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND ABMZ AND ABHP AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 42; USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY |
| MATT | MATERIAL | OVERALL NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL MFR REF SINGLE MATERIAL RESPONSE WA1106 |