| Item Name | Synchronizing Ring Inlet Guide V |
| 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) | 01-437-1124 (014371124) |
| NCB Code | USA (01) |
| Manufacturer | United Technologies Corporation |
| MRC | Criteria | Characteristic |
|---|---|---|
| FEAT | Special Features | FOUND IN THE NO. 1 BEARING HOUSING AND SEAL; COMPRESSOR STATOR INLET; WIDTH 0.520-0.524; 21 HOLES EQ SP 0.3120-0.3130 IN DIA. |
| AGAV | End Item Identification | F100 AIRCRAFT GAS TURBINE ENGINE |
| AFGW | Portion Of Circumference | 360 DEGREES |
| ABHP | Overall Length | 0.960 INCHES MINIMUM AND 0.980 INCHES MAXIMUM |
| RDAL | Reference Data And Literature | T.O. 2J-F100-24, FIG 116, IND 38 |
| CRTL | Criticality Code Justification | ABKV AND AARX AND ABHP AND FEAT |
| MATT | Material | TITANIUM ALLOY |
| ABKV | Outside Diameter | 37.264 INCHES MINIMUM AND 37.268 INCHES MAXIMUM |
| MRC | Decoded Requirement | Clear Text Reply |
| MDCL | Material Document And Classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE |
| AARX | Inside Diameter | 36.000 INCHES MINIMUM AND 36.004 INCHES MAXIMUM |
| Relevant Components for NSN - 2840-01-437-1124, 2840014371124 | ||||
| 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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