NSN 2840-01-448-7035 · NIIN 014487035 · FSC 2840
NO DASHES 2840014487035
In Stock
SEAL,AIR,AIRCRAFT GAS TURBINE EN
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F100-PW-229 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 0.258 AND INCHES MAXIMUM 0.268 |
| ABMZ | DIAMETER | INCHES MINIMUM 25.004 AND INCHES MAXIMUM 25.008 |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND ABMZ AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL BRUSH,COMBUSTION CHAMBER,OUTER ASSEMBLY |
| CZBJ | ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 86, IND 19F; USE ONLY ON P/NS 4083194, 4083560, AND 4083565; CONTAINS WIRE BRUSH, 2250-2650 WIRES PER CIRCUMFERENTIAL INCH; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY; TURBINE STATOR SUPPORT AND COMBUSTION CHAMBER |
| MATT | MATERIAL | OVERALL NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL ASSN STD 1ST MATERIAL RESPONSE A-S5599 OR ASSN STD 2ND MATERIAL RESPONSE A-S5666 |