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Item Name | Damper Turbine Blade Aircraft Tu |
Federal Supply Group (FSG) | Engines Turbines and Components |
Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
National Item Identification Number (NIIN) | 01-440-1697 (014401697) |
NCB Code | USA (01) |
Manufacturer | United Technologies Corporation, Inspektorat Wsparcia Sil Zbrojnych |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
4082885 | united technologies corporation | damper turbine blade aircraft tu | RFQ |
2840PL0712503 | inspektorat wsparcia sil zbrojnych | damper turbine blade aircraft tu | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 0.565 INCHES MINIMUM AND 0.571 INCHES MAXIMUM |
ABMZ | DIAMETER | 16.788 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CQFM | HARDNESS RATING | 34.0 ROCKWELL C MINIMUM OVERALL AND 44.0 ROCKWELL C MAXIMUM OVERALL |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
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 CO |
MATT | III MATERIAL | NICKEL ALLOY OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
Relevant Components for NSN - 2840-01-440-1697, 2840014401697 | ||||
2825-00-790-8901 (2825007908901) | 2825-01-010-8535 (2825010108535) | 2825-00-371-7811 (2825003717811) | 2805-01-264-5598 (2805012645598) | |
2840-01-375-6452 (2840013756452) | 2805-01-130-2594 (2805011302594) | 2835-01-234-6845 (2835012346845) | 2805-01-714-1073 (2805017141073) | |
2840-00-837-2120 (2840008372120) | 2840-01-708-1715 (2840017081715) | 2840-01-200-9553 (2840012009553) | 2805-00-710-5355 (2805007105355) | |
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