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 | ||||
2805-00-371-7568 (2805003717568) | 2835-00-626-9669 (2835006269669) | 2840-00-939-3493 (2840009393493) | 2840-01-321-1442 (2840013211442) | |
2825-00-309-1763 (2825003091763) | 2835-00-682-5353 (2835006825353) | 2815-00-139-3970 (2815001393970) | 2840-00-866-1571 (2840008661571) | |
2840-01-674-1631 (2840016741631) | 2840-01-310-6208 (2840013106208) | 2815-01-690-0888 (2815016900888) | 2835-01-177-9984 (2835011779984) | |
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