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| 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 | ||||
| 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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