9321M62G11: FRAME,FRONT,AIRCRAFT GAS TURBINE.
FRAME,FRONT,AIRCRAFT GAS TURBINE. Key specifications include overall_length: 4.530 INCHES MINIMUM AND 4.550 INCHES MAXIMUM IN, outside_diameter: 47.870 INCHES NOMINAL IN, special_features: T.O. 2J-F101-4, FIG 4, IND 20, end_item_identification: F101 AIRCRAFT ENGINE, reference_data_and_literature: 2J-F101-4, FIG 2, IND 1A A, number_of_variable_guide_vanes: 17.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-173-5491, 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.
| overall_length | 4.530 INCHES MINIMUM AND 4.550 INCHES MAXIMUM IN |
| outside_diameter | 47.870 INCHES NOMINAL IN |
| special_features | T.O. 2J-F101-4, FIG 4, IND 20 |
| end_item_identification | F101 AIRCRAFT ENGINE |
| reference_data_and_literature | 2J-F101-4, FIG 2, IND 1A A |
| number_of_variable_guide_vanes | 17 |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME FRAME ASSEMBLY,AIRCRAFT TURBINE ENGINE |
| NSN | 2840-01-173-5491 |
| REFERENCE DATA AND LITERATURE | 2J-F101-4, FIG 2, IND 1A A |
| OVERALL LENGTH | 4.530 INCHES MINIMUM AND 4.550 INCHES MAXIMUM IN |
| OUTSIDE DIAMETER | 47.870 INCHES NOMINAL IN |
| NUMBER OF VARIABLE GUIDE VANES | 17 |
| SPECIAL FEATURES | T.O. 2J-F101-4, FIG 4, IND 20 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME ASSEMBLY,AIRCRAFT TURBINE ENGINE |
| END ITEM IDENTIFICATION | F101 AIRCRAFT ENGINE |