BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: COPPER ALLOY BODY, leg_length: 1.276 INCHES MINIMUM AND 1.286 INCHES MAXIMUM IN, design_type: COMPRESSOR, stage_number: 10, overall_length: 2.083 INCHES MINIMUM AND 2.103 INCHES MAXIMUM IN, connection_type: UNTHREADED EXTERNAL HOSE FIRST FLUID END CONNECTION. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-01-160-6478, 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 | COPPER ALLOY BODY |
| leg_length | 1.276 INCHES MINIMUM AND 1.286 INCHES MAXIMUM IN |
| design_type | COMPRESSOR |
| stage_number | 10 |
| overall_length | 2.083 INCHES MINIMUM AND 2.103 INCHES MAXIMUM IN |
| connection_type | UNTHREADED EXTERNAL HOSE FIRST FLUID END CONNECTION |
| connection_style | BARBED OR SERRATED END ALL ENDS |
| special_features | WEAPON SYSTEM ESSENTIAL; LIFE SUPPORT ITEM; DETAIL SPECIFICATION SHEET, MIL-DTL-7560/1, TITLED: VALVE ASSEMBLY, OXYGEN CYLINDER, BAILOUT |
| style_designator | MALE COUPLING HALF |
| surface_treatment | ZINC BODY |
| end_item_identification | AIRCRAFT: C-141, C-5, C-130, F-111, T-39, B-52, F-15, C-135, AND THE B-2. |
| engine_section_location | COMPRESSOR |
| NSN | 2840-01-160-6478 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| DESIGN TYPE | COMPRESSOR |
| OVERALL LENGTH | 3.275 INCHES NOMINAL IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SPECIAL FEATURES | FORM, FIT AND FUNCTION |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| STAGE NUMBER | 10 |
| MATERIAL | STEEL BLADE |