NSN 2840-01-451-9636 · NIIN 014519636 · FSC 2840
NO DASHES 2840014519636
In Stock
DUCT,COMPRESSOR,AIRCRAFT GAS TUR
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 NOMINAL 12.130 |
| ABMK | OVERALL WIDTH | INCHES MINIMUM 2.320 AND INCHES MAXIMUM 2.326 |
| ABMZ | DIAMETER | INCHES MINIMUM 27.647 AND INCHES MAXIMUM 27.659 |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABMK AND ABHP AND ABMZ AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME DUCT SEGMENT,COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | NO 3. BEARING REAL SEAL ASSY, REAR COMPRESSOR STATOR VARIABLE INLET VANES, EXIT FAN STATOR AND COMPRESSOR INTERMEDIATE CASE ASSY; STAGE 4; REPLACES P/N 4081682-01; CORROSION RESISTANT SEGMENTS |
| MATT | MATERIAL | DUCT NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | DUCT ASSN STD SINGLE MATERIAL RESPONSE A-S5771 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 84, IND 16 AND 17 |