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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 | ||||
2840-00-132-3586 (2840001323586) | 2805-01-261-7918 (2805012617918) | 2840-01-389-4129 (2840013894129) | 2815-00-759-6468 (2815007596468) | |
2835-00-962-2709 (2835009622709) | 2835-01-104-3663 (2835011043663) | 2805-01-310-1770 (2805013101770) | 2805-00-424-7861 (2805004247861) | |
2815-01-225-5899 (2815012255899) | 2815-01-054-6079 (2815010546079) | 2815-01-048-6906 (2815010486906) | 2840-01-459-1273 (2840014591273) | |
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