| Item Name | Lock Compressor Blade Aircraft G |
| 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) | 01-374-4833 (013744833) |
| NCB Code | USA (01) |
| Manufacturer | United Technologies Corporation |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABPX | MATERIAL THICKNESS | 0.071 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
| FEAT | SPECIAL FEATURES | 44 UNITS PER ASSY; 1 PER 2 STATORVANES |
| ABHP | OVERALL LENGTH | 1.411 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F100PW229 ACFT ENG CORE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| ABMK | OVERALL WIDTH | 0.701 INCHES MINIMUM AND 0.708 INCHES MAXIMUM |
| CQFM | HARDNESS RATING | 36.0 ROCKWELL C NOMINAL |
| CZCJ | STAGE NUMBER | 6 |
| MATT | MATERIAL | NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5596 ASSN STD SINGLE MATERIAL RESPONSE |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-F100-54,FIG 96,IND 51 |
| Components Related to NSN - 2840-01-374-4833, 2840013744833 | ||||
| 2805-00-507-3292 (2805005073292) | 2840-01-454-2997 (2840014542997) | 2835-00-873-3811 (2835008733811) | 2815-01-342-5910 (2815013425910) | |
| 2815-01-240-3064 (2815012403064) | 2815-01-199-0446 (2815011990446) | 2820-00-388-1066 (2820003881066) | 2840-01-179-8314 (2840011798314) | |
| 2840-01-443-5775 (2840014435775) | 2825-00-372-9915 (2825003729915) | 2840-99-446-5984 (2840994465984) | 2840-00-088-9098 (2840000889098) | |
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