NSN 2840-01-448-7511 · NIIN 014487511 · FSC 2840
NO DASHES 2840014487511
In Stock
SUPPORT,TURBINE COMPONENT,AIRCRA
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 |
|---|---|---|
| AARX | INSIDE DIAMETER | INCHES MINIMUM 23.962 AND INCHES MAXIMUM 23.966 |
| ABHP | OVERALL LENGTH | INCHES MINIMUM 3.773 AND INCHES MAXIMUM 3.781 |
| ABKV | OUTSIDE DIAMETER | INCHES MINIMUM 26.217 AND INCHES MAXIMUM 26.221 |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABKV AND AARX AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SUPPORT TURBINE DUCT AND VANE, ASSEMBLY OF |
| FEAT | SPECIAL FEATURES | USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY |
| MATT | MATERIAL | NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MFR REF SINGLE MATERIAL RESPONSE WA1198 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 99, IND 34 |