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Item Name | Case Compressor Aircraft Gas Tur |
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) | 01-458-2761 (014582761) |
NCB Code | USA (01) |
Manufacturer | United Technologies Corporation |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | Diameter | 35.433 INCHES MINIMUM AND 35.443 INCHES MAXIMUM |
RDAL | Reference Data And Literature | T.O. 2J-TF33-44, FIG 11, IND 1; 2J-TF33-14, FIG 13, IND 1 |
CZBJ | Engine Section Location | COMPRESSOR |
FEAT | Special Features | THIS IS A REDESIGNED CASE FEATURING A REINFORCED 6TH STATOR SUPPORT LAND; REPLACES P/N 454832 |
ABHP | Overall Length | 18.028 INCHES MINIMUM AND 18.032 INCHES MAXIMUM |
CXCY | Part Name Assigned By Controlling Agency | ORIGINAL NAME CASE,FRONT COMPRESSOR |
MRC | Decoded Requirement | Clear Text Reply |
MATT | Material | STEEL OVERALL |
CRTL | Criticality Code Justification | ABHP AND ABMZ AND FEAT AND CZBJ |
CQFM | Hardness Rating | 26.0 ROCKWELL C MINIMUM OVERALL AND 32.0 ROCKWELL C MAXIMUM OVERALL |
AGAV | End Item Identification | TF33 AIRCRAFT GAS TURBINE ENG |
APGF | Design Type | AXIAL COMPRESSOR |
MDCL | Material Document And Classification | AMS6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
Relevant Components for NSN - 2840-01-458-2761, 2840014582761 | ||||
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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