NSN 2840-01-430-2158 · NIIN 014302158 · FSC 2840
NO DASHES 2840014302158
In Stock
ROTOR,COMPRESSOR,AIRCRAFT GAS TU
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F100PW229 AIRCRAFT GAS TURBINE ENGINE
Technical characteristics
8 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 NOMINAL 15.500 |
| ABMZ | DIAMETER | INCHES NOMINAL 18.783 |
| AGAV | END ITEM IDENTIFICATION | F100PW229 AIRCRAFT GAS TURBINE ENGINE |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 3 |
| FEAT | SPECIAL FEATURES | ROTOR CONSISTS OF 3 STGS; DISK & HUB; 1STG O/A DIA ON/C 14.590; O/A LENGTH 9.000; 2ND STG O/A DIA ON/C 16.188; O/A LENGTH 7.970; INVOLUTE SPLINE DATA: NO OF TEETH 79; SPLINE PITCH 20/40; PRESSURE ANGLE 30 DEG.; PITCH DIA. 3.9500; 3RD STG O/A LENGTH 4.000; ALL STAGES RECIEVE DOVETAIL BLADES |
| MATT | MATERIAL | OVERALL TITANIUM ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL MFR REF SINGLE MATERIAL RESPONSE WA 1215 |