434500: ENGINE,GAS TURBINE,AIRCRAFT.
The ENGINE,GAS TURBINE,AIRCRAFT is a the manufacturer industrial component. Key specifications include fuel_type: JET FUEL, end_item_identification: TF33-7 ENGINE, reference_data_and_literature: 2J-TF33-44, criticality_code_justification: AGAV, power_output_for_which_designed: PNEUMATIC/SHAFT. This part is cataloged in the U.S.
Government catalog under NSN 3120-00-364-8546, 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.
| fuel_type | JET FUEL |
| end_item_identification | TF33-7 ENGINE |
| reference_data_and_literature | 2J-TF33-44 |
| criticality_code_justification | AGAV |
| power_output_for_which_designed | PNEUMATIC/SHAFT |
| NSN | 3120-00-364-8546 |
| CORNER SHAPE | CHAMFERED INSIDE LEFT CORNER |
| CORNER SHAPE | SQUARE OUTSIDE RIGHT CORNER |
| CORNER SHAPE | SQUARE OUTSIDE LEFT CORNER |
| CORNER SHAPE | CHAMFERED INSIDE RIGHT CORNER |
| BODY OUTSIDE DIAMETER | 3.4375 INCHES MINIMUM AND 3.4382 INCHES MAXIMUM IN |
| STYLE DESIGNATOR | SEGMENTED, PLAIN, NO OUTSIDE FLANGES |
| MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD SINGLE MATERIAL RESPONSE OUTER LAYER |
| MATERIAL DOCUMENT AND CLASSIFICATION | SAE 49 ASSN STD SINGLE MATERIAL RESPONSE INNER LAYER |
| OVERALL LENGTH | 1.7450 INCHES MINIMUM AND 1.7550 INCHES MAXIMUM IN |
| BODY INSIDE DIAMETER | 2.9760 INCHES MINIMUM AND 2.9770 INCHES MAXIMUM IN |