NSN 2840-01-440-1697, 2840014401697 Damper Turbine Blade Aircraft Tu Parts Sourcing
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Alternative NSN: 2840-01-440-1697 | Item Name : Damper Turbine Blade Aircraft Tu | FSG : 28 Engines Turbines and Components | Federal Supply Class (FSC) : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components | NIIN: 014401697 | NCB Code: USA (01) |
Part Number's List for NSN 2840-01-440-1697, 2840014401697
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
4082885 | United Technologies Corp | damper turbine blade aircraft tu | Avl | RFQ |
Characteristics Data of NSN 2840014401697
MRC | Criteria | Characteristic |
---|---|---|
CQFM | HARDNESS RATING | 34.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL |
AGAV | III END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
ABMZ | DIAMETER | 16.788 INCHES NOMINAL |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
ABHP | OVERALL LENGTH | 0.565 INCHES MINIMUM AND 0.571 INCHES MAXIMUM |
FEAT | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 21; REPL P/N 4074864 ONCE TCTO HAS BEEN ACCOMPLISHED; RETAINING PLATE DAMPER IS SYMMETRICAL IN SHAPE AND HAS 6 RETENTION TABS FORWARD AND AFT TO PRECLUDE POSSIBLE REVERSE INSTALLATION AND RESULTING CUT-OFF OF COOLING AIR TO THE 2ND STAGE BLADES |
MATT | MATERIAL | NICKEL ALLOY OVERALL |
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