664433-1: GUIDE,SLEEVE,ARM.
The GUIDE,SLEEVE,ARM is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, overall_length: 2.670 INCHES MINIMUM AND 2.690 INCHES MAXIMUM IN, overall_diameter: 1.375 INCHES NOMINAL IN, fsc_application_data: VALVE,BUTTERFLY, end_item_identification: ACFT TYPE C-141, criticality_code_justification: TEST. This part is cataloged in the U.S.
Government catalog under NSN 4810-00-016-1010, 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 | ALUMINUM ALLOY |
| overall_length | 2.670 INCHES MINIMUM AND 2.690 INCHES MAXIMUM IN |
| overall_diameter | 1.375 INCHES NOMINAL IN |
| fsc_application_data | VALVE,BUTTERFLY |
| end_item_identification | ACFT TYPE C-141 |
| criticality_code_justification | TEST |
| general_characteristics_item_description | WW-T-789 OR 6061-T6; INSIDE DIA 1.259 IN.; SLOT ONE SIDE; PART OF NSN 4810-00-974-2847 APPL TO PNEUMATIC SYSTEM TF33 TURBOJET ENGINE IN |
| NSN | 4810-00-016-1010 |
| FSC APPLICATION DATA | VALVE,BUTTERFLY |
| OVERALL DIAMETER | 1.375 INCHES NOMINAL IN |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | WW-T-789 OR 6061-T6; INSIDE DIA 1.259 IN.; SLOT ONE SIDE; PART OF NSN 4810-00-974-2847 APPL TO PNEUMATIC SYSTEM TF33 TURBOJET ENGINE IN |
| CRITICALITY CODE JUSTIFICATION | TEST |
| OVERALL LENGTH | 2.670 INCHES MINIMUM AND 2.690 INCHES MAXIMUM IN |
| TEST DATA DOCUMENT | 99193-664433 DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) |
| END ITEM IDENTIFICATION | ACFT TYPE C-141 |
| MATERIAL | ALUMINUM ALLOY |
No substitute or cross-reference records for this part.