4079597: SYNCHRONIZING RING,INLET GUIDE V.
SYNCHRONIZING RING,INLET GUIDE V. Key specifications include material: TITANIUM ALLOY, overall_length: 0.960 INCHES MINIMUM AND 0.980 INCHES MAXIMUM IN, inside_diameter: 36.000 INCHES MINIMUM AND 36.004 INCHES MAXIMUM IN, outside_diameter: 37.264 INCHES MINIMUM AND 37.268 INCHES MAXIMUM IN, end_item_identification: F100 AIRCRAFT GAS TURBINE ENGINE, portion_of_circumference: 360 DEGREES. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-437-1124, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | TITANIUM ALLOY |
| overall_length | 0.960 INCHES MINIMUM AND 0.980 INCHES MAXIMUM IN |
| inside_diameter | 36.000 INCHES MINIMUM AND 36.004 INCHES MAXIMUM IN |
| outside_diameter | 37.264 INCHES MINIMUM AND 37.268 INCHES MAXIMUM IN |
| 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. IN |
| end_item_identification | F100 AIRCRAFT GAS TURBINE ENGINE |
| portion_of_circumference | 360 DEGREES |
| reference_data_and_literature | T.O. 2J-F100-24, FIG 116, IND 38 |
| criticality_code_justification | ABKV AND AARX AND ABHP AND FEAT |
| material_document_and_classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE |
| NSN | 2840-01-437-1124 |
| CRITICALITY CODE JUSTIFICATION | ABKV AND AARX AND ABHP AND FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-24, FIG 116, IND 38 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 0.960 INCHES MINIMUM AND 0.980 INCHES MAXIMUM IN |
| OUTSIDE DIAMETER | 37.264 INCHES MINIMUM AND 37.268 INCHES MAXIMUM IN |
| INSIDE DIAMETER | 36.000 INCHES MINIMUM AND 36.004 INCHES MAXIMUM IN |
| 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. IN |
| END ITEM IDENTIFICATION | F100 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | TITANIUM ALLOY |
| PORTION OF CIRCUMFERENCE | 360 DEGREES |
No substitute or cross-reference records for this part.